The invention relates to a device for determining and/or monitoring at least one property (3) of a rivet element (4) on a transporting line (5), in particular to a processing machine (1) and/or a riveting unit (7) of a processing machine (1), wherein the device (2) has a transmitting coil (9) and a receiving coil (10), wherein a transmitting signal (12) can be fed into the transmitting coil (9) by means of a signal generator (11) and a receiving signal (13) induced in the receiving coil (10) can be evaluated by means of an evaluation unit (14) for determining and/or monitoring at least one property (3) of the rivet element (4) on the transporting line (5).
B21J 15/32 - Dispositifs pour placer ou maintenir en position les rivets, avec ou sans systèmes d'alimentation
B23P 19/00 - Machines effectuant simplement l'assemblage ou la séparation de pièces ou d'objets métalliques entre eux ou des pièces métalliques avec des pièces non métalliques, que cela entraîne ou non une certaine déformationOutils ou dispositifs à cet effet dans la mesure où ils ne sont pas prévus dans d'autres classes
B21J 15/14 - Machines à riveter spécialement adaptées au rivetage de pièces déterminées, p. ex. machines pour poser les garnitures de frein
G01N 27/00 - Recherche ou analyse des matériaux par l'emploi de moyens électriques, électrochimiques ou magnétiques
2.
METHOD AND MACHINING SYSTEM FOR MACHINING AN AIRCRAFT STRUCTURAL COMPONENT
Method for machining an aircraft structural component using a machining system, the machining system having a drilling unit and a riveting unit, a manufacturing process controller for actuating the components of the machining system, an optical sensor and a projection unit. The method comprising the steps of: projecting a pattern by the projection unit onto a machining point with a rivet element inserted into a drill hole of the machining point, detecting the machining point including the projection of the pattern by the sensor and generating corresponding detection data by the sensor, evaluating the detection data by an evaluation unit, adapting the tool control data for a drill hole to be drilled subsequently according to the manufacturing specification at a further machining point, in particular the countersink depth of the drill hole to be drilled, by the manufacturing process controller on the basis of the evaluation of the detection data.
B21J 15/14 - Machines à riveter spécialement adaptées au rivetage de pièces déterminées, p. ex. machines pour poser les garnitures de frein
B21J 15/28 - Dispositifs de commande spécialement adaptés aux machines à riveter, non limités à l'un des sous-groupes précédents
G01B 11/25 - Dispositions pour la mesure caractérisées par l'utilisation de techniques optiques pour mesurer des contours ou des courbes en projetant un motif, p. ex. des franges de moiré, sur l'objet
The invention relates to a device for processing fibre-reinforced plastic, more particularly for producing structural components for aircraft (2) or preforms for same, said device comprising at least two functional units (4), the functional units (4) comprising at least one feed unit (5) for feeding a laid fibre scrim web (6) and a processing unit (8) for processing the laid fibre scrim web (6), with a primary drive (9) for driving the laid fibre scrim web (6), with a control arrangement (10) for open-loop or closed-loop control of the primary drive (9). According to the invention the device (3) has at least one secondary drive (11) for driving the laid fibre scrim web (6), the device (3) has a force-measuring device (12) associated with the secondary drive (11), with a force sensor (13) for measuring a web tension in the laid fibre scrim web (6) by means of the control arrangement (10), the control arrangement (10) controls the secondary drive (11) in a feedback control routine, the feedback control routine comprises a secondary feedback circuit (14) to control the secondary drive (11), the control arrangement (10) in the feedback control routine supplies the web tension measured by the force-measuring device (12) associated with the secondary drive (11) as an actual value (15) to the secondary feedback circuit (14) and determines and sets a controlled variable (16) for the secondary drive (11) on the basis of the web tension in the secondary feedback circuit (14).
B29C 70/56 - Tensionnage des renforcements avant ou pendant le façonnage
B64F 5/10 - Fabrication ou assemblage d’aéronefs, p. ex. gabarits à cet effet
B29C 70/50 - Façonnage ou imprégnation par compression pour la fabrication d'objets de longueur indéfinie, p. ex. de "prepregs", de préimprégnés [SMC] ou de nappes multiaxiales [XMC]
B29C 70/54 - Parties constitutives, détails ou accessoiresOpérations auxiliaires
Various embodiments of the disclosure relate to a spreading unit, having a shaper, for spreading viscous material, in particular sealing material, on a component, wherein the shaper has a shaping contour for the forming of the viscous material in the course of the spreading. It is proposed that the shaping contour of the shaper for the forming of the viscous material is adjustable by actuator-based means.
B05C 11/02 - Appareils pour étaler ou répartir des liquides ou d'autres matériaux fluides déjà appliqués sur une surfaceRéglage de l'épaisseur du revêtement
B05C 11/04 - Appareils pour étaler ou répartir des liquides ou d'autres matériaux fluides déjà appliqués sur une surfaceRéglage de l'épaisseur du revêtement comportant des lames
The disclosure relates to a spreading unit having a shaper for spreading viscous material, in particular sealing material, on a component, wherein the shaper has a first shaping contour for shaping the viscous material in the process of the spreading, wherein at least a second shaping contour of the shaper for shaping the viscous material can be brought by means of an actuator, in a direction of spreading, into superimposition with the first shaping contour, so that a shape of the shaper is adjustable during an application process.
B05C 11/04 - Appareils pour étaler ou répartir des liquides ou d'autres matériaux fluides déjà appliqués sur une surfaceRéglage de l'épaisseur du revêtement comportant des lames
B05C 5/02 - Appareillages dans lesquels un liquide ou autre matériau fluide est projeté, versé ou répandu sur la surface de l'ouvrage à partir d'un dispositif de sortie en contact, ou presque en contact, avec l'ouvrage
B05C 17/005 - Outils à main ou appareils utilisant des outils tenus à la main pour appliquer ou étaler des liquides ou d'autres matériaux fluides sur des surfaces, pour enlever partiellement des liquides ou d'autres matériaux fluides des surfaces pour décharger par pression des matériaux à travers un orifice d'évacuation
Embodiments relate to an atomizer unit that has a chamber assembly with an injection chamber and an atomizer chamber. The injection chamber is connected to the atomizer chamber by a nozzle, and the atomizer unit has a first feed channel for feeding a first compressed air flow into the injection chamber, a second feed channel for feeding a second compressed air flow into the atomizer chamber, and an injection valve for injecting a coolant and/or lubricant into the first compressed air flow in the injection region of the injection chamber. The first compressed air flow flows from the injection chamber into the atomizer chamber through the nozzle, is atomized in the atomizer chamber by the nozzle, is combined with the second compressed air flow in the atomizer chamber in order to form a transport flow for transporting the injected coolant and/or lubricant, and can be conducted to the machining location.
B05B 1/24 - Buses, têtes de pulvérisation ou autres dispositifs de sortie, avec ou sans dispositifs auxiliaires tels que valves, moyens de chauffage avec des moyens pour chauffer le liquide ou autre matériau fluide, p. ex. électriquement
B05B 1/30 - Buses, têtes de pulvérisation ou autres dispositifs de sortie, avec ou sans dispositifs auxiliaires tels que valves, moyens de chauffage agencés pour commander un débit, p. ex. à l'aide de conduits de section réglable
B05B 7/00 - Appareillages de pulvérisation pour débiter des liquides ou d'autres matériaux fluides provenant de plusieurs sources, p. ex. un liquide et de l'air, une poudre et un gaz
B05B 7/04 - Pistolets pulvérisateursAppareillages pour l'évacuation avec des dispositifs permettant le mélange de liquides ou d'autres matériaux fluides avant l'évacuation
B23Q 11/10 - Dispositions pour le refroidissement ou la lubrification des outils ou des pièces travaillées
A floor-bound vehicle, in particular for a movable production plant with a processing unit for processing a workpiece, with at least two drive units, wherein the drive units each comprise at least one drive wheel, a travel drive for driving the at least one drive wheel, a wheel carrier on which the at least one drive wheel is arranged, and a steering drive for adjusting the wheel carrier with the drive wheel about a geometric steering axis and thus steering the drive wheel, wherein for steering, the respective wheel carrier can be adjusted relative to the respective travel drive by means of the respective steering drive is provided.
B62D 5/04 - Direction assistée ou à relais de puissance électrique, p. ex. au moyen d'un servomoteur relié au boîtier de direction ou faisant partie de celui-ci
B62D 7/04 - Timonerie de directionFusées ou leur montage pour bogies à pivot comportant plus d'une roue
A method for machining a workpiece is provided, wherein drilling of the workpiece and subsequent countersinking of the bore, obtained by the drilling, in the workpiece are performed by means of a drilling/countersinking tool in a machining process, wherein the drilling/countersinking tool in the machining process while being axially rotated is subjected to an axial feed movement relative to the workpiece that reaches a counterbore terminal position, and wherein the axial feed movement is superimposed by an axial vibration, wherein, when reaching a predefined frequency lowering position of the axial feed movement by the drilling/countersinking tool, the frequency of the axial vibration is lowered to a final machining frequency, and the machining process is continued at the final machining frequency as the maximum frequency of the axial vibration until the counterbore terminal position is reached.
B23B 35/00 - Méthodes d'alésage ou de perçage ou autres méthodes de travail impliquant l'utilisation de machines à aléser ou à percerUtilisation d'équipements auxiliaires en relation avec ces méthodes
B23B 51/10 - Forets à chanfreiner, p. ex. travaillant comme des fraises
B23B 47/34 - Agencements pour enlever les copeaux des trous pendant le perçageAgencements fixés à l'outil pour briser les copeaux
A device for producing preforms for aircraft structural components, wherein the device has a supply unit, which is designed to supply a layered structure having at least one material ply of a thermally activatable, flexible fiber composite material, together with a protective film arranged in each case on at least one outer side of the layered structure, wherein the device has at least one shaping unit, which is arranged downstream of the supply unit in a conveying direction and is designed to shape the layered structure supplied, wherein in that the layered structure, together with the respective protective film, can be fed to the shaping unit or to one of the shaping units with a cross-sectional profile with which the protective film or at least one of the protective films extends along a straight line.
B29C 70/50 - Façonnage ou imprégnation par compression pour la fabrication d'objets de longueur indéfinie, p. ex. de "prepregs", de préimprégnés [SMC] ou de nappes multiaxiales [XMC]
B29B 11/16 - Fabrication de préformes caractérisées par la structure ou la composition comprenant des charges ou des agents de renforcement
B29C 70/54 - Parties constitutives, détails ou accessoiresOpérations auxiliaires
10.
METHOD AND MACHINING SYSTEM FOR MACHINING AN AIRCRAFT STRUCTURAL COMPONENT
The invention relates to a method for machining an aircraft structural component (2) using a machining system (1), the machining system (1) having a drilling unit (3a) and a riveting unit (3b), there being provided a manufacturing process controller (9) for actuating the components of the machining system (1), the manufacturing process controller (9) executing a sequence of drilling operations by means of the drilling unit (3a) and of riveting operations by means of the riveting unit (3b) using tool control data (9a) according to a manufacturing specification (10), the machining system (1) having an optical sensor (12) and a projection unit (13), the method comprising the steps of: • - projecting a pattern (M) by means of the projection unit (13) onto a machining point (B) with a rivet element (4) inserted into a drill hole (11) of the machining point (B), • - detecting the machining point (B) including the projection of the pattern (M) by means of the sensor (12) and generating corresponding detection data (14) by means of the sensor (12), • - evaluating the detection data (14) by means of an evaluation unit (15), • - adapting the tool control data (9a) for a drill hole (11) to be drilled subsequently according to the manufacturing specification (10) at a further machining point (BI), in particular the countersink depth (T) of the drill hole (11) to be drilled, by means of the manufacturing process controller (9) on the basis of the evaluation of the detection data (14). The invention also relates to a machining system.
B21J 15/14 - Machines à riveter spécialement adaptées au rivetage de pièces déterminées, p. ex. machines pour poser les garnitures de frein
B21J 15/28 - Dispositifs de commande spécialement adaptés aux machines à riveter, non limités à l'un des sous-groupes précédents
G01B 11/16 - Dispositions pour la mesure caractérisées par l'utilisation de techniques optiques pour mesurer la déformation dans un solide, p. ex. indicateur optique de déformation
G01B 11/25 - Dispositions pour la mesure caractérisées par l'utilisation de techniques optiques pour mesurer des contours ou des courbes en projetant un motif, p. ex. des franges de moiré, sur l'objet
Embodiments provide a mobile robot platform for processing an aircraft structural component with a robot, with a platform which can be moved on a floor in a horizontal movement direction, and with a height adjustment unit, arranged on the platform, the robot being arranged in a vertically adjustable fashion on the height adjustment unit and in at least one processing mode of the mobile robot platform the height adjustment unit is arranged in a non-pivoting fashion with respect to the platform, the robot having robot kinematics for positioning an end effector, and the robot kinematics having a first robot joint with a first robot limb, which is mounted ahead of the first robot joint, and with a second robot limb, which is mounted after the first robot joint, and a second robot joint ahead of which the second robot limb is mounted and after which a third robot limb is mounted.
B25J 5/00 - Manipulateurs montés sur roues ou sur support mobile
B21J 15/14 - Machines à riveter spécialement adaptées au rivetage de pièces déterminées, p. ex. machines pour poser les garnitures de frein
B25J 9/04 - Manipulateurs à commande programmée caractérisés par le mouvement des bras, p. ex. du type à coordonnées cartésiennes par rotation d'au moins un bras en excluant le mouvement de la tête elle-même, p. ex. du type à coordonnées cylindriques ou polaires
B64F 5/50 - Manipulation ou transport des composants d'aéronefs
The invention relates to a method for disinfecting a processing environment (1) using a cobot (2) in cooperation with a human processor (3), wherein the cobot (2) has a manipulator (4) having at least one end effector (5, 6) for disinfecting objects (7) in the processing environment (1), a drive arrangement (8) for moving the cobot (2) and a sensor arrangement (9) which is used to determine object-related sensor data for at least one object (7) in the processing environment (1), wherein the object (7) is processed in a work routine according to a treatment plan stipulated by means of a system controller (10). It is proposed that the treatment plan for the object (7) is stipulated by means of the system controller (10) in a planning routine according to a predefined planning rule on the basis of the object-related sensor data, on the basis of environmental parameters based on the processing environment (1) and on the basis of processor data relating to the human processor (3).
A61L 2/16 - Procédés ou appareils de désinfection ou de stérilisation de matériaux ou d'objets autres que les denrées alimentaires ou les lentilles de contactAccessoires à cet effet utilisant des substances chimiques
The invention relates to a device for processing fibre-reinforced plastic, more particularly for producing structural components for aircraft (2) or preforms for same, said device comprising at least two functional units (4), the functional units (4) comprising at least one feed unit (5) for feeding a laid fibre scrim web (6) and a processing unit (8) for processing the laid fibre scrim web (6), with a primary drive (9) for driving the laid fibre scrim web (6), with a control arrangement (10) for open-loop or closed-loop control of the primary drive (9). According to the invention the device (3) has at least one secondary drive (11) for driving the laid fibre scrim web (6), the device (3) has a force-measuring device (12) associated with the secondary drive (11), with a force sensor (13) for measuring a web tension in the laid fibre scrim web (6) by means of the control arrangement (10), the control arrangement (10) controls the secondary drive (11) in a feedback control routine, the feedback control routine comprises a secondary feedback circuit (14) to control the secondary drive (11), the control arrangement (10) in the feedback control routine supplies the web tension measured by the force-measuring device (12) associated with the secondary drive (11) as an actual value (15) to the secondary feedback circuit (14) and determines and sets a controlled variable (16) for the secondary drive (11) on the basis of the web tension in the secondary feedback circuit (14).
B29C 70/50 - Façonnage ou imprégnation par compression pour la fabrication d'objets de longueur indéfinie, p. ex. de "prepregs", de préimprégnés [SMC] ou de nappes multiaxiales [XMC]
B29C 70/54 - Parties constitutives, détails ou accessoiresOpérations auxiliaires
B29C 67/00 - Techniques de façonnage non couvertes par les groupes , ou
B29C 70/56 - Tensionnage des renforcements avant ou pendant le façonnage
14.
Atomizer unit of a minimal quantity lubrication system
An atomizer unit of a lubrication system has a chamber arrangement having a chamber arrangement interior, at least one first supply duct for supplying a first compressed-air stream into and through the chamber arrangement interior to a continuation duct, and an injection valve for injecting a coolant and/or lubricant into an injection region into the first compressed-air stream in the chamber arrangement interior. The atomizer unit has at least one second supply duct for supplying a second compressed-air stream into and through the chamber arrangement interior to the continuation duct. The atomizer unit is designed in such a manner that the second compressed-air stream combines with the first compressed-air stream and with the coolant and/or lubricant possibly injected into the first compressed-air stream, to form a transport stream for transporting the injected coolant and/or lubricant, and the transport stream is routed through the continuation duct to the machining location.
B05B 1/08 - Buses, têtes de pulvérisation ou autres dispositifs de sortie, avec ou sans dispositifs auxiliaires tels que valves, moyens de chauffage agencés pour produire un jet, un pulvérisat ou tout autre écoulement de forme ou de nature particulière, p. ex. sous forme de gouttes individuelles de nature pulsatoire, p. ex. débitant un liquide en quantités successives séparées
B05B 7/00 - Appareillages de pulvérisation pour débiter des liquides ou d'autres matériaux fluides provenant de plusieurs sources, p. ex. un liquide et de l'air, une poudre et un gaz
B05B 7/04 - Pistolets pulvérisateursAppareillages pour l'évacuation avec des dispositifs permettant le mélange de liquides ou d'autres matériaux fluides avant l'évacuation
Various embodiments relate to a device for the production of preforms for aircraft structural components, having a supply unit for the continuous supply of a layer structure with at least one fiber layer, having a heating unit with at least one infrared heater which has an infrared radiation source, wherein the supplied layer structure is passed through the heating unit in a conveying direction and can be heated there over at least part of its width in cross section by the at least one infrared heater, a disk which is permeable to infrared radiation being arranged between the layer structure and the infrared heater.
The invention relates to an atomizer unit of a minimal quantity lubricant system (2) for a cooling and/or lubricating function of a cutting-machining process. The atomizer unit (3) has a chamber assembly (8) with an injection chamber (9) and an atomizer chamber (10), wherein the injection chamber (9) is connected to the atomizer chamber (10) by a nozzle (11), and the atomizer unit (3) has at least one first feed channel (12) for feeding a first compressed air flow (13) into the injection chamber (9), at least one second feed channel (14) for feeding a second compressed air flow (15) into the atomizer chamber (10), and an injection valve (16) for injecting a coolant and/or lubricant (4) into the first compressed air flow (13) in the injection region (17) of the injection chamber (9). The atomizer unit (3) is designed such that the first compressed air flow (13) flows from the injection chamber (9) into the atomizer chamber (10) through the nozzle (11), is atomized in the atomizer chamber by the nozzle (11), is combined with the second compressed air flow (15) in the atomizer chamber (10) in order to form a transport flow (18) for transporting the injected coolant and/or lubricant (4), and can be conducted to the machining location (7). The atomizer unit (3) has a heater (20) which heats the coolant and/or lubricant (4), the first compressed air flow (13), the second compressed air flow (15), and/or the transport flow (18).
B23Q 11/10 - Dispositions pour le refroidissement ou la lubrification des outils ou des pièces travaillées
B05B 7/00 - Appareillages de pulvérisation pour débiter des liquides ou d'autres matériaux fluides provenant de plusieurs sources, p. ex. un liquide et de l'air, une poudre et un gaz
The invention relates to a floor-bound vehicle, in particular for a movable production system (1) having a processing unit (2) for processing a workpiece (3), the floor-bound vehicle comprising at least two drive units (5), the drive units (5) each comprising: at least one drive wheel (6); a travel drive (7) for driving the at least one drive wheel (6); a wheel carrier (8), on which the at least one drive wheel (6) is arranged; and a steering drive (9) for moving the wheel carrier (8) with the drive wheel (6) about a geometric steering axis (L) and thus steering the drive wheel (6). For steering, the wheel carrier (8) in question can be moved relative to the travel drive (7) in question by the steering drive (9) in question.
B62D 5/04 - Direction assistée ou à relais de puissance électrique, p. ex. au moyen d'un servomoteur relié au boîtier de direction ou faisant partie de celui-ci
B60G 3/00 - Suspensions élastiques pour une seule roue
B62D 7/04 - Timonerie de directionFusées ou leur montage pour bogies à pivot comportant plus d'une roue
18.
Machining system for aircraft structural components
The disclosure relates to a processing installation for aircraft structural components having a processing station comprising a clamping frame for receiving the structural component, wherein the clamping frame extends along a station longitudinal axis which extends in a longitudinal direction and a processing unit which has an upper tool unit having an upper tool and a lower tool unit, wherein the processing installation has a processing region which is formed by a laterally delimited, first spatial portion in which the clamping frame and the processing unit are arranged during processing, wherein the processing installation has a service region for carrying out service operations, wherein the first spatial portion is separated from the second spatial portion in a transverse direction, wherein a service platform is arranged in the service region and can be positioned in a service plane which is orthogonal to the vertical direction.
B21J 15/14 - Machines à riveter spécialement adaptées au rivetage de pièces déterminées, p. ex. machines pour poser les garnitures de frein
B64F 5/10 - Fabrication ou assemblage d’aéronefs, p. ex. gabarits à cet effet
B21J 13/08 - Accessoires pour la manipulation des pièces ou des outils
B21J 15/42 - Dispositifs particuliers de serrage des pièces à riveter ensemble, p. ex. dispositifs travaillant au travers des trous de rivet
B23Q 1/48 - Supports mobiles ou réglables d'outils ou de pièces utilisant des mécanismes particuliers avec des guidages en translation et des guidages en rotation
B23Q 3/157 - Agencements pour insérer ou retirer automatiquement les outils les outils rotatifs
B23Q 1/25 - Supports mobiles ou réglables d'outils ou de pièces
B23Q 41/04 - Caractéristiques se rapportant à la disposition des machines
B21J 15/36 - Outils et contre-outils pour former les têtes de rivetsMandrins pour le rivetage par expansion des rivets creux
B25J 5/04 - Manipulateurs montés sur roues ou sur support mobile se déplaçant le long d'un chemin de guidage dans lequel le chemin de guidage est aussi mobile, p. ex. du type pont roulant
The invention relates to a device for producing preforms (3) for aircraft structural parts (2), the device having a delivery unit (6) which is designed to deliver a layered structure (13) having at least one material ply (4) of a thermally activatable, flexible, fibre-reinforced composite material together with a protective foil (14) arranged on at least one outer side of the layered structure (13), the device having at least one shaping unit (7a, 7b) which is situated downstream of the delivery unit (6) in a conveying direction (F) and is designed to shape the delivered layered structure (13). According to the invention, the layered structure (13) together with the corresponding protective foil (14) can be supplied to the shaping unit (Ta) or to one of the shaping units (7a, 7b) with a cross-sectional profile with which the protective foil (14) or at least one of the protective foils (14) extends along a straight line (G).
B29B 11/16 - Fabrication de préformes caractérisées par la structure ou la composition comprenant des charges ou des agents de renforcement
B29C 70/50 - Façonnage ou imprégnation par compression pour la fabrication d'objets de longueur indéfinie, p. ex. de "prepregs", de préimprégnés [SMC] ou de nappes multiaxiales [XMC]
The invention relates to a method for machining a workpiece (1), wherein a drilling of the workpiece (1) and subsequent countersinking of the bore in the workpiece (1) obtained by the drilling are carried out in a machining process by means of a drilling-countersinking tool (2), wherein the drilling-countersinking tool (2) is subjected in the machining process, under axial rotation, to an axial feed movement relative to the workpiece (1), and wherein the axial feed movement is superimposed by an axial vibration. According to the invention, when a specified frequency lowering position (SF) of the axial feed movement is reached by the drilling-countersinking tool (1), the frequency (f) of the axial vibration is lowered to a final machining frequency (fc) and the machining process is continued at the final machining frequency (fc) as the maximum frequency (f) of the axial vibration until reaching the lowering final position (SE).
Various embodiments relate to a rivet element supply unit for providing rivet elements, wherein the rivet element supply unit comprises a rivet element provision unit and a handling unit, wherein the rivet element provision unit for conveying the rivet elements comprises a spiral conveyor having a longitudinal axis and a spiral, which extends around the longitudinal axis, wherein the longitudinal axis is inclined to the direction of gravity, wherein the rivet element provision unit has a pick-up region to which the spiral conveyor supplies rivet elements and from which the handling unit picks up the rivet elements for transporting to a rivet element receptacle.
B21J 15/14 - Machines à riveter spécialement adaptées au rivetage de pièces déterminées, p. ex. machines pour poser les garnitures de frein
B65G 3/04 - Emmagasinage de matériaux en vrac ou d'objets en vrac, c.-à-d. en désordre dans des réservoirs, des trémies ou dans de grands réceptacles de ce genre
B65G 11/06 - Colonnes de descente hélicoïdales ou en spirale
An end effector for laying down fibers on a laying mold, the end effector having at least one bobbin arrangement of a system type, the system type being defined by virtue of the fact that the bobbin arrangement has a first bobbin for providing a first fiber strand and a second bobbin for providing a second fiber strand, the rotational axes of the first and the second bobbin being arranged at an angle with respect to one another, the first fiber strand and the second fiber strand being merged over a deflection unit and being guided from a corner region of the end effector jointly into a center region of the end effector and further to a pressure roller.
A processing installation for aircraft structural components having a processing station comprising a clamping frame, wherein the clamping frame extends along a station longitudinal axis which extends in a longitudinal direction, and a processing unit which has an upper tool unit having an upper tool which is orientated along a first tool axis and a lower tool unit having a lower tool which is orientated along a second tool axis, wherein the first tool axis and the second tool axis can be orientated parallel with a vertical direction which is angular, in particular orthogonal, relative to the longitudinal direction, wherein in at least one processing position of the upper tool and in at least one processing position of the lower tool the first tool axis and the second tool axis are orientated coaxially relative to each other, and wherein the lower tool is supported on a lower tool carrier.
B64F 5/10 - Fabrication ou assemblage d’aéronefs, p. ex. gabarits à cet effet
B21J 15/14 - Machines à riveter spécialement adaptées au rivetage de pièces déterminées, p. ex. machines pour poser les garnitures de frein
B21J 15/42 - Dispositifs particuliers de serrage des pièces à riveter ensemble, p. ex. dispositifs travaillant au travers des trous de rivet
B23Q 1/48 - Supports mobiles ou réglables d'outils ou de pièces utilisant des mécanismes particuliers avec des guidages en translation et des guidages en rotation
B23Q 1/52 - Supports mobiles ou réglables d'outils ou de pièces utilisant des mécanismes particuliers avec des guidages en rotation uniquement avec un seul guidage en rotation
A separator for rivet elements, having an entrance and an exit for the rivet elements to be separated and having a guide extending along a center line from the entrance to the exit, through which the rivet elements can be delivered along a delivery direction, wherein the separator comprises a first blocking element, especially a first pin, and a second blocking element spaced apart from the first blocking element along the center line, wherein the first blocking element and the second blocking element are movable independently of each other between a blocking position blocking the guide for a rivet element and a releasing position releasing the guide for a rivet element. It is proposed that at least one blocking element is arranged such that the direction of movement of the blocking element or elements is oriented at a slant to the delivery direction of the rivet elements.
The disclosure relates to a processing installation for aircraft structural components having a processing station comprising a clamping frame, wherein the clamping frame extends along a station longitudinal axis, and a processing unit which has a first upper tool unit having an upper tool which is orientated along a first tool axis and a lower tool unit having a lower tool which is orientated along a second tool axis wherein the first tool axis and the second tool axis can be orientated parallel with a vertical direction which is angled with respect to the longitudinal direction, and wherein in at least one processing position of the upper tool of the first upper tool unit and in at least one processing position of the lower tool of the lower tool unit the first tool axis and the second tool axis are orientated coaxially relative to each other.
B64F 5/10 - Fabrication ou assemblage d’aéronefs, p. ex. gabarits à cet effet
B21J 13/08 - Accessoires pour la manipulation des pièces ou des outils
B21J 15/14 - Machines à riveter spécialement adaptées au rivetage de pièces déterminées, p. ex. machines pour poser les garnitures de frein
B21J 15/42 - Dispositifs particuliers de serrage des pièces à riveter ensemble, p. ex. dispositifs travaillant au travers des trous de rivet
B23Q 39/02 - Machines pour le travail des métaux incorporant un grand nombre de sous-ensembles capables chacun de réaliser une opération de travail du métal les sous-ensembles étant susceptibles d'être mis en fonctionnement à un seul poste de travail
B25J 5/00 - Manipulateurs montés sur roues ou sur support mobile
B25J 9/04 - Manipulateurs à commande programmée caractérisés par le mouvement des bras, p. ex. du type à coordonnées cartésiennes par rotation d'au moins un bras en excluant le mouvement de la tête elle-même, p. ex. du type à coordonnées cylindriques ou polaires
B64F 5/00 - Tracé, fabrication, assemblage, nettoyage, entretien ou réparation des aéronefs, non prévus ailleursManipulation, transport, test ou inspection de composants d’aéronefs, non prévus ailleurs
Various embodiments relate to a method for supplying a riveting machine with rivet elements, in particular during operation of the riveting machine, wherein at least one rivet element providing arrangement comprising at least one rivet element providing unit for providing and separating the rivet element is provided, wherein the riveting machine has a rivet element receiving arrangement comprising at least one rivet element receptacle for receiving the rivet elements, wherein at least a part of the transport from one of the rivet element providing units to one of the rivet element receptacles is realized in a robot-based manner.
B generates a low pressure for holding the workpiece, and wherein at least one gripper device has a different gripper unit, which carries the workpiece according to a physical principle which differs from that of the Bernoulli gripper unit.
The invention relates to an atomizer unit of a minimal quantity lubrication system (3) for cooling and/or lubricating a chip-removing machining process between a tool (5) and a workpiece (6) at a machining station, wherein the atomizer unit (2) has a chamber arrangement (8) with a chamber arrangement interior (9), at least one first supply duct (10) for supplying a first compressed air stream (11) into and through the chamber arrangement interior (9) to a continuation duct (12) and an injection valve (13) for injecting a coolant and/or lubricant (4) into an injection region (14) into the first compressed air stream (11) in the chamber arrangement interior (9). It is proposed that the atomizer unit (2) has at least one second supply duct (15) for supplying a second compressed air stream (16) into and through the chamber arrangement interior (9) to the continuation duct (12), wherein the atomizer unit (2) is configured such that the second compressed air stream (16) joins the first compressed air stream (11), and any coolant and/or lubricant (4) injected into the first compressed air stream (11), downstream of the injection region (14) to form a transport stream (17) for transporting the injected coolant and/or lubricant (4), and wherein the transport stream (17) is conveyed through the continuation duct (12) to the machining station (7).
B05B 7/24 - Appareillages de pulvérisation pour débiter des liquides ou d'autres matériaux fluides provenant de plusieurs sources, p. ex. un liquide et de l'air, une poudre et un gaz avec des moyens, p. ex. un récipient, pour alimenter en liquide ou autre matériau fluide un dispositif de décharge
B21J 15/14 - Machines à riveter spécialement adaptées au rivetage de pièces déterminées, p. ex. machines pour poser les garnitures de frein
B05B 7/00 - Appareillages de pulvérisation pour débiter des liquides ou d'autres matériaux fluides provenant de plusieurs sources, p. ex. un liquide et de l'air, une poudre et un gaz
B05B 7/04 - Pistolets pulvérisateursAppareillages pour l'évacuation avec des dispositifs permettant le mélange de liquides ou d'autres matériaux fluides avant l'évacuation
B05B 7/12 - Pistolets pulvérisateursAppareillages pour l'évacuation agencés pour commander le volume débité, p. ex. à l'aide de passages réglables
B23Q 11/00 - Accessoires montés sur les machines-outils pour maintenir les outils ou les organes de la machine dans de bonnes conditions de travail ou pour refroidir les pièces travailléesDispositifs de sécurité spécialement combinés aux machines-outils, disposés dans ces machines ou spécialement conçus pour être utilisés en relation avec ces machines
B05B 1/08 - Buses, têtes de pulvérisation ou autres dispositifs de sortie, avec ou sans dispositifs auxiliaires tels que valves, moyens de chauffage agencés pour produire un jet, un pulvérisat ou tout autre écoulement de forme ou de nature particulière, p. ex. sous forme de gouttes individuelles de nature pulsatoire, p. ex. débitant un liquide en quantités successives séparées
The disclosure relates to an articulated robot having a serial kinematic mechanism for positioning an end effector, the kinematic mechanism having at least one part kinematic mechanism with a robot joint, with a robot limb mounted upstream of the robot joint, and with a robot limb mounted downstream of the robot joint. The at least one part kinematic mechanism has a linear drive, with a drive element, and a coupler with two coupler joints which are spaced apart from one another along the coupler extent, wherein the linear drive is arranged on a first robot limb of the part kinematic mechanism, and wherein the coupler is articulated on one side on the drive element of the linear drive and on the other side on the second robot limb of the part kinematic mechanism, spaced apart from the geometric axis of the robot joint of the part kinematic mechanism.
B25J 9/04 - Manipulateurs à commande programmée caractérisés par le mouvement des bras, p. ex. du type à coordonnées cartésiennes par rotation d'au moins un bras en excluant le mouvement de la tête elle-même, p. ex. du type à coordonnées cylindriques ou polaires
B25J 9/06 - Manipulateurs à commande programmée caractérisés par des bras à articulations multiples
B25J 9/10 - Manipulateurs à commande programmée caractérisés par des moyens pour régler la position des éléments manipulateurs
B25J 9/12 - Manipulateurs à commande programmée caractérisés par des moyens pour régler la position des éléments manipulateurs électriques
An application unit for applying a viscous material to a component edge, in particular of varying width, of a component, wherein the application unit has a nozzle for applying the viscous material to the component edge, having a discharge opening of adjustable width, and wherein the application unit has a first feeler having a contact surface for contact against the component and a second feeler having a contact surface for contact against the component, wherein the first feeler and the second feeler are pretensionable with a pretensioning arrangement in opposite directions, and wherein the width of the discharge opening is adaptable in dependence on the distance of the contact surface of the first feeler from the contact surface of the second feeler.
B05C 5/02 - Appareillages dans lesquels un liquide ou autre matériau fluide est projeté, versé ou répandu sur la surface de l'ouvrage à partir d'un dispositif de sortie en contact, ou presque en contact, avec l'ouvrage
B05C 17/005 - Outils à main ou appareils utilisant des outils tenus à la main pour appliquer ou étaler des liquides ou d'autres matériaux fluides sur des surfaces, pour enlever partiellement des liquides ou d'autres matériaux fluides des surfaces pour décharger par pression des matériaux à travers un orifice d'évacuation
32.
Method for filling a rivet cartridge with rivet elements
A method is provided for filling a rivet cartridge with rivet elements by means of a rivet loading station having a rivet delivery unit for delivering the rivet elements and having a rivet cartridge receiving means for receiving a rivet cartridge. The rivet elements are supplied from the rivet delivery unit to a rivet cartridge which is received in the rivet cartridge receiving means and are received therein in an aligned manner. The rivet loading station detects pre-determined characteristics of the rivet elements that are relevant to the drilling process and/or the riveting process prior to supplying them to the rivet cartridge.
B21J 15/32 - Dispositifs pour placer ou maintenir en position les rivets, avec ou sans systèmes d'alimentation
B21J 15/28 - Dispositifs de commande spécialement adaptés aux machines à riveter, non limités à l'un des sous-groupes précédents
B23P 19/00 - Machines effectuant simplement l'assemblage ou la séparation de pièces ou d'objets métalliques entre eux ou des pièces métalliques avec des pièces non métalliques, que cela entraîne ou non une certaine déformationOutils ou dispositifs à cet effet dans la mesure où ils ne sont pas prévus dans d'autres classes
33.
Gripping device having a Bernoulli gripping unit and a vacuum gripping unit
The disclosure relates to a gripping device for an end effector of a manipulator for holding a workpiece via its workpiece surface, having a Bernoulli gripping unit, with an outflow unit for discharging a flow from the Bernoulli gripping unit between gripping device and workpiece surface in such a manner that in a region—Bernoulli-negative pressure region—a static negative pressure for holding the workpiece is generatable by the flow, and having a vacuum gripping unit with a suction chamber, wherein in a region delimited by the suction chamber—vacuum negative pressure region—a static negative pressure for holding the workpiece is generatable, wherein the Bernoulli negative pressure region and the vacuum negative pressure region intersect at least in part or wherein the Bernoulli negative pressure region and the vacuum negative pressure region surround one another.
An apparatus for applying a viscous material, comprising a bell having a circumferential mounting rim, and a feed line, wherein the material is conveyable via a conveying element through the feed line into the bell, wherein the bell can be transported with the mounting rim, in a direction of mounting, over a protruding element, in particular a rivet head, of a component, in order to encase the element with the material, wherein in the region of the bell or the feed line a metering member is provided, wherein in the course of an application process a flow of the material can be influenced by the metering member.
B05C 5/02 - Appareillages dans lesquels un liquide ou autre matériau fluide est projeté, versé ou répandu sur la surface de l'ouvrage à partir d'un dispositif de sortie en contact, ou presque en contact, avec l'ouvrage
B05C 11/10 - Stockage, débit ou réglage du liquide ou d'un autre matériau fluideRécupération de l'excès de liquide ou d'un autre matériau fluide
B05D 1/26 - Procédés pour appliquer des liquides ou d'autres matériaux fluides aux surfaces par application de liquides ou d'autres matériaux fluides, à partir d'un orifice en contact ou presque en contact avec la surface
B05D 7/14 - Procédés, autres que le flocage, spécialement adaptés pour appliquer des liquides ou d'autres matériaux fluides, à des surfaces particulières, ou pour appliquer des liquides ou d'autres matériaux fluides particuliers à du métal, p. ex. à des carrosseries de voiture
The invention relates to a device for producing preforms (3) for aircraft structural components (2), said device having a delivery unit (6), for continuously delivering a layered structure (7) with at least one fibre layer (4), and a heating unit (8) with at least one infra-red heater (9), which has an infra-red radiation source (10), wherein the delivered layered structure (7) is guided through the heating unit (8) in a conveying direction (F) and is heatable there over at least some of its width (B) in cross-section by the at least one infra-red heater (9), wherein a plate (11) which is permeable to infra-red radiation is arranged between the layered structure (7) and the infra-red heater (9).
The disclosure relates to a method for filling a rivet cartridge with rivet elements by means of a rivet loading station having a rivet delivery unit for delivering the rivet elements and having a rivet cartridge receiving means for receiving a rivet cartridge, wherein the rivet elements are supplied from the rivet delivery unit to a rivet cartridge which is received in the rivet cartridge receiving means and are received therein in an aligned manner. It is proposed that at least part of the transport from the rivet delivery unit to the rivet cartridge is effected in a robot-based manner.
B65G 47/14 - Dispositifs pour alimenter en objets ou matériaux les transporteurs pour alimenter en objets à partir de piles d'objets en désordre ou de tas d'objets en vrac disposant ou présentant les objets par des moyens mécaniques ou pneumatiques durant l'alimentation
515252) of the first and the second spools (5, 5a, 5b) are arranged at an angle to one another, wherein the first fibre strand (6, 6a) and the second fibre strand (6, 6b) are brought together via a deflection unit (7, 7a, 7b) and guided together from a corner region (8, 8a, 8b) of the end effector (2) into a central region (9) of the end effector (2) and onwards to a pressure roller (10).
The invention relates to a separator for rivet elements (3), comprising an inlet (4) and an outlet (5) for the rivet elements (3) to be separated and comprising a guide (6), which extends along a center line (M) from the inlet (4) to the outlet (5) and through which the rivet elements (3) can be conveyed in a conveying direction (F). The separator (2) has a first blocking element (8), in particular a first pin, and a second blocking element (9), in particular a second pin, which is spaced apart from the first blocking element (8) along the center line (M). The first blocking element (8) and the second blocking element (9) can be moved independently of each other between a blocking position, in which the blocking element blocks the guide (6) for a rivet element (3), and an unblocking position, in which the blocking element unblocks the guide (6) for a rivet element (3). According to the invention, at least one blocking element (8, 9), preferably both blocking elements (8, 9), is arranged in such a way that the direction of movement (B1, B2) of the one or both blocking elements (8, 9) is oriented oblique to the conveying direction (F) of the rivet elements (3).
The invention relates to a machining facility for aircraft structural components (2), comprising a machining station (3) having a mounting frame (4) for receiving each aircraft structural component (2) to be machined, the mounting frame (4) extending along a longitudinal axis (6) of the station, which runs in a longitudinal direction (X), and a machining unit (5) for machining the aircraft structural component (2), comprising a first upper tool unit (11) with an upper tool (13) oriented along a first tool axis (12a) and a lower tool unit (14) with a lower tool (15) oriented along a second tool axis (12b), the first tool axis (12a) and the second tool axis (12b) being oriented or orientable parallel to a height direction (Z) which is at an angle, particularly orthogonal, to the longitudinal direction (X), and in at least one machining position of the upper tool (13) of the first upper tool unit (11) and in at least one machining position of the lower tool (15) of the lower tool unit (14), the first tool axis (12a) and the second tool axis (12b) are oriented coaxially to each other. According to the invention, the machining unit (5) comprises a second upper tool unit (11') with an upper tool (13') oriented along a third tool axis (12a'), the third tool axis (12a') being oriented or orientable parallel to the height direction (Z), and in at least one machining position of the upper tool (13') of the second upper tool unit (11') and in at least one machining position of the lower tool (15) of the lower tool unit (14), the second tool axis (12b) and the third tool axis (12a') are oriented coaxially to each other.
B64F 5/10 - Fabrication ou assemblage d’aéronefs, p. ex. gabarits à cet effet
B21J 15/14 - Machines à riveter spécialement adaptées au rivetage de pièces déterminées, p. ex. machines pour poser les garnitures de frein
B23Q 39/04 - Machines pour le travail des métaux incorporant un grand nombre de sous-ensembles capables chacun de réaliser une opération de travail du métal les sous-ensembles étant disposés pour fonctionner simultanément à différents postes de travail, p. ex. avec une table de travail annulaire se déplaçant par paliers
40.
PROCESSING SYSTEM FOR AIRCRAFT STRUCTURAL COMPONENTS
The invention relates to a processing system for aircraft structural components (2), having a processing station (3) comprising a clamping frame (4) for receiving each particular aircraft structural component (2) to be processed, wherein the clamping frame (4) extends along a station longitudinal axis (6) extending in a longitudinal direction (X), and a processing unit (5) for processing the aircraft structural component (2), said unit (5) having an upper tool unit (11) with an upper tool (13) oriented along a first tool axis (12a) and a lower tool unit (14) with a lower tool (15) oriented along a second tool axis (12b), wherein the first tool axis (12a) and the second tool axis (12b) are oriented or orientable parallel to a vertical direction (Z) that is at an angle, in particular orthogonal, to the longitudinal direction (X), wherein, in at least one processing position of the upper tool (13) and in at least one processing position of the lower tool (15), the first tool axis (12a) and the second tool axis (12b) are oriented coaxially with one another and wherein the lower tool (15) is mounted on a lower tool carrier (17). It is proposed that, in at least one processing position of the upper tool (13) and/or in at least one processing position of the lower tool (15), the particular tool axis (12a, 12b) does not extend coaxially with the lower tool carrier axis (18).
The invention relates to a machining system for aircraft structural components (2), having a machining station (3), which comprises a clamping frame (4) for holding the aircraft structural component (2) to be machined, the clamping frame (4) extending along a station longitudinal axis (6) extending in a longitudinal direction (X), and which comprises a machining unit (5) for machining the aircraft structural component (2), which machining unit has an upper tool unit (11) having an upper tool (13) oriented along a first tool axis (12a) and has a lower tool unit (14) having a lower tool (15) oriented along a second tool axis (12b), the first tool axis (12a) and the second tool axis (12b) extending parallel to a vertical direction (Z), which is at an angle to, in particular orthogonal to, the longitudinal direction (X), the machining system (1) having a machining region (B) for machining the aircraft structural component (2), which machining region is formed by a laterally delimited, first spatial region (R1), in which the clamping frame (4) and the machining unit (5) are arranged during the machining, and the machining system (1) having a service region (S) for the performance of service work, which service region is formed by a laterally delimited, second spatial region (R2), the first spatial region (R1) being separated from the second spatial region (R2) in a perpendicular direction (Y) orthogonal to the longitudinal direction (X) and the vertical direction (Z), a service platform (16) being arranged in the service region (S), which service platform is or can be positioned in a service plane (E2) orthogonal to the vertical direction (Z). According to the invention, the upper tool (13) and the lower tool (15) each can be moved into at least one service position, and in the service positions the two tools (13, 15) are accessible from the common service platform (16) positioned in the service plane (E2).
B64F 5/10 - Fabrication ou assemblage d’aéronefs, p. ex. gabarits à cet effet
B66F 11/04 - Dispositifs de levage spécialement adaptés à des buts particuliers, non prévus ailleurs pour plates-formes ou cabines mobiles, p. ex. sur des véhicules, permettant à des ouvriers d'occuper toute position convenable pour exécuter les travaux demandés
B23Q 1/25 - Supports mobiles ou réglables d'outils ou de pièces
B21J 15/14 - Machines à riveter spécialement adaptées au rivetage de pièces déterminées, p. ex. machines pour poser les garnitures de frein
B25J 5/04 - Manipulateurs montés sur roues ou sur support mobile se déplaçant le long d'un chemin de guidage dans lequel le chemin de guidage est aussi mobile, p. ex. du type pont roulant
The disclosure relates to a processing station for aircraft structural components, having a gantry processing machine, a clamping frame for fastening at least one component, and a holding device assembly for receiving the clamping frame, wherein the gantry processing machine has a gantry and the gantry supports a processing tool which defines a processing point, wherein the processing tool is configured so as to be pivotable in relation to the gantry, and wherein the processing tool for displacing the processing point is height adjustable in the z direction in relation to the gantry, wherein the holding device assembly has at least two holding devices, and wherein at least one holding device has a drive for the height adjustment, and the clamping frame is height-adjustable in the z direction by means of the holding device.
The disclosure relates to an end effector for a riveting device, wherein the end effector includes a riveting module for placing a rivet element in a structural part, a rivet dispenser for dispensing rivet elements from a rivet magazine and a handling device for delivering a rivet element from the rivet dispenser to the riveting module The handling device includes an adjustment kinematics and a gripper arranged thereon for grabbing the rivet element. In some cases the adjustment kinematics has at least two adjustment axes for positioning the gripper.
B23P 19/00 - Machines effectuant simplement l'assemblage ou la séparation de pièces ou d'objets métalliques entre eux ou des pièces métalliques avec des pièces non métalliques, que cela entraîne ou non une certaine déformationOutils ou dispositifs à cet effet dans la mesure où ils ne sont pas prévus dans d'autres classes
B21J 15/14 - Machines à riveter spécialement adaptées au rivetage de pièces déterminées, p. ex. machines pour poser les garnitures de frein
The invention relates to a rivet element supply unit for providing rivet elements (5), wherein the rivet element supply unit (3) has a rivet element provision unit (6) and a handling unit (7), wherein to convey the rivet elements (5), the rivet element provision unit (6) has a spiral conveyor (8) with a longitudinal axis (2) and a spiral (9) that extends about the longitudinal axis (2), wherein the longitudinal axis (2) is inclined relative to the direction of gravity (G), wherein the rivet element provision unit (6) has a pick-up region (11) to which the spiral conveyor (8) feeds rivet elements (5) and from which the handling unit (7) picks up the rivet elements (5) for transportation to a rivet element receptacle (12).
B21J 15/32 - Dispositifs pour placer ou maintenir en position les rivets, avec ou sans systèmes d'alimentation
B23P 19/00 - Machines effectuant simplement l'assemblage ou la séparation de pièces ou d'objets métalliques entre eux ou des pièces métalliques avec des pièces non métalliques, que cela entraîne ou non une certaine déformationOutils ou dispositifs à cet effet dans la mesure où ils ne sont pas prévus dans d'autres classes
B21J 15/28 - Dispositifs de commande spécialement adaptés aux machines à riveter, non limités à l'un des sous-groupes précédents
B65G 47/14 - Dispositifs pour alimenter en objets ou matériaux les transporteurs pour alimenter en objets à partir de piles d'objets en désordre ou de tas d'objets en vrac disposant ou présentant les objets par des moyens mécaniques ou pneumatiques durant l'alimentation
45.
Method for producing a fiber metal laminate component of an airplane
A method for producing a Fiber Metal Laminate component of an airplane, using a manipulator system with an end effector and a control, wherein at least one metal layer and at least one unhardened fiber layer are being stacked onto each other in a mould in a stacking sequence, wherein each stacking cycle comprises picking up a metal layer or a fiber layer from a supply stack according to the stacking sequence, transporting the layer to the mould, placement of the layer at a deposition surface in the mould and depositing the so placed layer onto the deposition surface. After being picked up from the supply stack and before being deposited onto the deposition surface the layer to be stacked can be deformed by the end effector as to adapt the form of the layer to the form of the deposition surface.
B25J 15/06 - Têtes de préhension avec moyens de retenue magnétiques ou fonctionnant par succion
B29C 70/02 - Façonnage de matières composites, c.-à-d. de matières plastiques comprenant des renforcements, des matières de remplissage ou des parties préformées, p. ex. des inserts comprenant des combinaisons de renforcements et de matières de remplissage dans une matrice, formant une ou plusieurs couches, avec ou sans couches non renforcées ou non remplies
B29C 70/38 - Empilage automatisé, p. ex. utilisant des robots, par application de filaments selon des modèles prédéterminés
B29C 70/54 - Parties constitutives, détails ou accessoiresOpérations auxiliaires
B32B 15/14 - Produits stratifiés composés essentiellement de métal adjacent à une couche fibreuse ou filamenteuse
B32B 5/02 - Produits stratifiés caractérisés par l'hétérogénéité ou la structure physique d'une des couches caractérisés par les caractéristiques de structure d'une couche comprenant des fibres ou des filaments
B32B 15/04 - Produits stratifiés composés essentiellement de métal comprenant un métal comme seul composant ou comme composant principal d'une couche adjacente à une autre couche d'une substance spécifique
B32B 7/12 - Liaison entre couches utilisant des adhésifs interposés ou des matériaux interposés ayant des propriétés adhésives
B32B 38/18 - Manipulation des couches ou du stratifié
B32B 15/20 - Produits stratifiés composés essentiellement de métal comportant de l'aluminium ou du cuivre
B29C 31/08 - Alimentation, p. ex. chargement d'une cavité de moulage en préformes
B32B 1/00 - Produits stratifiés ayant une forme non plane
B32B 37/18 - Procédés ou dispositifs pour la stratification, p. ex. par polymérisation ou par liaison à l'aide d'ultrasons caractérisés par les propriétés des couches toutes les couches existant et présentant une cohésion avant la stratification impliquant uniquement l'assemblage de feuilles ou de panneaux individualisés
B29K 277/00 - Utilisation de polyamides, p. ex. polyesteramides, comme matière de renforcement
The invention relates to a method for supplying a riveting machine (2) with rivet elements (3), particularly during operation of the riveting machine (2), wherein at least one rivet element provision assembly (4) is provided having at least one rivet element provision unit (5) for providing and singling out the rivet elements (3), wherein the riveting machine (2) comprises a rivet element receiving arrangement (4) having at least one rivet element receiving unit (7) for receiving the rivet elements (3), wherein at least a portion of the transport from one of the rivet element provision units (5) to one of the rivet element receiving units (7) is robot-based.
The invention relates to a method for operating an end-effector arrangement (2) having an end effector (3) and a controller (4), wherein the end effector (3) has a tool arrangement (5) with a plurality of gripping devices (6) for gripping a flat workpiece (7) over the workpiece surface (7a) thereof, wherein the end effector can adopt different tool configurations, and wherein an adjusting arrangement (8) is provided, by means of which the tool configuration is adjustable and thus the relative position of the gripping devices (6) with respect to one another is adaptable to a target workpiece surface. It is proposed that the end effector (3) have a tactile arrangement (10) with a plurality of feelers (11) for producing tactile information, wherein the tactile information is created in a referencing operation and wherein the end effector (3) is adapted, with the gripping devices (6) thereof, to a reference surface (12) on the basis of the tactile information in the referencing operation, and that the resulting tool configuration be stored in the controller (4) as a reference tool configuration.
The invention relates to an application unit for the application of viscous material (4) to a component edge (5) of a component (6), varying in particular in the width (Βκ) and/or, wherein the application unit (3) has a nozzle (7) for applying the viscous material (4) to the component edge (4) having an outlet opening (8) that is adjustable in the width (BA), and wherein the application unit (3) has a first caliper (9) having a contact face (9a) for contact with the component (6), and a second caliper (10) having a contact face (10a) for contact with the component (6), wherein the first caliper (9) and the second caliper (10) can be preloaded in opposite directions (R1,R2) by a preloading arrangement (11), and wherein the width (BA) of the outlet opening (8) can be adapted, depending on the distance of the contact face (9a) of the first caliper (9) from the contact face (10a) of the second caliper (10).
B05C 5/02 - Appareillages dans lesquels un liquide ou autre matériau fluide est projeté, versé ou répandu sur la surface de l'ouvrage à partir d'un dispositif de sortie en contact, ou presque en contact, avec l'ouvrage
Various embodiments relate to a tool-clamping system having two metallic shaft portions, wherein the first shaft portion has a locking pin at the end and the second shaft portion has a locking sleeve at the end, wherein, in order to establish a releasable drive connection, the first shaft portion can be introduced coaxially, by way of its locking pin, into the locking sleeve of the second shaft portion and the two shaft portions can be pivoted in relation to one another, in a locking pivoting movement, about a common geometrical longitudinal axis into a locking pivot position, wherein, over the course of the locking pivoting movement, at least one latching formation arranged on the circumference of the locking pin, snap-fits or snap-fit over at least one corresponding mating latching formation of the locking sleeve, the locking pin and/or locking sleeve being elastically deformed in the process.
B23B 31/117 - Caractérisés par les dispositifs de maintien ou de serrage ou par leurs moyens d'action directe le maintien étant assurée uniquement par friction, p. ex. en utilisant des ressorts, des manchons élastiques, des cônes
B23Q 3/12 - Dispositifs permettant de maintenir, supporter ou positionner les pièces ou les outils, ces dispositifs pouvant normalement être démontés de la machine destinés à être fixés à une broche en général
B23Q 3/155 - Agencements pour insérer ou retirer automatiquement les outils
B23Q 3/157 - Agencements pour insérer ou retirer automatiquement les outils les outils rotatifs
Various embodiments relate to a method for motion simulation for a manipulator, such as an NC-controlled manipulator, in a machining environment, wherein the manipulator is moved in an operating mode by a control apparatus and the machining environment is at least partly mapped in an environment model and wherein the method comprises computation of a trajectory plan by the control apparatus from a setpoint movement of the manipulator starting from an initial situation and based on a kinematic model of the manipulator, performance of a kinematic collision check based on the trajectory plan, the kinematic model and the environment model, and production of a prediction result based on the kinematic collision check. The method is characterized in that the initial situation corresponds to the current manipulator state. Further, some embodiments relate to a corresponding computer program with program code and to a corresponding system for motion simulation for a manipulator.
The invention relates to an articulated robot having a serial kinematics unit (2) for the positioning of an end effector (3), wherein the kinematics unit (2) has at least one kinematics sub-unit (6, 7) with a robot joint (6.1), with a robot link (6.2) arranged upstream of the robot joint (6.1), and with a robot link (6.3) arranged downstream of the robot joint (6.1). It is proposed that the at least one kinematics sub-unit (6, 7), for the purpose of adjusting the robot links (6.2, 6.3) in relation to one another, should have a linear drive (6.4), with a drive element (6.6) which can be adjusted along a linear axis (6.5), and a coupling (6.7), with two coupling joints (6.8, 6.9) spaced apart from one another along the extent of the coupling, that the linear drive (6.4) should be arranged on a first robot link (6.10) of the kinematics sub-unit (6), and that the coupling (6.7) should be articulated, on one hand, to the drive element (6.6) of the linear drive (6.4) and, on the other hand, to the second robot link (6.11) of the kinematics sub-unit (6), at a distance from the geometrical axis (6.1a) of the robot joint (6.1) of the kinematics sub-unit (6).
B25J 9/04 - Manipulateurs à commande programmée caractérisés par le mouvement des bras, p. ex. du type à coordonnées cartésiennes par rotation d'au moins un bras en excluant le mouvement de la tête elle-même, p. ex. du type à coordonnées cylindriques ou polaires
B25J 9/10 - Manipulateurs à commande programmée caractérisés par des moyens pour régler la position des éléments manipulateurs
B25J 9/12 - Manipulateurs à commande programmée caractérisés par des moyens pour régler la position des éléments manipulateurs électriques
The invention relates to a spreading unit (1) having a shaper (2) for spreading viscous material (3), in particular sealing material, on a component (4), wherein the shaper (2) has a first shaping contour (5) for shaping the viscous material (3) during spreading, wherein at least a second shaping contour (6) of the shaper (2) can be brought to overlap with the first shaping contour (5) in a spreading direction (V) by means of an actuator (7) for shaping the viscous material (3), so that a shape of the shaper (2) can be adjusted during an application process.
B05C 5/02 - Appareillages dans lesquels un liquide ou autre matériau fluide est projeté, versé ou répandu sur la surface de l'ouvrage à partir d'un dispositif de sortie en contact, ou presque en contact, avec l'ouvrage
B05C 11/04 - Appareils pour étaler ou répartir des liquides ou d'autres matériaux fluides déjà appliqués sur une surfaceRéglage de l'épaisseur du revêtement comportant des lames
The invention relates to a device for applying a viscous material (3), comprising a bell (1) with a peripheral placement rim (8), and a feed line (2), wherein a delivery medium can be used to deliver the material (3) into the bell (1) through the feed line (2), wherein the bell (1) can be moved with the placement rim (8) in a placement direction to bring it over a projecting element (9), in particular a rivet head, of a component (9a) in order to encapsulate the element (9) with the material (3), wherein a metering member (12) is provided in the region of the bell (1) or the feed line (2), wherein a stream of the material can be influenced by means of the metering member (12) in the course of an application process.
B05C 11/10 - Stockage, débit ou réglage du liquide ou d'un autre matériau fluideRécupération de l'excès de liquide ou d'un autre matériau fluide
B05C 3/18 - Appareillages dans lesquels un ouvrage est mis en contact avec une grande quantité de liquide ou autre matériau fluide un côté uniquement de l'ouvrage venant en contact avec le liquide ou autre matériau fluide
B05C 3/109 - Appareillages dans lesquels un ouvrage est mis en contact avec une grande quantité de liquide ou autre matériau fluide l'ouvrage étant immergé dans le liquide ou autre matériau fluide pour traiter des objets individuels en faisant passer des liquides ou d'autres matériaux fluides dans, ou au travers, de chambres contenant des objets immobiles
The invention relates to an end effector assembly, comprising an end effector (2) for a manipulator (3) and comprising a controller (4) for the end effector (2), wherein the end effector (2) has a tool assembly (5) having a plurality of gripping device (6) for retaining a planar workpiece (7), wherein at least one gripping device (6) has a Bernoulli gripping unit (8), which has an outflow unit (9) for discharging a flow SB from the Bernoulli gripping unit (8) between the gripping device (6) and the workpiece (7) in such a way that the flow SB produces a negative pressure in a delimited region between the gripping device (6) and the workpiece (7) in order to retain the workpiece (7), and wherein at least one gripping device (6) has a gripping unit (10) of a different type, which gripping unit bears the workpiece (7) according to a different physical principle in comparison with the Bernoulli gripping unit (10). According to the invention, the controller (4) is designed to switch the end effector (2) between retention of the workpiece (7) by means of at least one Bernoulli gripping unit (8) and retention by means of at least one gripping unit (10) of a different type during the retention of the workpiece (7).
The invention relates to a gripping device for an end effector (2) of a manipulator (3) for retaining a workpiece (4) over the workpiece surface (5) of said workpiece, comprising a Bernoulli gripping unit (6), which has an outflow unit (7) for discharging a flow (SB) from the Bernoulli gripping unit (6) between the gripping device (1) and the workpiece surface (5) in such a way that a static negative pressure can be produced in a delimited region - the Bernoulli negative-pressure region (8) - by means of the flow (SB) in order to retain the workpiece (4), and comprising a vacuum gripping unit (9), which has a suction chamber (10), wherein a static negative pressure can be produced in a region delimited by the suction chamber (10) - the vacuum negative-pressure region (11) - in order to retain the workpiece (4), wherein the Bernoulli negative-pressure region (8) and the vacuum negative-pressure region (11) at least partially coincide or wherein the Bernoulli negative-pressure region (8) and the vacuum negative-pressure region (11) surround each other.
Various embodiments relate to a system for the production of fiber composite components, having at least a first fiber placement machine for the application of fiber layers to a workpiece, and a further processing station, distinct from the fiber placement machine, for the modification of the workpiece, wherein the workpiece can be brought both to the fiber placement machine and to the further processing station by means of an automated conveyor means. Various additional embodiments are also disclosed herein.
B29C 70/34 - Façonnage par empilage, c.-à-d. application de fibres, de bandes ou de feuilles larges sur un moule, un gabarit ou un noyauFaçonnage par pistolage, c.-à-d. pulvérisation de fibres sur un moule, un gabarit ou un noyau et façonnage ou imprégnation par compression
B29C 70/38 - Empilage automatisé, p. ex. utilisant des robots, par application de filaments selon des modèles prédéterminés
B29C 33/34 - Moules ou noyauxLeurs détails ou accessoires mobiles, p. ex. vers le, ou à partir du poste de moulage
Various embodiments relate to a fiber-laying machine for producing laid fiber scrims, including a tool table for feeding a workpiece along a feed direction; a laying head for applying fibers onto the workpiece; and a fiber-providing unit for feeding several fiber strands to the laying head; the several fiber strands are combined on the laying head to form a fiber web which is to be applied onto the workpiece; the laying head is movable in a laying direction relative to the fiber-providing unit; a clamping device is arranged on the laying head for releasably clamping the fiber strands, a portion of the fiber web is laid on the workpiece once the fiber strands have been pulled forward by a laying stroke by means of the laying head such that while the fibers are being applied on the workpiece, no fibers are pulled out of the fiber-providing unit.
The disclosure relates to a method for screwing a locking ring onto a threaded bolt, wherein a coupling device for being threaded into the threaded bolt is driven in rotation by a rotary drive, and wherein the locking ring is then screwed onto the threaded bolt, which is fixed by the coupling device, by a locking ring holder which is driven in rotation by the rotary drive. The disclosure likewise relates to a method for screwing a locking ring comprising a fastening part and a tear-off part onto a threaded bolt, wherein a removal gripper grips the tear-off part and removes the tear-off part after the tear-off part has been torn off. The disclosure further relates to a screwing apparatus for executing a method according to the disclosure.
B23P 19/06 - Machines pour mettre ou retirer les vis ou les écrous
B21J 15/14 - Machines à riveter spécialement adaptées au rivetage de pièces déterminées, p. ex. machines pour poser les garnitures de frein
F16B 31/02 - Assemblages à vis spécialement modifiés en vue de résister à une charge de tractionBoulons de rupture signalant ou limitant la charge de traction
B21J 15/32 - Dispositifs pour placer ou maintenir en position les rivets, avec ou sans systèmes d'alimentation
B21J 15/34 - Dispositifs pour placer ou maintenir en position les rivets, avec ou sans systèmes d'alimentation pour placer les rivets tubulaires
B23P 19/12 - Alignement de pièces pour leur insertion dans des orifices
B25B 21/00 - Outils portatifs à moteur pour serrer ou desserrer les vis ou les écrousAccessoires pour appareils à percer ayant les mêmes buts
59.
Method for compensating for a deviation in an operating point
Various embodiments relate to compensating for a deviation in an operating point of a manipulator during the processing of a workpiece. A command sequence is processed for controlling the manipulator, and a piece of setpoint position information is generated. The operating point is set based on the setpoint position information. The setpoint position information is processed using a compensation parameter set for ascertaining a compensation value. The setpoint position information is adjusted according to the compensation value for compensating for a deviation between an actual position of the operating point and the setpoint position. The actual position is measured during the processing of the workpiece. A correction value is ascertained, based on a comparison between the measured actual position and the setpoint position. The compensation parameter set is adjusted during the processing of the workpiece for reducing the deviation based on the correction value.
G05B 19/404 - Commande numérique [CN], c.-à-d. machines fonctionnant automatiquement, en particulier machines-outils, p. ex. dans un milieu de fabrication industriel, afin d'effectuer un positionnement, un mouvement ou des actions coordonnées au moyen de données d'un programme sous forme numérique caractérisée par des dispositions de commande pour la compensation, p. ex. pour le jeu, le dépassement, le décalage d'outil, l'usure d'outil, la température, les erreurs de construction de la machine, la charge, l'inertie
B23Q 15/18 - Compensation de la déformation de l'outil due à la température ou à l'effort
60.
Processing system for aircraft structural components
The disclosure relates to a processing installation for aircraft structural components having at least one processing station, wherein the processing station has a clamping frame which extends along a longitudinal station axis for receiving the aircraft structural component which is intended to be processed in each case and a processing unit, such as a riveting unit, for processing the aircraft structural component and wherein the clamping frame is articulated so as to be adjustable in terms of height and pivotable to two positioning towers which are arranged in a vertical tower plane. It is proposed that there be provided transversely relative to the tower plane a transverse offset of the clamping frame which enables an aircraft structural component to be loaded onto and/or unloaded from the clamping frame along the tower plane and at least one positioning tower to be passed laterally.
The invention relates to a method for filling a rivet cartridge (2) with rivet elements (3) using a rivet loading station (1) that includes a rivet supply unit (4) for supplying the rivet elements (3) and a rivet cartridge holder (5) for accepting a rivet cartridge (2); in said method, the rivet elements (3) are delivered from the rivet supply unit (4) to a rivet cartridge (2) accommodated in the rivet cartridge holder (5) and are accepted therein in an oriented manner. According to the invention, the rivet loading station (1) detects predefined properties of the rivet elements (3) before the rivet elements (3) are delivered to the rivet cartridge (2), said properties being relevant to the drilling process and/or the riveting process.
B21J 15/28 - Dispositifs de commande spécialement adaptés aux machines à riveter, non limités à l'un des sous-groupes précédents
B21J 15/32 - Dispositifs pour placer ou maintenir en position les rivets, avec ou sans systèmes d'alimentation
B23P 19/00 - Machines effectuant simplement l'assemblage ou la séparation de pièces ou d'objets métalliques entre eux ou des pièces métalliques avec des pièces non métalliques, que cela entraîne ou non une certaine déformationOutils ou dispositifs à cet effet dans la mesure où ils ne sont pas prévus dans d'autres classes
62.
METHOD FOR FILLING A RIVET CARTRIDGE WITH RIVET ELEMENTS
The invention relates to a method for filling a rivet cartridge (2) with rivet elements (3) using a rivet loading station (1) that includes a rivet supply unit (4) for supplying the rivet elements (3) and a rivet cartridge holder (5) for accepting a rivet cartridge (2); in said method, the rivet elements (3) are delivered from the rivet supply unit (4) to a rivet cartridge (2) accommodated in the rivet cartridge holder (5) and are accepted therein in an oriented manner. According to the invention, at least one section of the conveying path from the rivet supply unit (4) to the rivet cartridge (2) is robot-controlled.
B21J 15/28 - Dispositifs de commande spécialement adaptés aux machines à riveter, non limités à l'un des sous-groupes précédents
B21J 15/32 - Dispositifs pour placer ou maintenir en position les rivets, avec ou sans systèmes d'alimentation
B23P 19/00 - Machines effectuant simplement l'assemblage ou la séparation de pièces ou d'objets métalliques entre eux ou des pièces métalliques avec des pièces non métalliques, que cela entraîne ou non une certaine déformationOutils ou dispositifs à cet effet dans la mesure où ils ne sont pas prévus dans d'autres classes
B65G 47/14 - Dispositifs pour alimenter en objets ou matériaux les transporteurs pour alimenter en objets à partir de piles d'objets en désordre ou de tas d'objets en vrac disposant ou présentant les objets par des moyens mécaniques ou pneumatiques durant l'alimentation
A holding device for a test sheet includes a receiving arrangement for engagement with the test sheet, a handle arrangement connected rigidly to the receiving arrangement for a user for positioning the test sheet, and a pushbutton arrangement for producing a switching signal on the basis of an actuation by the user.
B25B 9/02 - Outils de serrage tenus à la main autres que ceux prévus au groupe sans connexions coulissantes ou pivotantes, p. ex. brucelles, pincettes de cheminées
F16P 3/18 - Commandes exigeant l'emploi des deux mains
B21J 15/42 - Dispositifs particuliers de serrage des pièces à riveter ensemble, p. ex. dispositifs travaillant au travers des trous de rivet
B21J 15/28 - Dispositifs de commande spécialement adaptés aux machines à riveter, non limités à l'un des sous-groupes précédents
The invention relates to a spreading unit (1) with a shaper (2) to spread viscous material (3), in particular sealing material, on a component (4), the shaper (2) having a shaper contour (5) for shaping the viscous material (3) during spreading. It is proposed that the shaper contour (5) of the shaper (2) is adjustable in an actuator-based manner for shaping the viscous material (3).
B05C 11/04 - Appareils pour étaler ou répartir des liquides ou d'autres matériaux fluides déjà appliqués sur une surfaceRéglage de l'épaisseur du revêtement comportant des lames
A manufacturing system for producing airplane structural components, including a drilling unit for producing bores in a material assembly made of at least two material plies for the purposes of inserting fastening elements and having a measuring unit for ascertaining geometry parameters for a previously produced bore. The measuring unit includes measuring electronics with an optical sensor element, a measuring optical unit and a measuring lance. The measuring unit produces an optical measurement beam that emerges from the measuring lance via the measuring optical unit and that is incident on a measurement point on the respective bore inner surface. A measurement movement between measuring lance and material assembly is provided in a measurement cycle and the measuring unit cyclically ascertains distance values to various measurement points at a scanning rate during the measurement movement and ascertains at least one geometry parameter for the respective bore from the distance values.
G01B 11/24 - Dispositions pour la mesure caractérisées par l'utilisation de techniques optiques pour mesurer des contours ou des courbes
B21J 15/28 - Dispositifs de commande spécialement adaptés aux machines à riveter, non limités à l'un des sous-groupes précédents
B23B 49/00 - Systèmes de mesure ou de calibrage des machines à aléser, pour le positionnement ou le guidage du foretDispositif pour indiquer les défauts des forets pendant l'alésageDispositifs à centrer les trous à aléser
G01B 11/08 - Dispositions pour la mesure caractérisées par l'utilisation de techniques optiques pour mesurer des diamètres
B23Q 17/24 - Agencements sur les machines-outils pour indiquer ou mesurer utilisant des moyens optiques
G01B 9/023 - Interféromètres utilisant des techniques holographiques pour produire des contours
B21J 15/14 - Machines à riveter spécialement adaptées au rivetage de pièces déterminées, p. ex. machines pour poser les garnitures de frein
The invention relates to an end effector for a riveting device (1). The end effector (2) has a riveting module (3) for introducing a rivet element (4) into a component (5), a rivet discharge (6) for discharging rivet elements (4) out of a rivet store (7), and a handling device (8) for transporting a rivet element (4) from the rivet discharge (6) to the riveting module (3). The handling device (8) has adjustment kinematics (9) and a gripper (10) arranged thereon for gripping the rivet element (1). According to the invention, the adjustment kinematics have at least two adjustment axes (A1, A2, A3, A4, A5, A6, A7) in order to position the gripper (10).
common metals and their alloys, unwrought or semi-unwrought; non-electric cables and wires of common metal; pipes and tubes of metal; goods of common metal namely, metal molds for forming and laying fiber tapes and fibers for building airplanes; metal rails; metal chains, not being driving chains for vehicles; metal pipes and tubes for use in aircraft, not being structural parts machine tools of common metal, namely, jigs being clamps for mounting airplane parts on machine tables for building airplanes; machines, namely, drilling machines, fastening machines, riveting machines, and tape laying and fiber placement machines; machines for manufacturing and assembling airplane parts, especially structural airplane parts; machines for manufacturing fiber-reinforced airplane parts; machines for curing fiber-reinforced airplane parts; machines for treating cutting, coating, and forming fibers used in the construction of airplanes; machines for manufacturing fiber-composite airplane parts; machines for treating and applying glues and sealants for use in airplane construction; industrial robots for drilling, fastening, riveting, tape laying, and fiber placing; industrial robots for manufacturing and assembling airplane parts, especially structural airplane parts; industrial robots for manufacturing and curing fiber-reinforced airplane parts; preforming machines, namely, machines for treating and curing fibers used in the construction of fiber-composite airplane parts; metalworking machines, namely, bending machines, boring machines, and cutting machines; die-cutting and tapping machines; drilling machines; electric welding machines; fastening machines, namely, riveting machines for attachment to industrial robots; gas-operated soldering apparatus; spraying machines; automatic handling machines, namely, material handling machines in the nature of palletizers, case elevators, automatic pallet dispensing, and automatic slip sheet dispensing machines; industrial robots for fiber treatment, fiber cutting, fiber coating, and fiber forming; industrial robots for applying glues and sealants; industrial robots for treating glues and sealants; machines for positioning, joining, assembling, and manufacturing automobile, aircraft, and wind energy generation parts and components; cranes; machines, namely, elevating or lifting work platforms; handling machines, namely, loading and unloading machines; end effectors, namely, machines for assembling airplane parts for attachment to industrial robots; drilling, punching, and riveting machines; machine tools, namely, work holding fixtures for precision machining applications; motors, other than for land vehicles; drives, namely, rotary belt drives for machines for manufacturing and assembling airplane parts; hydraulic controls for agricultural aircraft motors and engines; machine couplings and transmission components except for land vehicles; drive belts, except for land vehicles
The disclosure relates to a method for checking a rivet, the rivet being transported from a rivet filling station along a transporting path in the direction of a riveting machine during operation of the riveting machine. The method is characterized in that the rivet is measured on the transporting path for determining a rivet geometry of the rivet. The disclosure similarly relates to a corresponding measuring arrangement for checking a rivet.
The invention relates to a processing station for aircraft structural components, comprising a portal processing machine (3), a clamping frame (4) for fastening at least one component (2), and a holding device arrangement (5) for receiving the clamping frame (4). The portal processing machine (3) has a portal (6), said portal supporting a processing tool (7) that defines a processing point (P). The processing tool (7) is designed such that the processing tool is pivotable with respect to the portal (6), wherein the processing tool (7) is height-adjustable with respect to the portal (6) for displacing the processing point (P) in a z-direction. The holding device arrangement (5) has at least two holding devices (8), wherein at least one holding device (8) has a drive (9) for height adjustment, and the clamping frame (4) is height-adjustable in the z-direction by means of the holding device (8).
B23Q 1/01 - Bâtis, bancs, colonnes ou éléments similairesAgencement des glissières de guidage
B21J 15/14 - Machines à riveter spécialement adaptées au rivetage de pièces déterminées, p. ex. machines pour poser les garnitures de frein
B64F 5/00 - Tracé, fabrication, assemblage, nettoyage, entretien ou réparation des aéronefs, non prévus ailleursManipulation, transport, test ou inspection de composants d’aéronefs, non prévus ailleurs
A method for operating an automation arrangement, having a manipulator and an input/output module for automated production and also a computer apparatus uses the computer apparatus to execute a PLC computer program for providing a programmable logic controller for the input/output module, which PLC computer program is communitively connected to the input/output module via a module bus for the purpose of actuating said input/output module. The method is characterized in that the computer apparatus is used to execute a cell control computer program for actuating the PLC computer program via a PLC interface of the PLC computer program, in that the cell control computer program provides an NC controller for the manipulator and in that the cell-control computer program is communicatively connected to the manipulator via a network bus for the purpose of actuating said manipulator.
G05B 19/414 - Structure du système de commande, p. ex. automate commun ou systèmes à multiprocesseur, interface vers le servo-contrôleur, contrôleur à interface programmable
G05B 19/05 - Automates à logique programmables, p. ex. simulant les interconnexions logiques de signaux d'après des diagrammes en échelle ou des organigrammes
The disclosure relates to an apparatus for the production of parisons from fiber-reinforced plastic, having a feed arrangement for the continuous feed of a laid fiber fabric and having a transverse deformation arrangement with a draping apparatus for the deformation of the fed laid fiber fabric to form a predefined nominal profile. The apparatus is distinguished by the fact that the draping apparatus is adjustable for a variation of a cross section of the nominal profile. The disclosure also relates to a corresponding method for the production of parisons from fiber-reinforced plastic.
B29K 105/08 - Présentation, forme ou état de la matière moulée contenant des agents de renforcement, charges ou inserts de grande longueur, p. ex. ficelles, mèches, mats, tissus ou fils
72.
METHOD FOR PRODUCING A FIBER LAMINATE COMPONENT OF AN AIRPLANE
The invention is directed to a method for producing a Fiber Metal Laminate component of an airplane, using a manipulator system (1) with an end effector (3) and a control (4) assigned to the manipulator system (2), wherein at least one metal layer (5) and at least one unhardened fiber layer (6) are being stacked onto each other in a mould (7) by the manipulator system (2) in a stacking sequence, wherein each stacking cycle comprises picking up a metal layer (5) or a fiber layer (6) from a respective supply stack (8, 9) according to the stacking sequence, transporting the layer (5, 6) to the mould (7), placement of the layer (5, 6) at a deposition surface in the mould (7) according to the stacking sequence and depositing the so placed layer (5, 6) onto the deposition surface (10). It is proposed that after being picked up from the supply stack (8, 9) and before being deposited onto the deposition surface (10) the layer (5, 6) to be stacked is being deformed by the end effector (3) as to adapt the form of the layer (5, 6) to the form of the deposition surface (10).
The invention relates to a tool clamping system (2) having two metal shaft portions (3, 4), wherein the first shaft portion (3) has a locking pin (5) at its end and the second shaft portion (4) has a locking sleeve (6) at its end, wherein, in order to produce a releasable drive-related connection, the first shaft portion (3) is able to be introduced coaxially with its locking pin (5) into the locking sleeve (6) of the second shaft portion (4), and the two shaft portions (3, 4) are pivotable with respect to one another into a locking pivoted position by way of a locking pivoting movement (7) about a common geometric longitudinal axis (8), wherein at least one latching formation (9a-c) arranged on the circumference of the locking pin (5), preferably at least three latching formations (9a-c) distributed around the circumference of the locking pin (5), snaps or snap over at least one corresponding mating latching formation (10a-c) on the locking sleeve (6), preferably over at least three corresponding mating latching formations (10a-c) on the locking sleeve (6), during the locking pivoting movement, with elastic deformation of the locking pin (5) and/or locking sleeve (6).
B23B 31/117 - Caractérisés par les dispositifs de maintien ou de serrage ou par leurs moyens d'action directe le maintien étant assurée uniquement par friction, p. ex. en utilisant des ressorts, des manchons élastiques, des cônes
B23Q 3/12 - Dispositifs permettant de maintenir, supporter ou positionner les pièces ou les outils, ces dispositifs pouvant normalement être démontés de la machine destinés à être fixés à une broche en général
B23Q 3/155 - Agencements pour insérer ou retirer automatiquement les outils
B23Q 3/157 - Agencements pour insérer ou retirer automatiquement les outils les outils rotatifs
B23B 31/00 - Mandrins de serrageMandrins extensiblesLeurs adaptations à la commande à distance
74.
MACHINING SYSTEM FOR AIRCRAFT STRUCTURAL COMPONENTS
The invention relates to a machining system for aircraft structural components, comprising a first frame (1) for holding a work piece, and a second frame (7) for holding a tool pair (8), comprising an upper tool (9) and a lower tool (10) cooperating therewith, wherein the workpiece is positioned between the upper tool (9) and the lower tool (10), wherein the second frame (7) is designed for displacement at least in a longitudinal direction (L) with respect to a base, and wherein the tool pair (8) is accommodated in the second frame (7) for displacement in a transverse direction (Q) angled with respect to the longitudinal direction (L), wherein the second frame (7) is accommodated on at least one pivot bearing (16) so the second frame (7) can be pivoted together with the tool pair (8) in an adjustable manner about a pivot axis (B).
B21J 15/14 - Machines à riveter spécialement adaptées au rivetage de pièces déterminées, p. ex. machines pour poser les garnitures de frein
B64F 5/00 - Tracé, fabrication, assemblage, nettoyage, entretien ou réparation des aéronefs, non prévus ailleursManipulation, transport, test ou inspection de composants d’aéronefs, non prévus ailleurs
75.
FIBER-LAYING MACHINE AND METHOD FOR LAYING A FIBROUS WEB ONTO A WORKPIECE
The invention relates to a fiber-laying machine (2) and a method for the production of laid fiber scrims, comprising a tool table (23) for feeding a workpiece (12) along a feed direction (x); a laying head (26) for the application of fibers (13) onto the workpiece (12); and a fiber provision unit (42) for feeding a plurality of fiber strands (13) to the laying head (26); wherein the plurality of fiber strands (13) are combined at the laying head (26) to form a fibrous web that is to be applied onto the workpiece (12); wherein the laying head (26) is movable in a laying direction (y) relative to the fiber provision unit (42); wherein a clamping device (111) for detachable clamping of the fiber strands (13) is arranged on the laying head (26), wherein a laying of a portion of the fibrous web (13) on the workpiece (12) is carried out after the fiber strands (13) have been pulled forward by the laying head (26) by a laying stroke, so that no fibers (13) are pulled from the fiber provision unit (42) during the application of the fibers (13) onto the workpiece (12).
The invention relates to a system for manufacturing fibre composite components, comprising at least one first fibre laying machine (2) for applying fibre scrims to a workpiece (12); and one additional processing station for modifying the workpiece, which is different from said fibre laying machine (2), the workpiece (12) being able to be brought to both the fibre laying machine (2) and the additional processing station by means of an automatic conveyor device (4, 5).
B29C 70/38 - Empilage automatisé, p. ex. utilisant des robots, par application de filaments selon des modèles prédéterminés
B29C 70/34 - Façonnage par empilage, c.-à-d. application de fibres, de bandes ou de feuilles larges sur un moule, un gabarit ou un noyauFaçonnage par pistolage, c.-à-d. pulvérisation de fibres sur un moule, un gabarit ou un noyau et façonnage ou imprégnation par compression
B29C 33/34 - Moules ou noyauxLeurs détails ou accessoires mobiles, p. ex. vers le, ou à partir du poste de moulage
77.
METHOD FOR COMPENSATING FOR A DEVIATION OF AN OPERATING POINT
The invention relates to a method for compensating for a deviation of an operating point (1) of a manipulator (2) during the machining of a workpiece (3) by an end-effector (4) on the manipulator (2), wherein an instruction sequence for controlling the manipulator (2) for the purpose of machining the workpiece (3) is executed and, based on the instruction sequence, target position information (5) corresponding to a target position (6) is generated, on the basis of which target position information (5) the operating point (1) of the manipulator (2) is adjusted, wherein the target position information (5) is processed using a set of compensation parameters (7) relating to the target position information (5) to determine a compensation value (8), and the target position information (5) is adapted according to the compensation value (8) to compensate for a deviation (9) between an actual position (10) of the operating point (1) and the target position (6). The invention is characterized in that the actual position (10) is measured during the machining of the workpiece (3), in that a correction value (12) is determined based on a comparison between the measured actual position (10) and the target position (6), and in that the set of compensation parameters (7) is adapted, based on the correction value (12), during the machining of the workpiece (3) to reduce the deviation (9).
G05B 19/404 - Commande numérique [CN], c.-à-d. machines fonctionnant automatiquement, en particulier machines-outils, p. ex. dans un milieu de fabrication industriel, afin d'effectuer un positionnement, un mouvement ou des actions coordonnées au moyen de données d'un programme sous forme numérique caractérisée par des dispositions de commande pour la compensation, p. ex. pour le jeu, le dépassement, le décalage d'outil, l'usure d'outil, la température, les erreurs de construction de la machine, la charge, l'inertie
B23Q 15/18 - Compensation de la déformation de l'outil due à la température ou à l'effort
The invention relates to a method for motion simulation of a manipulator (1a,b), preferably a NC-controlled manipulator (1a,b), in a processing environment (3a,b), wherein the manipulator (1a,b) is moved in a working operation by a control device (10) and the processing environment (3a,b) is at least partially mapped in a model of the environment, said method comprising the steps of calculating a path planning (12a,b) by the control device (10) from a desired movement of the manipulator (1a,b) starting from an initial position (11a,b) and on the basis of a kinematic model of the manipulator (1a,b), carrying out a kinematic collision test on the basis of the path planning (12a,b), the kinematic model and the model of the environment, and generating a prediction result on the basis of the kinematic collision test. The method is characterized in that the initial position (11a,b) corresponds to the current state of the manipulator. The invention further relates to a corresponding computer program having a program code and to a corresponding system for motion simulation of a manipulator (1a,b).
The invention relates to a holding device for a test sheet (1), comprising a receiving arrangement (2) for engagement with the test sheet (1), a handle arrangement (3) for a user, which is rigidly connected to the receiving arrangement (2), for positioning the test sheet (1), as well as a sensor arrangement (5) for generating a switching signal on the basis of an actuation by the user (4).
F16P 3/18 - Commandes exigeant l'emploi des deux mains
B21D 5/02 - Cintrage des tôles le long de lignes droites, p. ex. pour former un pli simple sur des presses particulières sans fixation de la pièce
B21D 43/00 - Dispositifs d'alimentation, de positionnement ou de stockage combinés à des appareils pour travailler ou traiter les tôles, les tubes ou les profilés, disposés dans ces appareils ou spécialement adaptés pour être utilisés en association avec ces appareilsAssociation de dispositifs de coupe avec ces appareils
B21D 55/00 - Dispositifs de sécurité protégeant la machine ou l'opérateur, spécialement adaptés aux appareils ou machines couverts par la présente sous-classe
B25B 9/02 - Outils de serrage tenus à la main autres que ceux prévus au groupe sans connexions coulissantes ou pivotantes, p. ex. brucelles, pincettes de cheminées
B23Q 7/04 - Agencements pour la manipulation des pièces, spécialement combinés aux machines-outils ou disposés dans ces machines ou spécialement conçus pour être utilisés en relation avec ces machines, p. ex. pour le transport, le chargement, le positionnement, le déchargement, le triage au moyen de pinces
The invention relates to a processing system for aircraft structural components (2), comprising at least one processing station (3, 4) wherein the processing station (3, 4) has a clamping frame (7, 8), extending along a longitudinal axis (5, 6) of the station, for receiving the respective aircraft structural component (2) to be processed, and a processing unit (9, 10), preferably a riveting unit, for processing the aircraft structural component (2), and wherein the clamping frame (7, 8) is connected to two positioning towers (11, 12), arranged in a vertical tower plane (13), in a height-adjustable and swivelable manner. According to the invention, a transverse offsetting of the clamping frame (7, 8) is provided in a transverse direction in relation to the tower plane (13), permitting a loading and/or unloading of an aircraft structural component (2) into/from the clamping frame (7, 8) to be carried out along the tower plane (13), and to laterally pass by at at least one positioning tower (11, 12).
B21J 15/14 - Machines à riveter spécialement adaptées au rivetage de pièces déterminées, p. ex. machines pour poser les garnitures de frein
B64F 5/00 - Tracé, fabrication, assemblage, nettoyage, entretien ou réparation des aéronefs, non prévus ailleursManipulation, transport, test ou inspection de composants d’aéronefs, non prévus ailleurs
81.
METHOD FOR SCREWING A LOCKING RING ONTO A THREADED BOLT
The invention relates to a method for screwing a locking ring (1) onto a threaded bolt (2), wherein a coupling device (6) for threading into the threaded bolt (2) is rotatably driven by a rotary drive (4) and wherein the locking ring (1) is then screwed by a locking ring holder (3) that is rotatably driven by the rotary drive (4) onto the threaded bolt (2) fixed by the coupling device (6). The invention likewise relates to a method for screwing a locking ring (1) comprising a fastening part (18a) and a tear-off part (18b) onto a threaded bolt (2), wherein a removal gripper (22) grips the tear-off part (18b) after the tear-off part (18b) is torn off and removes the tear-off part (18b). The invention further relates to a screwing device for carrying out a method according to the invention.
B21J 15/14 - Machines à riveter spécialement adaptées au rivetage de pièces déterminées, p. ex. machines pour poser les garnitures de frein
B21J 15/32 - Dispositifs pour placer ou maintenir en position les rivets, avec ou sans systèmes d'alimentation
B21J 15/34 - Dispositifs pour placer ou maintenir en position les rivets, avec ou sans systèmes d'alimentation pour placer les rivets tubulaires
B23P 19/06 - Machines pour mettre ou retirer les vis ou les écrous
F16B 31/02 - Assemblages à vis spécialement modifiés en vue de résister à une charge de tractionBoulons de rupture signalant ou limitant la charge de traction
The invention relates to a production system for producing aircraft structural components, comprising a boring unit (2) for producing bores (3) in a material packet (4) consisting of at least two material layers (4a, 4b) for inserting securing elements, in particular rivet elements, and comprising a measuring unit (5) for ascertaining geometric parameters for a previously produced bore (3). The measuring unit (5) has an electronic measuring system (6) with an optical sensor element (7), an optical measuring system (8), and a measuring lance (9); the measuring unit (5) generates an optical measuring beam (13) in order to ascertain a distance (10) between the measuring lance (9) and a measuring point (11) on the respective bore inner surface (12), said optical measuring beam exiting the measuring lance (9) via the optical measuring system (8) and striking the measuring point (11) on the respective bore inner surface (12); a measuring movement is produced between the measuring lance (9) and the material packet (4) during a measurement cycle; and the measuring unit (5) cyclically ascertains distance values at different measuring points (11) at a sampling rate during the measuring movement, and at least one geometric parameter for the respective bore (3) is ascertained from the distance values.
G01B 9/023 - Interféromètres utilisant des techniques holographiques pour produire des contours
B23Q 17/24 - Agencements sur les machines-outils pour indiquer ou mesurer utilisant des moyens optiques
B23Q 17/20 - Agencements sur les machines-outils pour indiquer ou mesurer pour indiquer ou mesurer les caractéristiques de la pièce, p. ex. contour, dimensions, dureté
G01B 11/24 - Dispositions pour la mesure caractérisées par l'utilisation de techniques optiques pour mesurer des contours ou des courbes
The invention relates to a method for checking a rivet (1), wherein the rivet (1) is conveyed from a rivet-filling station (2) along a transport path (3) in the direction of a riveting machine (4) during an operation of the riveting machine (4). The method is characterized in that the rivet (1) is measured on the transport path (3) to determine a geometry of the rivet (1). The invention also relates to a corresponding measuring arrangement for checking a rivet (1).
B21J 15/28 - Dispositifs de commande spécialement adaptés aux machines à riveter, non limités à l'un des sous-groupes précédents
B05C 7/04 - Appareillages spécialement agencés pour appliquer un liquide ou autre matériau fluide à l'intérieur d'une pièce creuse le liquide ou autre matériau fluide s'écoulant ou étant entraîné à travers l'ouvrageAppareillages spécialement agencés pour appliquer un liquide ou autre matériau fluide à l'intérieur d'une pièce creuse l'ouvrage étant rempli de liquide ou autre matériau fluide puis vidé
B21J 15/32 - Dispositifs pour placer ou maintenir en position les rivets, avec ou sans systèmes d'alimentation
G01N 21/952 - Inspection de la surface extérieure de corps cylindriques ou de fils
The invention relates to a method for operating an automation arrangement (1), preferably an automation cell (la), comprising a manipulator (2a, b) and an input/output module (3a, b) for automated production and a computer device (5), wherein a PLC computer program (6) is configured on the computer device (5) for providing programmable logic control for the input/output module (3a, b), said PLC computer program (6) having a communication connection with the input/output module (3a, b) via a module bus (7) for controlling said input/output module (3a, b). The method is characterized in that a cell control computer program (8) is configured on the computer device (5) for controlling the PLC computer program (6) via a PLC interface (9) of the PLC computer program (6), that the cell control computer program (8) provides an NC control (10) for the manipulator (2a, b), and that the cell control computer program (8) has a communication connection with the manipulator (2a, b) via a network bus (11) for controlling said manipulator (2a, b).
G05B 19/414 - Structure du système de commande, p. ex. automate commun ou systèmes à multiprocesseur, interface vers le servo-contrôleur, contrôleur à interface programmable
The invention relates to an apparatus for producing fiber-reinforced plastic preforms, comprising a feeding arrangement (1) for continuously feeding a non-crimp fabric (2), and a transverse shaping arrangement (3) that includes a draping device (4) for shaping the fed non-crimp fabric (2) into a predefined desired profiled element (5). The apparatus is characterized in that the draping device (4) can be adjusted so as to be able to modify a cross-section of the desired profiled element (5). The invention further relates to a corresponding method for producing fiber-reinforced plastic preforms.
A fibre-laying machine (2) for producing laid fibre scrims has a tool table (23) for positioning a forming tool (12), said tool table (23) being movable linearly in an x direction by means of an x carriage (21) and being pivotable about a vertical pivot axis (25). Arranged above the tool table (23) is a fibre-laying head (26) which is movable linearly and transversely to the x direction by means of a y carriage (28). Since the fibre-laying head (26) is linearly movable, the arrangement of the tool table (23) on the machine frame (15) is comparatively easy, and so laid fibre scrims are producible quickly and efficiently. In particular, automatic loading and unloading of the tool table (23) is easily possible.
The invention relates to a centring arrangement for a component carrier, in particular for a mounting frame for structural aircraft components, having a centring pin, a centring receptacle for the centring pin, and a rotary drive for rotating the centring pin about a longitudinal axis of the centring pin, so that the centring pin can be brought into centring engagement with the centring receptacle as a result of the rotation. The invention further relates to a method for centring and locking a centring receptacle.
B64F 5/00 - Tracé, fabrication, assemblage, nettoyage, entretien ou réparation des aéronefs, non prévus ailleursManipulation, transport, test ou inspection de composants d’aéronefs, non prévus ailleurs
B23Q 1/25 - Supports mobiles ou réglables d'outils ou de pièces
B23Q 1/01 - Bâtis, bancs, colonnes ou éléments similairesAgencement des glissières de guidage
B23Q 3/18 - Dispositifs permettant de maintenir, supporter ou positionner les pièces ou les outils, ces dispositifs pouvant normalement être démontés de la machine pour positionner uniquement
The invention relates to an end effector for a manipulator, wherein the end effector interacts with a workpiece, wherein at least one carrier, configured in particular as a carrier plate, for a tool arrangement is provided, and wherein the tool arrangement serves to interact with the workpiece. It is proposed that the carrier is formed at least in part from a deformable material, in particular from an elastically deformable material, and that the carrier is assigned an actuating arrangement, by way of which the carrier is deformable and thus the tool arrangement is orientable in space.
In a method and apparatus for producing fiber composite material components, a first web of the fiber composite material is applied to a mold by means of an application tool arranged on a positioning device. A height profile of the applied first web is measured by means of a height profile measuring sensor. During the application of a second web of the fiber composite material to the mold, a control device activates at least one drive motor of the positioning device depending on the measured height profile, so that application errors, such as overlapping of the webs, are avoided. The webs are applied in opposite application directions by rotating the application tool 180° relative to the positioning device upon a change in the application direction. Two height profile measuring sensors arranged next to one another on the application tool for measuring the height profile of the applied webs.
09 - Appareils et instruments scientifiques et électriques
35 - Publicité; Affaires commerciales
37 - Services de construction; extraction minière; installation et réparation
41 - Éducation, divertissements, activités sportives et culturelles
Produits et services
Installations for the manufacture and transport of aircraft. Computer software and computer programs relating to installations for the manufacture and transport of aircraft. Business management consultancy relating to strategy, marketing, production, personnel and logistics for manufacturing companies; Outsourcing services, in particular outsourcing services relating to production and logistics processes. Construction; Repair; Installation services; Including repair and maintenance of installations for the manufacture and transport of aircraft; Installation optimisation relating to installations for the manufacture and transport of aircraft. Providing of training, conferences, preparation of teaching material, all in the fields of design, certification, operation, maintenance, repair, inspection and production of installations for the manufacture and transport of aircraft, and in the field of logistics.
91.
Production system for producing fibre composite material components
Deutsches Zentrum Fur Luft—Und Raumfahrt E.V. (Allemagne)
Broetje-Automation GmbH (Allemagne)
Inventeur(s)
Boge, Christian
Pause, Bernhard
Meyer, Matthias
Röstermundt, Dirk
Abrégé
To produce a fiber composite material component, a production system has a mold providing unit with at least one component mold. Fiber composite material can be applied to the at least one component mold by means of at least two production units. The at least two production units can be moved for this purpose on a guide path. The guide path runs round the mold providing unit so that the at least two production units can travel round the mold providing unit along the guide path. The productivity and flexibility of production can thereby be increased.
The invention relates to an operating method for a positioning system 1, in particular for the structural assembly of aircraft, wherein the positioning system 1 comprises a plurality of positioners 2a, 2b, 2c, each of which has at least one manipulator M. The manipulators M grasp a component B and manipulate it in a synchronised manner, while it is jointly grasped by the manipulators M.
B64F 5/10 - Fabrication ou assemblage d’aéronefs, p. ex. gabarits à cet effet
B64F 5/50 - Manipulation ou transport des composants d'aéronefs
B23P 21/00 - Machines pour l'assemblage de nombreuses pièces différentes destinées à composer des ensembles, avec ou sans usinage de ces pièces avant ou après leur assemblage, p. ex. à commande programmée
93.
Device for providing and controlling motion of connection elements
A connection elements control for motion control of connection elements such as rivet elements or the like has at least one control unit with connection elements channel through which the connection elements are pushed, possibly by a fluid flow, the connection elements channel having an inlet section and an outlet section, and a control shaft extending through at least a portion of the connection elements channel in a control region between the sections, and the system is designed such that the passage of the connection elements and/or fluid through control region is controlled by swiveling control shaft.
B21J 15/28 - Dispositifs de commande spécialement adaptés aux machines à riveter, non limités à l'un des sous-groupes précédents
B21J 15/32 - Dispositifs pour placer ou maintenir en position les rivets, avec ou sans systèmes d'alimentation
B21J 15/26 - Entraînements pour machines à riveterMoyens de transmission correspondants actionnés par un entraînement rotatif, p. ex. par des moteurs électriques
B23P 19/00 - Machines effectuant simplement l'assemblage ou la séparation de pièces ou d'objets métalliques entre eux ou des pièces métalliques avec des pièces non métalliques, que cela entraîne ou non une certaine déformationOutils ou dispositifs à cet effet dans la mesure où ils ne sont pas prévus dans d'autres classes
A device for providing connection elements, such as rivets and the like has a storage unit with at least one outlet, two stacked, replaceable cartridges each having at least one output flange for dispensing connection elements, and a cartridge guide and a detachable cartridge lock assigned to each cartridge which for its installation is slideable via the cartridge guide to an operating position and fixable by the cartridge lock assigned to the cartridge guide and engaged with the cartridge for locking.
In a method for the offline programming of an NC-controlled manipulator which follows at least one real trajectory, possibly in a sensor-supported manner, with tool center point thereof in the real working mode, a kinematic manipulator model and, possibly, an environmental model are stored in an offline programming environment with user interface, at least one virtual trajectory of the manipulator and a virtual tolerance zone assigned to said trajectory are defined using the offline programming environment in a definition routine, and the offline programming environment is used to check, in a check routine, the previously defined tolerance zone at least in part in terms of kinematic singularities of the manipulator, the occurrence of which prompts a singularity routine to be executed.
A method is used for controlling a paced production line for processing airplane structural components, wherein the production line comprises at least one workstation having at least one processing machine. It is provided that the processing sequence in the workstation is determined for a production step by determining the expected or actual occupation of the working area by structural component(s) or structural component section(s) for the production step, and, on the basis of the occupation, all of the operations to be performed in this workstation in this production step are determined, and the processing sequence of these operations is optimized.
G06F 19/00 - Équipement ou méthodes de traitement de données ou de calcul numérique, spécialement adaptés à des applications spécifiques (spécialement adaptés à des fonctions spécifiques G06F 17/00;systèmes ou méthodes de traitement de données spécialement adaptés à des fins administratives, commerciales, financières, de gestion, de surveillance ou de prévision G06Q;informatique médicale G16H)
G05B 13/02 - Systèmes de commande adaptatifs, c.-à-d. systèmes se réglant eux-mêmes automatiquement pour obtenir un rendement optimal suivant un critère prédéterminé électriques
B23P 11/00 - Assemblage ou désassemblage de pièces ou d'objets métalliques par des processus du travail du métal non prévus ailleurs
97.
Method and device for manufacturing preforms of fiber reinforced plastic
In a device and method for manufacturing preforms of fiber reinforced plastic, in a first step, continuously supplied fiber layers are laterally reshaped in a predetermined manner, and the section that is obtained is curved longitudinally in a specific manner in a second step.
B29C 70/50 - Façonnage ou imprégnation par compression pour la fabrication d'objets de longueur indéfinie, p. ex. de "prepregs", de préimprégnés [SMC] ou de nappes multiaxiales [XMC]
B29B 11/16 - Fabrication de préformes caractérisées par la structure ou la composition comprenant des charges ou des agents de renforcement
A receptacle for receiving fastening elements for connection of two components of a unit to be assembled, the receptacle has means for providing a separate reception of different fastening elements which differ from one another with regard to a shape, and/or a size, and/or a material, such that different ones of the fastening elements with which the receptacle is charged are coordinated with the components which are respectively to be connected, and a number of the fastening elements to be received by the receptacle corresponds at least to a number of connection sites on the components.
B65D 85/24 - Réceptacles, éléments d'emballage ou paquets spécialement adaptés à des objets ou à des matériaux particuliers pour objets incompressibles ou rigides en forme de baguette ou tubulaires pour aiguilles, clous ou petits objets de forme allongée similaires
B65D 25/10 - Dispositifs pour placer les objets dans les réceptacles
A system for identification of different fastening elements used for connecting of components of a unit to be assembled has a receptacle to receive different fastening elements which differ from each other with regard to shape and/or size and/or material and are coordinated to the components which are respectively to be connected so that the number of fastening elements which are able to be received by the receptacle corresponds at least to the number of connection sites on the components, a housing which serves to receive the receptacle, and identification elements to display the individual charging position of a fastening element in the receptacle.
For manufacture of fiber-reinforced components, a positionable base frame is used on which a controllable holding device is provided for gripping and holding at least one reinforced fiber layer. A draping device is provided on the base frame, using which the reinforced fiber layer may be draped onto a mold core via the application of a vacuum.
