B21D 39/04 - Utilisation de procédés permettant d'assembler des objets ou des parties d'objets, p. ex. revêtement par des tôles, autrement que par placageDispositifs de mandrinage des tubes des tubes avec des tubesUtilisation de procédés permettant d'assembler des objets ou des parties d'objets, p. ex. revêtement par des tôles, autrement que par placageDispositifs de mandrinage des tubes des tubes avec des barres
C08L 63/00 - Compositions contenant des résines époxyCompositions contenant des dérivés des résines époxy
Provided is a latch assembly for a door. The latch assembly includes a housing defining a cavity, a handle movable relative to the housing, a latch disposed in the cavity, the latch having bolt movable between a locked and an unlocked position and a damping mechanism for delaying movement of the latch, wherein the handle is biased in a first position abutting the bolt to hold the bolt in the locked position, and the handle is movable to a second position away from the bolt allowing for movement of the bolt to the unlocked position.
E05C 1/16 - Dispositifs d'immobilisation avec pênes se déplaçant de façon rectiligne avec action d'une clenche avec poignée de manœuvre ou organe équivalent se déplaçant autrement que rigidement avec la clenche dont la poignée ou organe se déplace essentiellement dans un plan sensiblement parallèle au battant
An aircraft door includes a body defining a first body aperture therein and a primary panel pivotably attached to the body and configured to pivot between first and second positions, wherein when the primary panel is in the first position, the primary panel partially encloses the first body aperture, and wherein the primary panel has a first panel aperture defined therein. The aircraft door also includes a secondary panel pivotably attached to the primary panel and configured to pivot between first and second positions, wherein when the secondary panel is in the first position, the secondary panel encloses the first panel aperture.
An aircraft door includes a body defining a first body aperture therein and a primary panel pivotably attached to the body and configured to pivot between first and second positions, wherein when the primary panel is in the first position, the primary panel partially encloses the first body aperture, and wherein the primary panel has a first panel aperture defined therein. The aircraft door also includes a secondary panel pivotably attached to the primary panel and configured to pivot between first and second positions, wherein when the secondary panel is in the first position, the secondary panel encloses the first panel aperture.
A hold open rod that includes a locking collar that may be configured to operate in a first unlocked mode and a second unlocked mode in which the hold open rod is adjustable in a different manner than the first unlocked mode. For example, when in the first unlocked mode, the locking collar may be configured to lock the hold open rod when the hold open rod is compressed to an intermediately compressed configuration. When in the second unlocked mode, the locking collar may be configured allow the hold open rod to compress to the intermediately compressed configuration and continue compressing without locking the hold open rod, thereby bypassing locking of the hold open rod when in the intermediately compressed configuration.
A61B 17/70 - Dispositifs de mise en position ou de stabilisation de la colonne vertébrale, p. ex. stabilisateurs comprenant un liquide de remplissage dans un implant
E21B 17/046 - AccouplementsJoints entre tige et trépan, ou entre tiges avec nervures, goupilles ou mâchoires et rainures complémentaires ou similaires, p. ex. accrochage à baïonnette
6.
MULTI-FUNCTIONING LOCKING MECHANISM OF A HOLD OPEN ROD
A hold open rod that includes a locking collar that may be configured to operate in a first unlocked mode and a second unlocked mode in which the hold open rod is adjustable in a different manner than the first unlocked mode. For example, when in the first unlocked mode, the locking collar may be configured to lock the hold open rod when the hold open rod is compressed to an intermediately compressed configuration. When in the second unlocked mode, the locking collar may be configured allow the hold open rod to compress to the intermediately compressed configuration and continue compressing without locking the hold open rod, thereby bypassing locking of the hold open rod when in the intermediately compressed configuration.
E05C 17/30 - Dispositifs pour tenir les battants dans une position d'ouvertureDispositifs pour limiter l'ouverture des battants ou pour tenir les battants dans une position d'ouverture par une pièce mobile disposée entre le battant et le dormantDispositifs de freinage, butées ou tampons combinés avec ces dispositifs par des moyens mécaniques par une barre mobile ou une pièce équivalente disposée entre le dormant et le battant de structure extensible, p. ex. télescopique
B64C 1/14 - FenêtresPortesTrappes d'évacuation ou panneaux de visiteStructures de cadres environnantsVerrièresPare-brise
7.
PARACHUTE WITH CANOPY SLITS OR OPENINGS FOR PREVENTING CANOPY INVERSION
Parachutes which have a generally circular skirt or hem, such as semi-hemispherical, extended gore, or any variant of axisymmetric parachutes and cruciform parachutes with arms attached are disclosed with a plurality of vertical slits located in a circumferential band adjacent the skirt or hem of the parachute to prevent canopy inversion. During deployment, when the outer portion of the canopy is exposed to air flow, the slits open up and the drag of the skirt of the canopy is reduced, thus limiting the potential for hem migration. The slits are positioned to allow airflow therethrough in order for the pressure on the outside of the canopy to be transferred through the slit openings and released or transferred to inside of the lower section of the canopy. Instead of slits, elongated narrow openings can be utilized.
A method of connecting one or more fittings to a composite tube includes induction heating the composite tube to its gel transition temperature, inserting a first fitting into a first end portion of the tube after the induction heating, and compressing the first end portion of the tube over the first fitting.
A method of connecting one or more fittings to a composite tube includes induction heating the composite tube to its gel transition temperature, inserting a first fitting into a first end portion of the tube after the induction heating, and compressing the first end portion of the tube over the first fitting.
A drain assembly includes a drain body having an upper opening, a lower opening, a passage extending between the upper and lower openings, and a side opening into the passage, a drain insert received in the upper opening of drain body and movable relative to the drain body, the drain insert including an insert opening, and a locking knob coupled to the drain body, the locking knob including a stem extending through the side opening in the drain body into the insert opening to serve as a stop to prevent removal of the drain insert.
E03C 1/262 - Collecteurs ou dispositifs similaires de rétention d'objets pour les orifices d'écoulement ou les tuyaux d'évacuation des eaux usées combinés avec des bouchons d'orifice de sortie
A drain assembly includes a drain body having an upper opening, a lower opening, a passage extending between the upper and lower openings, and a side opening into the passage, a drain insert received in the upper opening of drain body and movable relative to the drain body, the drain insert including an insert opening, and a locking knob coupled to the drain body, the locking knob including a stem extending through the side opening in the drain body into the insert opening to serve as a stop to prevent removal of the drain insert.
A strut that includes a biasing member and a locking body that is configured to deactivate the biasing member. For example, the biasing member may be configured to urge an inner tube and an outer tube of the strut apart when the locking body is in a first position, and the biasing member may be configured to not urge the inner tube and the outer tube apart when the locking body is in a second position. Deactivation of the biasing member such that the inner tube and the outer tube are not urged apart by the biasing member may provide for increased safety during use of the when maintaining a spring door operating system that includes the strut.
E05F 1/10 - Appareils de fermeture ou d'ouverture pour battants, non prévus ailleurs dans la présente sous-classe actionnés par ressort pour battants pivotants
E05C 19/02 - Loquets automatiques, c.-à-d. libérés en tirant ou poussant le battant
13.
Laminate Structures For Aerospace and Commercial Transportation Interiors
The invention pertains to decorative laminate structures made with a combination of thermoplastic film and embossing resin layers with at least one layer of a thermoset polyimide. The laminate construction optimizes the low flammability characteristics, as well as providing low combustion toxicity and low smoke to comply with regulations and customer requirements. The laminates also providing formability and a lightweight, safe, and environmentally friendly material for use in the aerospace or other commercial transportation. The laminate also has high dimensional stability and tensile strength to facilitate manufacture and use, by retention of designs, textures, patterns, or three-dimensional characteristics. The laminate reduces or eliminates use of possibly hazardous flame retardant materials, and significantly reduces the weight of the laminate for various applications.
B32B 27/08 - Produits stratifiés composés essentiellement de résine synthétique comme seul composant ou composant principal d'une couche adjacente à une autre couche d'une substance spécifique d'une résine synthétique d'une sorte différente
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 7/12 - Liaison entre couches utilisant des adhésifs interposés ou des matériaux interposés ayant des propriétés adhésives
B32B 27/28 - Produits stratifiés composés essentiellement de résine synthétique comprenant des copolymères de résines synthétiques non complètement couverts par les sous-groupes suivants
An electro-mechanical power door operating system includes a strut having an inner tube and an outer tube; and an electrical actuator. The inner tube and the outer tube are in axial alignment and slidable relative to one another in a telescoping manner in response to operation of the electrical actuator.
E05F 15/622 - Mécanismes pour battants mus par une force motrice utilisant des actionneurs électriques utilisant des électromoteurs rotatifs pour battants pivotants manœuvrés par mécanismes "pousser-tirer" utilisant des mécanismes à écrou et vis
B64C 1/14 - FenêtresPortesTrappes d'évacuation ou panneaux de visiteStructures de cadres environnantsVerrièresPare-brise
15.
PLASMA GENERATION SYSTEM WITH PLASMA GENERATOR HAVING SHORT ELECTRODE PROTRUSION AND/OR DISCONNECTABLE PORTION
A plasma generation system includes a plasma generator such as an igniter and circuitry configured to apply a breakdown voltage across electrodes of the plasma generator to thereby form a plasma in an initiation region between the electrodes and then sustain and propagate the plasma outwardly for purposes such as combustion of a fuel. Various electrode configurations may be utilized that, along with plasma generating circuitry, enable the formation of virtual electrodes extending from the distal ends of the electrodes, resulting in a projection of plasma well beyond the physical electrodes. Such plasma generators may be used in various aerospace applications where only a short service life of the plasma generator is needed. Included are various techniques and components for enabling disconnection of the plasma generator from the system following ignition.
A plasma generation system includes a plasma generator such as an igniter and circuitry configured to apply a breakdown voltage across electrodes of the plasma generator to thereby form a plasma in an initiation region between the electrodes and then sustain and propagate the plasma outwardly for purposes such as combustion of a fuel. Various electrode configurations may be utilized that, along with plasma generating circuitry, enable the formation of virtual electrodes extending from the distal ends of the electrodes, resulting in a projection of plasma well beyond the physical electrodes. Such plasma generators may be used in various aerospace applications where only a short service life of the plasma generator is needed. Included are various techniques and components for enabling disconnection of the plasma generator from the system following ignition.
An igniter having at least two electrodes spaced from each other by an insulating member having a substantially continuous surface along a path between the electrodes. The electrodes extend substantially parallel to each other for a distance both above and below said surface. The insulating member has a channel (recess) for receiving at least a portion of a length of at least one of said electrodes below and to said surface of the insulating member. The surface of the insulating member may preferably be augmented with a conductivity enhancing agent. The insulating member and electrodes are configured so that an electric field between the electrodes at said surface does not have abrupt field intensity changes, whereby when a potential is applied to the electrodes sufficient to cause breakdown to occur between the electrodes, discharge occurs at said surface of the insulating member to define a plasma initiation region.
H01T 13/52 - Bougies d'allumage caractérisées par la décharge le long d'une surface
F02P 9/00 - Commande de l'allumage par étincelle électrique, non prévue ailleurs
F02P 23/04 - Autres moyens physiques d'allumage, p. ex. par laser
H01T 13/22 - Bougies d'allumage caractérisées par les particularités des électrodes ou de l'isolement avec plusieurs électrodes enrobées dans l'isolant
H01T 13/34 - Bougies d'allumage caractérisées par les particularités des électrodes ou de l'isolement caractérisées par le montage des électrodes dans l'isolant, p. ex. par enrobage
H01T 13/46 - Bougies d'allumage à plusieurs éclateurs
18.
SHARED CIRCUITRY CONFIGURATIONS FOR PLASMA GENERATION
The present disclosure provides shared circuitry configurations that may be implemented in a plasma generation system to improve control over application of electrical energy to a plasma generator, thereby providing improved performance. In some embodiments, shared circuitry configurations described herein may be implemented to improve performance of a traveling spark igniter that is configured to generate and propagate plasma using a Lorentz force and a thermal force, such as by applying electrical energy to electrodes of a plasma generator following breakdown between the electrodes. Other plasma generator configurations may also benefit from the circuitry configurations described herein.
The present disclosure provides shared circuitry configurations that may be implemented in a plasma generation system to improve control over application of electrical energy to a plasma generator, thereby providing improved performance. In some embodiments, shared circuitry configurations described herein may be implemented to improve performance of a traveling spark igniter that is configured to generate and propagate plasma using a Lorentz force and a thermal force, such as by applying electrical energy to electrodes of a plasma generator following breakdown between the electrodes. Other plasma generator configurations may also benefit from the circuitry configurations described herein.
A composite tube includes a first end opposite a second end, a first axial section including a non-conductive material through its thickness, and a second axial section including a conductive material. A method for forming a composite tube includes laying a plurality of composite material layers over a mandrel forming a composite tube, and each of the plurality of layers includes a non-conductive section and a conductive section.
B64C 13/30 - Dispositifs de transmission sans amplification de puissance ou dans les cas où l'amplification de puissance est sans objet mécaniques utilisant des mécanismes à câbles, chaînes ou tiges
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
F16L 7/00 - Support de tuyaux ou de câbles à l'intérieur d'autres tuyaux ou manchons, p. ex. pour permettre la pose ou le retrait de tuyaux ou de câbles sous des routes ou des voies ferrées sans devoir interrompre la circulation
21.
ELECTRODES WITH HIGH ASPECT RATIO FOR PLASMA GENERATION
A plasma generating system having an igniter or other plasma generator for use in low pressure environments, such as occurs in aviation. Combustion is initiated with an electrode configuration having a large usable area of electrodes for high current plasma discharge over a longer length of the electrodes, resulting in a long useful life of the plasma generator. The plasma generation system includes circuitry that generates and propagate plasma along the electrodes by a Lorentz force and a thermal force using high currents that move the plasma along the electrodes without causing a destructive material state change in the electrodes.
The present disclosure provides plasma generation techniques that may be implemented to maintain plasma coherence, resulting in high performance and long useful life of components, and which are suitable for use in a low-pressure environment (e.g., as in some aerospace applications) but are not limited thereto. In some embodiments, plasma generation and coherence maintaining techniques may be implemented to improve construction and/or operation of a traveling spark igniter that is configured to generate and propagate plasma using a Lorentz force and thermal force.
A plasma generating system having an igniter or other plasma generator for use in low pressure environments, such as occurs in aviation. Combustion is initiated with an electrode configuration having a large usable area of electrodes for high current plasma discharge over a longer length of the electrodes, resulting in a long useful life of the plasma generator. The plasma generation system includes circuitry that generates and propagate plasma along the electrodes by a Lorentz force and a thermal force using high currents that move the plasma along the electrodes without causing a destructive material state change in the electrodes.
The present disclosure provides plasma generation techniques that may be implemented to maintain plasma coherence, resulting in high performance and long useful life of components, and which are suitable for use in a low-pressure environment (e.g., as in some aerospace applications) but are not limited thereto. In some embodiments, plasma generation and coherence maintaining techniques may be implemented to improve construction and/or operation of a traveling spark igniter that is configured to generate and propagate plasma using a Lorentz force and thermal force.
B21D 39/04 - Utilisation de procédés permettant d'assembler des objets ou des parties d'objets, p. ex. revêtement par des tôles, autrement que par placageDispositifs de mandrinage des tubes des tubes avec des tubesUtilisation de procédés permettant d'assembler des objets ou des parties d'objets, p. ex. revêtement par des tôles, autrement que par placageDispositifs de mandrinage des tubes des tubes avec des barres
C08L 63/00 - Compositions contenant des résines époxyCompositions contenant des dérivés des résines époxy
B29C 64/153 - Procédés de fabrication additive n’utilisant que des matériaux solides utilisant des couches de poudre avec jonction sélective, p. ex. par frittage ou fusion laser sélectif
B64C 13/30 - Dispositifs de transmission sans amplification de puissance ou dans les cas où l'amplification de puissance est sans objet mécaniques utilisant des mécanismes à câbles, chaînes ou tiges
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
F16C 7/00 - Bielles ou organes de liaisons similaires pivotant aux deux extrémitésStructure des pieds de bielles
27.
3D PRINTED FITTINGS AND METHODS OF FORMING THE SAME
A 3D printed fitting includes an axially extending body having a first end opposite a second end. The body extends along a first axis, and the body is 3D printed by laying horizontal successive horizontal layers of material with the first axis at a print angle between 0 degrees and 65 degrees from a vertical axis.
B29C 64/147 - Procédés de fabrication additive n’utilisant que des matériaux solides utilisant des matériaux stratifiés, p. ex. fabrication d’objets stratifiés ou matériau stratifié prédécoupé selon les sections en coupe de l’objet en 3D
28.
AIRCRAFT PISTON ENGINE MAGNETO AND IGNITION SYSTEM
An aircraft piston engine magneto having a magnetic rotor and an ignition circuit that includes a charging coil inductively coupled to magnetic poles of the rotor. The charging coil includes a plurality of power coils that are inductively powered off the magnetic rotor and that charge the ignition circuit during rotation of the rotor. One or more of the power coils are electronically utilized by the ignition circuit as a higher turn power coil when the rotor is running at low speeds and as a lower turn power coil when the rotor is running at higher speeds. The ignition circuit is a fully electronic ignition circuit that generates and distributes ignition pulses to the piston engine spark plugs using only non-mechanically actuated electrical components within the magneto.
H02K 11/00 - Association structurelle de machines dynamo-électriques à des organes électriques ou à des dispositifs de blindage, de surveillance ou de protection
H01F 38/12 - Allumage, p. ex. pour moteurs à combustion interne
H02J 50/10 - Circuits ou systèmes pour l'alimentation ou la distribution sans fil d'énergie électrique utilisant un couplage inductif
H02K 1/22 - Parties tournantes du circuit magnétique
A fitting includes an annular composite interface having a first end opposite a second end. A first insert is at least partially within the composite interface and is couple or threaded to a second insert such that a portion to the composite interface is sandwiched between the first and second inserts. A method of forming such fitting includes 3D printing the annular composite interface.
A 3D printed fitting includes an axially extending body having a first end opposite a second end. The body extends along a first axis, and the body is 3D printed by laying horizontal successive horizontal layers of material with the first axis at a print angle between 0 degrees and 65 degrees from a vertical axis.
F16C 7/02 - Structure des bielles de longueur fixe
B29C 64/118 - Procédés de fabrication additive n’utilisant que des matériaux liquides ou visqueux, p. ex. dépôt d’un cordon continu de matériau visqueux utilisant un matériau filamentaire mis en fusion, p. ex. modélisation par dépôt de fil en fusion [FDM]
B29C 64/194 - Procédés de fabrication additive impliquant des opérations supplémentaires effectuées sur les couches ajoutées, p. ex. lissage, meulage ou contrôle d’épaisseur pendant l’empilage des couches
An electronic module assembly (EMA) for use in controlling one or more personal restraint systems. A programmed processor within the EMA is configured to determine when a personal restraint system associated with each seat in a vehicle should be deployed. In addition, the programmed processor is configured to perform a diagnostic self-test to determine if the EMA and the personal restraint systems are operational. In one embodiment, results of the diagnostic self-test routine are displayed on a display included on the electronic module assembly. In an alternative embodiment, the results of the diagnostic self-test routine are transmitted via a wireless transceiver to a remote device. The remote device can include a wireless interrogator or can be a remote computer system such as a cabin management computer system.
B64D 11/06 - Aménagements ou adaptations des sièges
B60R 21/00 - Dispositions ou équipements sur les véhicules pour protéger les occupants ou les piétons ou pour leur éviter des blessures en cas d'accidents ou d'autres incidents dus à la circulation
B60R 21/01 - Circuits électriques pour déclencher le fonctionnement des dispositions de sécurité en cas d'accident, ou d'accident imminent, de véhicule
B60R 21/0132 - Circuits électriques pour déclencher le fonctionnement des dispositions de sécurité en cas d'accident, ou d'accident imminent, de véhicule comportant des moyens pour détecter les collisions, les collisions imminentes ou un renversement réagissant à des paramètres de mouvement du véhicule
B60R 21/015 - Circuits électriques pour déclencher le fonctionnement des dispositions de sécurité en cas d'accident, ou d'accident imminent, de véhicule comportant des moyens pour détecter la présence ou la position des passagers, des sièges des passagers ou des sièges pour enfants, p. ex. pour mettre hors service le déclenchement
B60R 21/017 - Circuits électriques pour déclencher le fonctionnement des dispositions de sécurité en cas d'accident, ou d'accident imminent, de véhicule comportant des dispositions pour alimenter les dispositions de sécurité en courant électrique
B64D 25/00 - Appareils ou dispositifs pour circonstances critiques, non prévus ailleurs
B64D 25/02 - Dispositifs de soutien ou de maintien du corps humain
G07C 5/08 - Enregistrement ou indication de données de marche autres que le temps de circulation, de fonctionnement, d'arrêt ou d'attente, avec ou sans enregistrement des temps de circulation, de fonctionnement, d'arrêt ou d'attente
34.
LAMINATE STRUCTURES FOR AEROSPACE AND COMMERCIAL TRANSPORTATION INTERIORS
The invention pertains to decorative laminate structures made with a combination of thermoplastic film and embossing resin layers with at least one layer of a thermoset polyimide. The laminate construction optimizes the low flammability characteristics, as well as providing low combustion toxicity and low smoke to comply with regulations and customer requirements. The laminates also providing formability and a lightweight, safe, and environmentally friendly material for use in the aerospace or other commercial transportation. The laminate also has high dimensional stability and tensile strength to facilitate manufacture and use, by retention of designs, textures, patterns, or three-dimensional characteristics. The laminate reduces or eliminates use of possibly hazardous flame retardant materials, and significantly reduces the weight of the laminate for various applications.
B32B 27/28 - Produits stratifiés composés essentiellement de résine synthétique comprenant des copolymères de résines synthétiques non complètement couverts par les sous-groupes suivants
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 27/06 - Produits stratifiés composés essentiellement de résine synthétique comme seul composant ou composant principal d'une couche adjacente à une autre couche d'une substance spécifique
B32B 27/08 - Produits stratifiés composés essentiellement de résine synthétique comme seul composant ou composant principal d'une couche adjacente à une autre couche d'une substance spécifique d'une résine synthétique d'une sorte différente
B32B 27/12 - Produits stratifiés composés essentiellement de résine synthétique adjacente à une couche fibreuse ou filamenteuse
35.
Ignition system and igniter having ruthenium ground electrode and platinum-iridium alloy center electrode
An igniter for a gas turbine engine has a shell; an insulator secured within said shell; a center electrode secured within said insulator and electrically isolated from said shell by said insulator, said center electrode having a firing tip formed from a platinum-iridium (PtIr) alloy and having a diameter of at least 0.09 inches; and a ground electrode mounting on said shell and terminating at a firing end of the igniter that is spaced from the firing tip by a gap, said ground electrode having at least one pin comprising ruthenium (Ru) or a ruthenium alloy. The igniter is advantageously used with an ignition system having a positive polarity pulse output.
ADELWIGGINS GROUP, A DIVISION OF TRANSDIGM INC. (USA)
Inventeur(s)
Chung, Kevin Yun Jo
Quang, Christopher
Burgard, Kyle John
Medina, Andrew Daniel
Abrégé
A fuel refill system shutoff valve is provided for a fluid delivery system which provides internal pilot lines for use with a jet fluid level sensor. The shutoff valve is closed unless there is a positive signal from the return pilot line, so the shutoff valve fails in the closed position and avoids the situation where a failure leads to over-filling of the tank. An internal piston opens and closes peripheral fluid outlets based on the presence and/or absence of back pressure provided by the return signal of a fluid level sensor located inside the fuel tank of a vehicle.
B67D 7/36 - Aménagements des vannes de commande du débit ou de la pression
F16K 21/08 - Obturateurs à fermeture automatique, c.-à-d. se fermant d'eux-même après fonctionnement dans lesquels le mouvement de fermeture, ralenti ou non, commence immédiatement après l'ouverture avec éléments de fermeture en forme de sphère
F16K 21/18 - Obturateurs à fermeture automatique, c.-à-d. se fermant d'eux-même après fonctionnement fermés quand la montée du liquide atteint un niveau prédéterminé
F16K 27/02 - Structures des logementsMatériaux utilisés à cet effet des soupapes de levage
ADELWIGGINS GROUP, A DIVISION OF TRANSDIGM INC. (USA)
Inventeur(s)
Quang, Christopher
Medina, Andrew Daniel
Burgard, Kyle John
Abrégé
A fuel level sensor for a fast refill fuel system is presented having a T shaped valve for positive and negative pressure relief, and a non-spill valve that is overcome when there is a risk of over-pressurization. The level sensor is configured with first and second pilot lines located fully inside the fuel tank to avoid externally pilot lines. The jet level sensor is adjustable to set a height of the sensor corresponding to a selected fuel level.
F16K 21/18 - Obturateurs à fermeture automatique, c.-à-d. se fermant d'eux-même après fonctionnement fermés quand la montée du liquide atteint un niveau prédéterminé
B67D 7/36 - Aménagements des vannes de commande du débit ou de la pression
F16K 21/08 - Obturateurs à fermeture automatique, c.-à-d. se fermant d'eux-même après fonctionnement dans lesquels le mouvement de fermeture, ralenti ou non, commence immédiatement après l'ouverture avec éléments de fermeture en forme de sphère
F16K 27/02 - Structures des logementsMatériaux utilisés à cet effet des soupapes de levage
A lock for a secondary aircraft cockpit barrier, the lock comprising: a locking bar sub-assembly comprising: a locking bar; a receiving sub-assembly comprising: a cavity for receiving the locking bar; a locking retainer for retaining the locking bar in the cavity, the locking retainer comprising a lock cylinder and a locking plate; wherein the locking retainer is configured to move between a first position prior to the cavity receiving the locking bar, and a second position once the cavity receives the locking bar; wherein the lock cylinder is retained within the locking bar in the second position; a locking plate retainer configured to move between a first position in which the locking plate is retained and a second position in which the locking plate is released such that the locking retainer moves from the first to the second position; and a damped locking bar releasing mechanism for releasing the locking retainer, thereby unlocking the locking bar from the cavity; wherein the damped locking bar releasing mechanism is damped such that releasing the locking retainer requires about 5 seconds, is provided
A self-closing faucet comprises a faucet body having first and second ends and a through passage, a faucet cap positioned at the first end of the faucet body and movable relative to the faucet body, and a cartridge having a cartridge body disposed in the through passage and a cartridge cap connected to the faucet cap and movable relative to the cartridge body and faucet body, the cartridge body having a mixing chamber that receives fluid from one or more fluid sources, the mixing chamber being non-concentric to allow for a linear volume change rate during rotation of the faucet cap.
Provided is a faucet including a faucet body having first and second ends and a through passage, a faucet cap positioned at the first end of the faucet body and movable relative to the faucet body, and a cartridge having a cartridge body disposed in the through passage and a cartridge cap connected to the faucet cap and movable relative to the cartridge body and faucet body, the cartridge body having a mixing chamber that receives fluid from one or more fluid sources, the mixing chamber being non-concentric to allow for a linear volume change rate during rotation of the faucet cap.
Parachutes which have a generally circular skirt or hem, such as semi-hemispherical, extended gore, or any variant of axisymmetric parachutes and cruciform parachutes with arms attached are disclosed with a plurality of vertical slits located in a circumferential band adjacent the skirt or hem of the parachute to prevent canopy inversion. During deployment, when the outer portion of the canopy is exposed to air flow, the slits open up and the drag of the skirt of the canopy is reduced, thus limiting the potential for hem migration. The slits are positioned to allow airflow therethrough in order for the pressure on the outside of the canopy to be transferred through the slit openings and released or transferred to inside of the lower section of the canopy. Instead of slits, elongated narrow openings can be utilized.
Web retractors and associated systems and methods for retracting a web, such as a seat belt web, are disclosed herein. In some embodiments, a sealed web retractor includes a frame having a side wall with a first opening, a locking assembly housing attached to the side wall and having a second opening adjacent to the first opening, and a spool shaft having a portion that extends through the first and second openings. In some embodiments, the retractor can further include a bushing and a seal operably disposed in the first opening and extending around an outer periphery of the spool shaft.
B60R 22/347 - Moyens de rétraction de la ceinture, p. ex. enrouleurs avec des moyens pour verrouiller les moyens de rétraction de façon permanente durant le port de la ceinture
B60R 22/34 - Moyens de rétraction de la ceinture, p. ex. enrouleurs
Aircraft parts and accessories, namely, magnetos and magneto parts; ignition magnetos for engines; ignition harnesses, being aircraft engine parts; spark plugs.
Aircraft parts and accessories, namely, magnetos and magneto parts; ignition magnetos for engines; ignition harnesses, being aircraft engine parts; spark plugs.
48.
SEAT BELT WEB RETRACTORS AND ASSOCIATED SYSTEMS AND METHODS
Seat belt web retractor (100) having web (122) locking mechanisms are described herein. In some embodiments, a seat belt web retractor (100) includes an inertial locking mechanism (320) operably coupled to a spool (322) about which a seat belt web (122) is wound. The web retractor (100) further includes a web locking mechanism (470) operably coupled to the inertial locking mechanism (320). The web locking mechanism (470) can include a driving member (471) that is actuated by engagement of the inertial locking mechanism (320) with the web spool (322) in response to rapid extraction of the web (122) from the retractor (100). Actuation of the driving member (471) drives first and second clamping portions (482A, 482B) toward each other, thereby clamping the web (122) in between the clamping members (482A, 482B) and restraining the web (122) from further movement out of the retractor (100).
B60R 22/42 - Moyens de rétraction de la ceinture, p. ex. enrouleurs auto-verrouillables en cas d'urgence comportant des éléments agissant directement sur la ceinture, p. ex. par pincement ou friction
49.
SEAT BELT WEB RETRACTORS AND ASSOCIATED SYSTEMS AND METHODS
Seat belt web retractors having web locking mechanisms are described herein. In some embodiments, a seat belt web retractor includes an inertial locking mechanism operably coupled to a spool about which a seat belt web is wound. The web retractor further includes a web locking mechanism operably coupled to the inertial locking mechanism. The web locking mechanism can include a driving member that is actuated by engagement of the inertial locking mechanism with the web spool in response to rapid extraction of the web from the retractor. Actuation of the driving member drives first and second clamping portions toward each other, thereby clamping the web in between the clamping members and restraining the web from further movement out of the retractor.
An aircraft piston engine magneto having a magnetic rotor and an ignition circuit with a reconfigurable charging coil inductively coupled to magnetic rotor. The charging coil includes multiple coils inductively powered by the magnetic rotor and electronically reconfigurable from a higher turn, lower amperage power coil for use when running at low speeds into a lower turn, higher amperage coil at higher speeds. The charging coil is configured into the higher turn coil by electronically connecting the multiple coils in series, and into the lower turn power coil by electronically connecting the coils in parallel. The ignition circuit is a fully electronic ignition circuit that generates and distributes ignition pulses to the piston engine spark plugs using only non-mechanically actuated electrical components within the magneto.
A method for coupling a fitting to a tubing end includes pressing a collar over the outer surface of the tubing until the strain on the collar in the hoop direction is at a predetermined level, or pressing a collar with a predetermined axial load.
B21D 39/04 - Utilisation de procédés permettant d'assembler des objets ou des parties d'objets, p. ex. revêtement par des tôles, autrement que par placageDispositifs de mandrinage des tubes des tubes avec des tubesUtilisation de procédés permettant d'assembler des objets ou des parties d'objets, p. ex. revêtement par des tôles, autrement que par placageDispositifs de mandrinage des tubes des tubes avec des barres
C08L 63/00 - Compositions contenant des résines époxyCompositions contenant des dérivés des résines époxy
52.
AIRCRAFT PISTON ENGINE MAGNETO AND IGNITION SYSTEM
An aircraft piston engine magneto having a magnetic rotor and an ignition circuit with a reconfigurabie charging coil inductively coupled to magnetic rotor. The charging coil includes multiple coils inductively powered by the magnetic rotor and electronically reconfigurable from a higher turn, lower amperage power coil for use when running at low speeds into a lower turn, higher amperage coil at higher speeds. The charging coil is configured into the higher turn coil by electronically connecting the multiple coils in series, and into the lower turn power coil by electronically connecting the coils in parallel. The ignition circuit is a fully electronic ignition circuit that generates and distributes ignition pulses to the piston engine spark plugs using only non-mechanically actuated electrical components within the magneto.
F02P 15/00 - Allumage par étincelle électrique ayant des caractéristiques non couvertes dans les groupes ou présentant un intérêt autre que celui visé par ces groupes
B64D 27/04 - Aéronefs caractérisés par le type ou la position des groupes moteurs du type à pistons
Provided is a latch assembly for a door. The latch assembly includes a housing defining a cavity, a handle movable relative to the housing, a latch disposed in the cavity, the latch having bolt movable between a locked and an unlocked position and a damping mechanism for delaying movement of the latch, wherein the handle is biased in a first position abutting the bolt to hold the bolt in the locked position, and the handle is movable to a second position away from the bolt allowing for movement of the bolt to the unlocked position.
E05B 41/00 - Serrures à indication visible de la position de verrouillage ou de déverrouillage
E05B 51/02 - Fonctionnement ou commande des serrures ou autres dispositifs d'immobilisation par d'autres moyens non mécaniques par des moyens pneumatiques ou hydrauliques
E05B 63/18 - Serrures à caractéristiques structurales particulières avec dispositions indépendantes du mécanisme de verrouillage pour maintenir le pêne en position de retrait
E05B 63/24 - Aménagements dans lesquels les pièces montées respectivement sur le battant et le dormant, et s'engageant l'une dans l'autre, sont toutes deux mobiles, p. ex. pour être libérées par le déplacement de l'une ou l'autre d'entre elles
E05C 1/06 - Dispositifs d'immobilisation avec pênes se déplaçant de façon rectiligne sans action d'une clenche avec poignée de manœuvre ou organe équivalent se déplaçant autrement que rigidement
E05C 3/24 - Dispositifs d'immobilisation avec pênes se déplaçant de façon pivotante ou rotative avec action d'une clenche avec poignée de manœuvre ou organe équivalent se déplaçant autrement que rigidement avec la clenche le pêne étant commandé par un ressort ayant la forme d'un organe bifurqué
Provided is a latch assembly for a door. The latch assembly includes a housing defining a cavity, a handle movable relative to the housing, a latch disposed in the cavity, the latch having bolt movable between a locked and an unlocked position and a damping mechanism for delaying movement of the latch, wherein the handle is biased in a first position abutting the bolt to hold the bolt in the locked position, and the handle is movable to a second position away from the bolt allowing for movement of the bolt to the unlocked position.
E05C 1/16 - Dispositifs d'immobilisation avec pênes se déplaçant de façon rectiligne avec action d'une clenche avec poignée de manœuvre ou organe équivalent se déplaçant autrement que rigidement avec la clenche dont la poignée ou organe se déplace essentiellement dans un plan sensiblement parallèle au battant
Provided is a latch assembly for a door. The latch assembly includes a housing defining a cavity, a handle movable relative to the housing, a latch disposed in the cavity, the latch having bolt movable between a locked and an unlocked position and a damping mechanism for delaying movement of the latch, wherein the handle is biased in a first position abutting the bolt to hold the bolt in the locked position, and the handle is movable to a second position away from the bolt allowing for movement of the bolt to the unlocked position.
E05B 15/10 - Pênes de serrures ou verrous de sûreté
E05B 15/00 - Autres détails constitutifs des serruresÉléments permettant l'enclenchement par pênes des dispositifs de fermeture
E05B 63/18 - Serrures à caractéristiques structurales particulières avec dispositions indépendantes du mécanisme de verrouillage pour maintenir le pêne en position de retrait
E05B 63/24 - Aménagements dans lesquels les pièces montées respectivement sur le battant et le dormant, et s'engageant l'une dans l'autre, sont toutes deux mobiles, p. ex. pour être libérées par le déplacement de l'une ou l'autre d'entre elles
E05C 1/06 - Dispositifs d'immobilisation avec pênes se déplaçant de façon rectiligne sans action d'une clenche avec poignée de manœuvre ou organe équivalent se déplaçant autrement que rigidement
E05C 3/24 - Dispositifs d'immobilisation avec pênes se déplaçant de façon pivotante ou rotative avec action d'une clenche avec poignée de manœuvre ou organe équivalent se déplaçant autrement que rigidement avec la clenche le pêne étant commandé par un ressort ayant la forme d'un organe bifurqué
E05B 51/02 - Fonctionnement ou commande des serrures ou autres dispositifs d'immobilisation par d'autres moyens non mécaniques par des moyens pneumatiques ou hydrauliques
E05B 41/00 - Serrures à indication visible de la position de verrouillage ou de déverrouillage
59.
IGNITION SYSTEM AND IGNITER HAVING RUTHENIUM GROUND ELECTRODE AND PLATINUM-IRIDIUM ALLOY CENTER ELECTRODE
An igniter for a gas turbine engine has a shell; an insulator secured within said shell; a center electrode secured within said insulator and electrically isolated from said shell by said insulator, said center electrode having a firing tip formed from a platinum-iridium (Ptlr) alloy and having a diameter of at least 0.09 inches; and a ground electrode mounting on said shell and terminating at a firing end of the igniter that is spaced from the firing tip by a gap, said ground electrode having at least one pin comprising ruthenium (Ru) or a ruthenium alloy. The igniter is advantageously used with an ignition system having a positive polarity pulse output.
H01T 13/32 - Bougies d'allumage caractérisées par les particularités des électrodes ou de l'isolement caractérisées par les particularités de l'électrode de masse
A touchless faucet includes a faucet body having a first compartment and a second compartment, where the second compartment has a mixing chamber for mixing fluid and a flow passage. The faucet also includes an aerator coupled to the faucet body and configured to receive fluid from the flow passage, a control board disposed in the first compartment, a solenoid disposed in the second compartment and communicatively coupled to the control board, and an IR sensor disposed in the first compartment for sensing a presence of a user.
E03C 1/05 - Aménagements des dispositifs installés sur les lavabos, baignoires, éviers ou similaires pour commander les robinets à distance
F16K 11/00 - Soupapes ou clapets à voies multiples, p. ex. clapets mélangeursRaccords de tuyauteries comportant de tels clapets ou soupapesAménagement d'obturateurs et de voies d'écoulement spécialement conçu pour mélanger les fluides
An electronic module assembly (EMA) for use in controlling one or more personal restraint systems. A programmed processor within the EMA is configured to determine when a personal restraint system associated with each seat in a vehicle should be deployed. In addition, the programmed processor is configured to perform a diagnostic self-test to determine if the EMA and the personal restraint systems are operational. In one embodiment, results of the diagnostic self-test routine are displayed on a display included on the electronic module assembly. In an alternative embodiment, the results of the diagnostic self-test routine are transmitted via a wireless transceiver to a remote device. The remote device can include a wireless interrogator or can be a remote computer system such as a cabin management computer system.
B60R 21/00 - Dispositions ou équipements sur les véhicules pour protéger les occupants ou les piétons ou pour leur éviter des blessures en cas d'accidents ou d'autres incidents dus à la circulation
B60R 21/01 - Circuits électriques pour déclencher le fonctionnement des dispositions de sécurité en cas d'accident, ou d'accident imminent, de véhicule
B60R 21/0132 - Circuits électriques pour déclencher le fonctionnement des dispositions de sécurité en cas d'accident, ou d'accident imminent, de véhicule comportant des moyens pour détecter les collisions, les collisions imminentes ou un renversement réagissant à des paramètres de mouvement du véhicule
B60R 21/015 - Circuits électriques pour déclencher le fonctionnement des dispositions de sécurité en cas d'accident, ou d'accident imminent, de véhicule comportant des moyens pour détecter la présence ou la position des passagers, des sièges des passagers ou des sièges pour enfants, p. ex. pour mettre hors service le déclenchement
B60R 21/017 - Circuits électriques pour déclencher le fonctionnement des dispositions de sécurité en cas d'accident, ou d'accident imminent, de véhicule comportant des dispositions pour alimenter les dispositions de sécurité en courant électrique
B64D 11/06 - Aménagements ou adaptations des sièges
B64D 25/00 - Appareils ou dispositifs pour circonstances critiques, non prévus ailleurs
B64D 25/02 - Dispositifs de soutien ou de maintien du corps humain
G07C 5/08 - Enregistrement ou indication de données de marche autres que le temps de circulation, de fonctionnement, d'arrêt ou d'attente, avec ou sans enregistrement des temps de circulation, de fonctionnement, d'arrêt ou d'attente
AdelWiggins Group, a division of TransDigm Inc. (USA)
Inventeur(s)
Chung, Kevin Yun Jo
Abrégé
A non-metallic fluid coupling is disclosed with electrical current transferring elements incorporated therein. The coupling is formed of two C-shaped halves of non-metal, non-conducting material, where each halve includes integral hinges and latches, or hinges and latches made of a common material with the C-shaped halves. A non-metallic, substantially rigid sealing sleeve can be incorporated into the coupling to seal the coupling while maintaining the strength of the coupling.
F16L 25/01 - Structure ou détails de raccords de tuyaux non prévus dans les groupes ou présentant in intérêt autre que celui visé par ces groupes spécialement adaptés pour réaliser une conduction électrique entre les deux extrémités raccordées des tuyaux ou entre leurs éléments
F16L 25/06 - Structure ou détails de raccords de tuyaux non prévus dans les groupes ou présentant in intérêt autre que celui visé par ces groupes comprenant des moyens de verrouillage radiaux
F16L 25/02 - Structure ou détails de raccords de tuyaux non prévus dans les groupes ou présentant in intérêt autre que celui visé par ces groupes spécialement adaptés pour isoler électriquement l'une de l'autre les extrémités raccordées des tuyaux
69.
PARACHUTE WITH CANOPY SLITS OR OPENINGS FOR PREVENTING CANOPY INVERSION
Parachutes which have a generally circular skirt or hem, such as semi-hemispherical, extended gore, or any variant of axisymmetric parachutes and cruciform parachutes with arms attached are disclosed with a plurality of vertical slits located in a circumferential band adjacent the skirt or hem of the parachute to prevent canopy inversion. During deployment, when the outer portion of the canopy is exposed to air flow, the slits open up and the drag of the skirt of the canopy is reduced, thus limiting the potential for hem migration. The slits are positioned to allow airflow therethrough in order for the pressure on the outside of the canopy to be transferred through the slit openings and released or transferred to inside of the lower section of the canopy. Instead of slits, elongated narrow openings can be utilized.
Parachutes which have a generally circular skirt or hem, such as semi-hemispherical, extended gore, or any variant of axisymmetric parachutes and cruciform parachutes with arms attached are disclosed with a plurality of vertical slits located in a circumferential band adjacent the skirt or hem of the parachute to prevent canopy inversion. During deployment, when the outer portion of the canopy is exposed to air flow, the slits open up and the drag of the skirt of the canopy is reduced, thus limiting the potential for hem migration. The slits are positioned to allow airflow therethrough in order for the pressure on the outside of the canopy to be transferred through the slit openings and released or transferred to inside of the lower section of the canopy. Instead of slits, elongated narrow openings can be utilized.
Parachutes which have a generally circular skirt or hem, such as semi-hemispherical, extended gore, or any variant of axisymmetric parachutes and cruciform parachutes with arms attached are disclosed with a plurality of vertical slits located in a circumferential band adjacent the skirt or hem of the parachute to prevent canopy inversion. During deployment, when the outer portion of the canopy is exposed to air flow, the slits open up and the drag of the skirt of the canopy is reduced, thus limiting the potential for hem migration. The slits are positioned to allow airflow therethrough in order for the pressure on the outside of the canopy to be transferred through the slit openings and released or transferred to inside of the lower section of the canopy. Instead of slits, elongated narrow openings can be utilized.
An ignition circuit and a method of operating an igniter (preferably a traveling spark igniter) in an internal combustion engine, including a high pressure engine. A high voltage is applied to electrodes of the igniter, sufficient to cause breakdown to occur between the electrodes, resulting in a high current electrical discharge in the igniter, over a surface of an isolator between the electrodes, and formation of a plasma kernel in a fuel-air mixture adjacent said surface. Following breakdown, a sequence of one or more lower voltage and lower current pulses is applied to said electrodes, with a low “simmer” current being sustained through the plasma between pulses, preventing total plasma recombination and allowing the plasma kernel to move toward a free end of the electrodes with each pulse.
40 - Traitement de matériaux; recyclage, purification de l'air et traitement de l'eau
Produits et services
Manufacture of engineered aerospace products, namely, electromechanical products and mechanical products, namely, linear actuators, rotary actuators, ball screws, compressors, pumps, gear boxes, control electronics, flexible shafts and systems, namely, cargo handling systems for civil and military applications to order and/or specification of others
A shock absorber includes a first end configured to be mechanically fastened to a first component, a second end configured to be mechanically fastened to a second component, a main body, a main shaft, and a primary piston. The primary piston configured to move within the main body and further configured to provide a first damping force by movement of a fluid through the primary piston while the main shaft moves a first distance. The shock absorber also includes a deformable solid material arranged in the main body. The primary piston configured to further move within the main body and further configured to provide a second damping force by deforming the deformable solid material after the main shaft moves the first distance.
F16F 7/12 - Amortisseurs de vibrationsAmortisseurs de chocs utilisant une déformation plastique de ses organes
B64C 1/14 - FenêtresPortesTrappes d'évacuation ou panneaux de visiteStructures de cadres environnantsVerrièresPare-brise
E05B 77/54 - Verrouillage ou déverrouillage automatique de pênes provoqué par certains paramètres du véhicule, p. ex. par le dépassement d’un seuil de vitesse
E05F 3/04 - Appareils de fermeture ou d'ouverture à dispositif de freinage, p. ex. ralentisseursStructure des dispositifs de freinage pneumatique ou à liquide avec freins à piston à liquide
F16F 9/00 - Ressorts, amortisseurs de vibrations, amortisseurs de chocs ou amortisseurs de mouvement de structure similaire, utilisant un fluide ou moyen équivalent comme agent d'amortissement
F16F 9/19 - Dispositifs à un ou plusieurs organes, p. ex. des pistons, des aubes, se déplaçant en va-et-vient dans des chambres et utilisant un effet d'étranglement comportant uniquement un déplacement rectiligne des parties travaillant avec un cylindre fermé et un piston déterminant, à l’intérieur de ce cylindre, plusieurs espaces de travail avec un seul cylindre
F16F 9/48 - Dispositions permettant différents effets d'amortissement à différents points de la course
B64C 1/00 - FuselagesCaractéristiques structurales communes aux fuselages, voilures, surfaces stabilisatrices ou organes apparentés
F16F 9/16 - Dispositifs à un ou plusieurs organes, p. ex. des pistons, des aubes, se déplaçant en va-et-vient dans des chambres et utilisant un effet d'étranglement comportant uniquement un déplacement rectiligne des parties travaillant
F16F 9/30 - Ressorts, amortisseurs de vibrations, amortisseurs de chocs ou amortisseurs de mouvement de structure similaire, utilisant un fluide ou moyen équivalent comme agent d'amortissement avec un matériau solide ou semi-solide, p. ex. des masses pâteuses, comme agent d'amortissement
22 - Cordes; filets; tentes, auvents, voiles et sacs; matières de rembourrage
Produits et services
Nets; cargo nets; belly hold nets; barrier nets; door nets;
bulk-hold baggage nets; bulk cargo nets; pallet nets;
freight nets; throw-over nets; helicopter under-slung nets;
airdrop nets; restraint nets; cargo slings of rope or
fabric; adjustable restraint straps for handling loads; net,
string, cords and twine; ropes and slings for the handling
and transportation of loads, all being non-metallic;
camouflage nets; sacks; armour systems made wholly or
principally from net material; net-based defensive shields;
net-based RPG (rocket propelled grenades) countermeasures;
vehicle mounted net-based defensive shields; ground mounted
net-based defensive shields; parts and fittings for all the
aforesaid goods.
77.
Dual drive redundant load transmission device and process
A redundant load transmission includes an input shaft configured to receive a rotational torque from a primary drive, an output shaft configured to transmit the rotational torque to an actuator, and a coupling assembly configured to connect the input shaft to the output shaft to transmit the rotational torque. The input shaft is configured to receive the rotational torque from the primary drive and transmit the rotational torque through the coupling assembly when the coupling assembly is in a primary drive configuration. The coupling assembly is configured to be disconnected from the input shaft and transmit a rotational torque to the output shaft from a secondary drive when the coupling assembly is in a secondary drive configuration.
F16H 19/08 - Transmissions comportant essentiellement et uniquement des engrenages ou des organes de friction et qui ne peuvent transmettre un mouvement rotatif indéfini pour convertir un mouvement rotatif en mouvement oscillant et vice versa
A redundant load transmission includes an input shaft configured to receive a rotational torque from a primary drive, an output shaft configured to transmit the rotational torque to an actuator, and a coupling assembly configured to connect the input shaft to the output shaft to transmit the rotational torque. The input shaft is configured to receive the rotational torque from the primary drive and transmit the rotational torque through the coupling assembly when the coupling assembly is in a primary drive configuration. The coupling assembly is configured to be disconnected from the input shaft and transmit a rotational torque to the output shaft from a secondary drive when the coupling assembly is in a secondary drive configuration.
F16H 37/06 - Combinaisons de transmissions mécaniques non prévues dans les groupes comportant essentiellement et uniquement des transmissions à engrenages ou à friction à plusieurs arbres d’entraînement ou entraînésCombinaisons de transmissions mécaniques non prévues dans les groupes comportant essentiellement et uniquement des transmissions à engrenages ou à friction avec dispositions pour répartir le couple entre plusieurs arbres intermédiaires
79.
DUAL DRIVE REDUNDANT LOAD TRANSMISSION DEVICE AND PROCESS
A redundant load transmission includes an input shaft configured to receive a rotational torque from a primary drive, an output shaft configured to transmit the rotational torque to an actuator, and a coupling assembly configured to connect the input shaft to the output shaft to transmit the rotational torque. The input shaft is configured to receive the rotational torque from the primary drive and transmit the rotational torque through the coupling assembly when the coupling assembly is in a primary drive configuration. The coupling assembly is configured to be disconnected from the input shaft and transmit a rotational torque to the output shaft from a secondary drive when the coupling assembly is in a secondary drive configuration.
F16H 37/06 - Combinaisons de transmissions mécaniques non prévues dans les groupes comportant essentiellement et uniquement des transmissions à engrenages ou à friction à plusieurs arbres d’entraînement ou entraînésCombinaisons de transmissions mécaniques non prévues dans les groupes comportant essentiellement et uniquement des transmissions à engrenages ou à friction avec dispositions pour répartir le couple entre plusieurs arbres intermédiaires
An igniter having at least two electrodes spaced from each other by an insulating member having a substantially continuous surface along a path between the electrodes. The electrodes extend substantially parallel to each other for a distance both above and below said surface. The insulating member has a channel (recess) for receiving at least a portion of a length of at least one of said electrodes below and to said surface of the insulating member. The surface of the insulating member may preferably be augmented with a conductivity enhancing agent. The insulating member and electrodes are configured so that an electric field between the electrodes at said surface does not have abrupt field intensity changes, whereby when a potential is applied to the electrodes sufficient to cause breakdown to occur between the electrodes, discharge occurs at said surface of the insulating member to define a plasma initiation region.
H01T 13/52 - Bougies d'allumage caractérisées par la décharge le long d'une surface
F02P 9/00 - Commande de l'allumage par étincelle électrique, non prévue ailleurs
H01T 13/34 - Bougies d'allumage caractérisées par les particularités des électrodes ou de l'isolement caractérisées par le montage des électrodes dans l'isolant, p. ex. par enrobage
H01T 13/46 - Bougies d'allumage à plusieurs éclateurs
H01T 13/22 - Bougies d'allumage caractérisées par les particularités des électrodes ou de l'isolement avec plusieurs électrodes enrobées dans l'isolant
F02P 23/04 - Autres moyens physiques d'allumage, p. ex. par laser
21 - Ustensiles, récipients, matériaux pour le ménage; verre; porcelaine; faience
Produits et services
Faucet aerators; faucet handles; faucet sprayers; faucets; automatic faucets; flush handles for toilets, namely, flush switch for toilet Accessories for waste baskets in the nature of waste basket flaps
A latch mechanism includes a hook, a displaceable handle, and links connected between the handle and hook for the operation of the latch mechanism. The handle and links cooperate with the hook to hold the latch mechanism in a locked position.
E05B 63/06 - Serrures à caractéristiques structurales particulières avec pênes réglables dans le sens de la longueur
E05C 19/14 - Immobilisations à crochetImmobilisations dans lesquelles un maillon enclenche un élément fixe du type crochet montées sur pivot à action articulée
A fabric barrier for an aircraft compartmental barrier includes a fabric barrier portion and a flexible crosspiece, wherein at least part of one edge of the fabric barrier portion terminates at the flexible crosspiece, wherein the flexible crosspiece is adapted to fit into and be retained within a partially covered groove, wherein the partially covered groove includes a pair of opposing flange portions covering a groove whereby a central longitudinal portion of the groove remains uncovered, wherein the flexible crosspiece is adapted to be released from the partially covered groove by passing between the pair of opposing flange portions during a decompression event. A decompression system for an aircraft compartmental barrier includes said fabric barrier, and a method for isolating two internal volumes within an aircraft using said decompression system.
A62C 3/08 - Prévention, limitation ou extinction des incendies spécialement adaptées pour des objets ou des endroits particuliers dans les véhicules, p. ex. les véhicules routiers dans les avions
B64C 1/00 - FuselagesCaractéristiques structurales communes aux fuselages, voilures, surfaces stabilisatrices ou organes apparentés
B64C 1/14 - FenêtresPortesTrappes d'évacuation ou panneaux de visiteStructures de cadres environnantsVerrièresPare-brise
A method for coupling a fitting to a tubing end includes pressing a collar over the outer surface of the tubing until the strain on the collar in the hoop direction is at a predetermined level, or pressing a collar with a predetermined axial load.
B21D 39/04 - Utilisation de procédés permettant d'assembler des objets ou des parties d'objets, p. ex. revêtement par des tôles, autrement que par placageDispositifs de mandrinage des tubes des tubes avec des tubesUtilisation de procédés permettant d'assembler des objets ou des parties d'objets, p. ex. revêtement par des tôles, autrement que par placageDispositifs de mandrinage des tubes des tubes avec des barres
C08L 63/00 - Compositions contenant des résines époxyCompositions contenant des dérivés des résines époxy
22 - Cordes; filets; tentes, auvents, voiles et sacs; matières de rembourrage
Produits et services
Nets, namely cargo nets, belly hold nets, barrier nets, door nets, bulk-hold baggage nets, bulk cargo nets, pallet nets, freight nets, throw-over nets, helicopter under-slung net, airdrop nets, restraint nets; cargo slings of rope or fabric; adjustable restraint straps for handling loads of rope or fabric; net wrapping for pallets, string, cords and twine; ropes and slings for the handling and transportation of loads, all being non-metallic; camouflage nets; sacks for the transport or storage of materials in bulk; armour systems made wholly or principally from net material, namely, net-based defensive shields; net-based RPG (rocket propelled grenades) countermeasures; vehicle mounted net-based defensive shields; ground mounted net-based defensive shields; structural parts and fittings for all the aforesaid goods
89.
CONTROL SURFACES AND SYSTEMS AND METHODS FOR SANITATION OF CONTROL SURFACES
The invention relates to sanitizing surfaces designed to be touched with sanitation systems and methods for sanitizing such surfaces, such as a control surface which must be touched to either directly or indirectly cause an action. At least one irradiation system includes at least one UVGI emitter in at least one array configured to irradiate at least a portion of a predetermined surface with a predetermined dose of UV radiation, such as after touching of the surface.
A61L 2/10 - 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 phénomènes physiques des radiations des ultraviolets
A61L 2/24 - Appareils utilisant des opérations programmées ou automatiques
90.
SANITIZING SYSTEMS AND METHODS FOR COMMERCIAL PASSENGER VEHICLES
The invention relates to a sanitation treatment system and methods for use in association with commercial passenger vehicles such as aircraft. The sanitation system may operate along with a filtration system in an air distribution system associated with an aircraft or like commercial passenger vehicles and/or to provide disinfected air and surfaces in the passenger cabin associated with the aircraft or like vehicle.
A61L 9/20 - Désinfection, stérilisation ou désodorisation de l'air utilisant des phénomènes physiques des radiations des ultraviolets
A61L 2/10 - 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 phénomènes physiques des radiations des ultraviolets
B64D 13/08 - Aménagements ou adaptations des appareils de conditionnement d'air pour équipages d'aéronefs, passagers ou pour emplacements réservés au fret l'air étant climatisé l'air étant réchauffé ou refroidi
A touchless faucet includes a faucet body having a first compartment and a second compartment, where the second compartment has a mixing chamber for mixing fluid and a flow passage. The faucet also includes an aerator coupled to the faucet body and configured to receive fluid from the flow passage, a control board disposed in the first compartment, a solenoid disposed in the second compartment and communicatively coupled to the control board, and an IR sensor disposed in the first compartment for sensing a presence of a user.
E03C 1/05 - Aménagements des dispositifs installés sur les lavabos, baignoires, éviers ou similaires pour commander les robinets à distance
F16K 11/00 - Soupapes ou clapets à voies multiples, p. ex. clapets mélangeursRaccords de tuyauteries comportant de tels clapets ou soupapesAménagement d'obturateurs et de voies d'écoulement spécialement conçu pour mélanger les fluides
A method for coupling a fitting to a tubing end includes pressing a collar over the outer surface of the tubing until the strain on the collar in the hoop direction is at a predetermined level, or pressing a collar with a predetermined axial load.
B21D 39/04 - Utilisation de procédés permettant d'assembler des objets ou des parties d'objets, p. ex. revêtement par des tôles, autrement que par placageDispositifs de mandrinage des tubes des tubes avec des tubesUtilisation de procédés permettant d'assembler des objets ou des parties d'objets, p. ex. revêtement par des tôles, autrement que par placageDispositifs de mandrinage des tubes des tubes avec des barres
C08L 63/00 - Compositions contenant des résines époxyCompositions contenant des dérivés des résines époxy
A latching system for releasably securing a first structure relative to a second structure. The latching system includes a latch assembly coupled to the first structure and a keeper assembly coupled to the second structure. The latch assembly is selectively engageable with the keeper assembly to hold the first structure against movement relative to the second structure.
B64D 29/06 - Fixation des nacelles, carénages ou capotages
E05B 63/00 - Serrures à caractéristiques structurales particulières
E05C 19/14 - Immobilisations à crochetImmobilisations dans lesquelles un maillon enclenche un élément fixe du type crochet montées sur pivot à action articulée
ADEL WIGGINS GROUP, A DIVISION OF TRANSDIGM INC. (USA)
Inventeur(s)
Chung, Kevin Yun Jo
Abrégé
A non-metallic fluid coupling is disclosed with electrical current transferring elements incorporated therein. The coupling is formed of two C-shaped halves of non-metal, non-conducting material, where each halve includes integral hinges and latches, or hinges and latches made of a common material with the C-shaped halves. A non-metallic, substantially rigid sealing sleeve can be incorporated into the coupling to seal the coupling while maintaining the strength of the coupling.
F16L 19/10 - Raccords dans lesquels les surfaces d'étanchéité sont maintenues en contact par un organe, p. ex. un écrou à oreilles vissé dans, ou vissé sur une des parties du raccord avec segments métalliques qui mordent dans la paroi du tuyau le profil du segment étant déformé
F16L 19/12 - Raccords dans lesquels les surfaces d'étanchéité sont maintenues en contact par un organe, p. ex. un écrou à oreilles vissé dans, ou vissé sur une des parties du raccord avec segments métalliques qui mordent dans la paroi du tuyau le profil du segment étant déformé avec des moyens d'étanchéité supplémentaires
F16L 25/01 - Structure ou détails de raccords de tuyaux non prévus dans les groupes ou présentant in intérêt autre que celui visé par ces groupes spécialement adaptés pour réaliser une conduction électrique entre les deux extrémités raccordées des tuyaux ou entre leurs éléments
ADELWIGGINS GROUP, A DIVISION OF TRANSDIGM INC. (USA)
Inventeur(s)
Chung, Kevin Yun Jo
Abrégé
A non-metallic fluid coupling is disclosed with electrical current transferring elements incorporated therein. The coupling is formed of two C-shaped halves of non-metal, non-conducting material, where each halve includes integral hinges and latches, or hinges and latches made of a common material with the C-shaped halves. A non-metallic, substantially rigid sealing sleeve can be incorporated into the coupling to seal the coupling while maintaining the strength of the coupling.
F16L 25/01 - Structure ou détails de raccords de tuyaux non prévus dans les groupes ou présentant in intérêt autre que celui visé par ces groupes spécialement adaptés pour réaliser une conduction électrique entre les deux extrémités raccordées des tuyaux ou entre leurs éléments
F16L 37/00 - Accouplements du type à action rapide
F16L 19/10 - Raccords dans lesquels les surfaces d'étanchéité sont maintenues en contact par un organe, p. ex. un écrou à oreilles vissé dans, ou vissé sur une des parties du raccord avec segments métalliques qui mordent dans la paroi du tuyau le profil du segment étant déformé
F16L 19/12 - Raccords dans lesquels les surfaces d'étanchéité sont maintenues en contact par un organe, p. ex. un écrou à oreilles vissé dans, ou vissé sur une des parties du raccord avec segments métalliques qui mordent dans la paroi du tuyau le profil du segment étant déformé avec des moyens d'étanchéité supplémentaires
AdelWiggins Group, a division of TransDigm Inc. (USA)
Inventeur(s)
Chung, Kevin Yun Jo
Abrégé
A non-metallic fluid coupling is disclosed with electrical current transferring elements incorporated therein. The coupling is formed of two C-shaped halves of non-metal, non-conducting material, where each halve includes integral hinges and latches, or hinges and latches made of a common material with the C-shaped halves. A non-metallic, substantially rigid sealing sleeve can be incorporated into the coupling to seal the coupling while maintaining the strength of the coupling.
F16L 25/01 - Structure ou détails de raccords de tuyaux non prévus dans les groupes ou présentant in intérêt autre que celui visé par ces groupes spécialement adaptés pour réaliser une conduction électrique entre les deux extrémités raccordées des tuyaux ou entre leurs éléments
F16L 25/06 - Structure ou détails de raccords de tuyaux non prévus dans les groupes ou présentant in intérêt autre que celui visé par ces groupes comprenant des moyens de verrouillage radiaux
F16L 25/02 - Structure ou détails de raccords de tuyaux non prévus dans les groupes ou présentant in intérêt autre que celui visé par ces groupes spécialement adaptés pour isoler électriquement l'une de l'autre les extrémités raccordées des tuyaux
Containers of metal for transportation; hooklift containers
of metal; containers of metal [storage, transport];
containers of metal for storage and transport of goods;
storage containers of metal; general purpose storage
containers of metal. Containers, not of metal [storage, transport]; shipping and
storage boxes of plastic.
A latch mechanism includes a hook-handle assembly coupled to a first panel and a clevis coupled to a second panel. The hook-handle assembly engages the clevis to secure the first panel relative to the second panel.
E05B 27/00 - Serrures cylindriques avec broches à gorges ou billes qui sont mises en place par l'introduction de la clé
E05B 63/12 - Serrures à caractéristiques structurales particulières avec des moyens fixés sur le pêne pour le verrouillage par enclenchement avec la gâche
E05B 15/02 - GâchesPlatinesPênes-cramponsÉcussons de serrures
E05B 41/00 - Serrures à indication visible de la position de verrouillage ou de déverrouillage
E05C 19/14 - Immobilisations à crochetImmobilisations dans lesquelles un maillon enclenche un élément fixe du type crochet montées sur pivot à action articulée
E05B 13/00 - Dispositifs empêchant l'utilisation de la clé, de la poignée ou des deux
E05B 27/08 - Serrures cylindriques avec broches à gorges ou billes qui sont mises en place par l'introduction de la clé à fonctionnement commandé par la tranche de la clé à montage axial
E05B 63/18 - Serrures à caractéristiques structurales particulières avec dispositions indépendantes du mécanisme de verrouillage pour maintenir le pêne en position de retrait
E05B 13/10 - Dispositifs empêchant l'utilisation de la clé, de la poignée ou des deux consistant en une serrure montée dans la poignée
