This specification discloses an aircraft maintenance kit. The aircraft maintenance kit comprises a plurality of packages with each package of the plurality of packages comprising a unique aircraft maintenance zone designation and at least one maintenance zone component. Each unique aircraft maintenance zone designation preferably corresponds to a unique maintenance zone of the aircraft. Preferably, the aircraft maintenance kit also comprises an aircraft schematic comprising a plurality of aircraft schematic zones. Each aircraft schematic zone preferably comprises a unique aircraft schematic zone designation corresponding to one of the unique aircraft maintenance zone designations.
This specification discloses an article of manufacture. The article of manufacture has at least one structural blank and at least one guide. The structural blank has a plurality of oriented fiber plies in a thermoplastic matrix. The guide has a plurality of random dispersed fibers in a thermoplastic matrix. The guide is affixed to the structural blank by injection molding and over molding the guide onto the structural blank. The article of manufacture can take a number of forms for use in industries such as aircraft, automobiles, motorcycles, bicycles, trains or watercraft.
B29C 45/14 - Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mouldApparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles
B29C 70/74 - Moulding material on a relatively small portion of the preformed part, e.g. outsert moulding
B29C 70/76 - Moulding on edges or extremities of the preformed part
B29C 70/12 - Fibrous reinforcements only characterised by the structure of fibrous reinforcements using fibres of short length, e.g. in the form of a mat
B29C 65/00 - Joining of preformed partsApparatus therefor
A47C 7/40 - Supports for the head or the back for the back
B29C 65/48 - Joining of preformed partsApparatus therefor using adhesives
B29C 65/56 - Joining of preformed partsApparatus therefor using mechanical means
B32B 3/26 - Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layerLayered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by a layer with cavities or internal voids
B32B 5/26 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by the presence of two or more layers which comprise fibres, filaments, granules, or powder, or are foamed or specifically porous one layer being a fibrous or filamentary layer another layer also being fibrous or filamentary
B32B 5/28 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by the presence of two or more layers which comprise fibres, filaments, granules, or powder, or are foamed or specifically porous one layer being a fibrous or filamentary layer impregnated with or embedded in a plastic substance
B32B 5/02 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by structural features of a layer comprising fibres or filaments
B32B 27/28 - Layered products essentially comprising synthetic resin comprising copolymers of synthetic resins not wholly covered by any one of the following subgroups
B29L 31/30 - Vehicles, e.g. ships or aircraft, or body parts thereof
B29K 105/08 - Condition, form or state of moulded material containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
B29K 71/00 - Use of polyethers as moulding material
B29K 67/00 - Use of polyesters as moulding material
B29K 79/00 - Use of other polymers having nitrogen, with or without oxygen or carbon only, in the main chain, as moulding material
B29K 81/00 - Use of polymers having sulfur, with or without nitrogen, oxygen or carbon only, in the main chain, as moulding material
B29C 70/20 - Fibrous reinforcements only characterised by the structure of fibrous reinforcements using fibres of substantial or continuous length oriented in a single direction, e.g. roving or other parallel fibres
B29C 70/22 - Fibrous reinforcements only characterised by the structure of fibrous reinforcements using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure
B29C 70/16 - Fibrous reinforcements only characterised by the structure of fibrous reinforcements using fibres of substantial or continuous length
B29C 65/08 - Joining of preformed partsApparatus therefor by heating, with or without pressure using ultrasonic vibrations
B29C 65/34 - Joining of preformed partsApparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement"
B29C 65/50 - Joining of preformed partsApparatus therefor using adhesives using adhesive tape
B29C 65/72 - Joining of preformed partsApparatus therefor by combined operations, e.g. welding and stitching
B29C 45/00 - Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mouldApparatus therefor
This specification discloses an article of manufacture. The article of manufacture has at least one structural blank and at least one guide. The structural blank has a plurality of oriented fiber plies in a thermoplastic matrix. The guide has a plurality of random dispersed fibers in a thermoplastic matrix. The guide is affixed to the structural blank by injection molding and over molding the guide onto the structural blank. The article of manufacture can take a number of forms for use in industries such as aircraft, automobiles, motorcycles, bicycles, trains or watercraft.
B32B 3/24 - Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. apertured or formed of separate pieces of material characterised by an apertured layer, e.g. of expanded metal
B32B 5/02 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by structural features of a layer comprising fibres or filaments
B29C 70/12 - Fibrous reinforcements only characterised by the structure of fibrous reinforcements using fibres of short length, e.g. in the form of a mat
B29C 70/16 - Fibrous reinforcements only characterised by the structure of fibrous reinforcements using fibres of substantial or continuous length
B29C 70/20 - Fibrous reinforcements only characterised by the structure of fibrous reinforcements using fibres of substantial or continuous length oriented in a single direction, e.g. roving or other parallel fibres
B29C 70/22 - Fibrous reinforcements only characterised by the structure of fibrous reinforcements using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure
B29C 45/14 - Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mouldApparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles
B32B 3/26 - Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layerLayered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by a layer with cavities or internal voids
B29C 70/74 - Moulding material on a relatively small portion of the preformed part, e.g. outsert moulding
B29C 70/76 - Moulding on edges or extremities of the preformed part
B29C 65/00 - Joining of preformed partsApparatus therefor
A47C 7/40 - Supports for the head or the back for the back
B29C 65/48 - Joining of preformed partsApparatus therefor using adhesives
B29C 65/56 - Joining of preformed partsApparatus therefor using mechanical means
B32B 5/26 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by the presence of two or more layers which comprise fibres, filaments, granules, or powder, or are foamed or specifically porous one layer being a fibrous or filamentary layer another layer also being fibrous or filamentary
B32B 5/28 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by the presence of two or more layers which comprise fibres, filaments, granules, or powder, or are foamed or specifically porous one layer being a fibrous or filamentary layer impregnated with or embedded in a plastic substance
B32B 27/28 - Layered products essentially comprising synthetic resin comprising copolymers of synthetic resins not wholly covered by any one of the following subgroups
B29L 31/30 - Vehicles, e.g. ships or aircraft, or body parts thereof
B29K 105/08 - Condition, form or state of moulded material containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
B29K 71/00 - Use of polyethers as moulding material
B29K 67/00 - Use of polyesters as moulding material
B29K 79/00 - Use of other polymers having nitrogen, with or without oxygen or carbon only, in the main chain, as moulding material
B29K 81/00 - Use of polymers having sulfur, with or without nitrogen, oxygen or carbon only, in the main chain, as moulding material
B29C 65/08 - Joining of preformed partsApparatus therefor by heating, with or without pressure using ultrasonic vibrations
B29C 65/34 - Joining of preformed partsApparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement"
B29C 65/50 - Joining of preformed partsApparatus therefor using adhesives using adhesive tape
B29C 65/72 - Joining of preformed partsApparatus therefor by combined operations, e.g. welding and stitching
B29C 45/00 - Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mouldApparatus therefor
This specification discloses an article of manufacture. The article of manufacture has at least one structural blank and at least one guide. The structural blank has a plurality of oriented fiber plies in a thermoplastic matrix. The guide has a plurality of random dispersed fibers in a thermoplastic matrix. The guide is affixed to the structural blank by injection molding and over molding the guide onto the structural blank. The article of manufacture can take a number of forms for use in industries such as aircraft, automobiles, motorcycles, bicycles, trains or watercraft.
B32B 5/26 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by the presence of two or more layers which comprise fibres, filaments, granules, or powder, or are foamed or specifically porous one layer being a fibrous or filamentary layer another layer also being fibrous or filamentary
B32B 3/26 - Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layerLayered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by a layer with cavities or internal voids
B29C 45/14 - Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mouldApparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles
B29C 70/74 - Moulding material on a relatively small portion of the preformed part, e.g. outsert moulding
B29C 70/76 - Moulding on edges or extremities of the preformed part
B29C 70/12 - Fibrous reinforcements only characterised by the structure of fibrous reinforcements using fibres of short length, e.g. in the form of a mat
B32B 5/28 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by the presence of two or more layers which comprise fibres, filaments, granules, or powder, or are foamed or specifically porous one layer being a fibrous or filamentary layer impregnated with or embedded in a plastic substance
B32B 5/02 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by structural features of a layer comprising fibres or filaments
B32B 27/28 - Layered products essentially comprising synthetic resin comprising copolymers of synthetic resins not wholly covered by any one of the following subgroups
B29L 31/30 - Vehicles, e.g. ships or aircraft, or body parts thereof
B29K 105/08 - Condition, form or state of moulded material containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
B29K 71/00 - Use of polyethers as moulding material
B29K 67/00 - Use of polyesters as moulding material
B29K 79/00 - Use of other polymers having nitrogen, with or without oxygen or carbon only, in the main chain, as moulding material
B29K 81/00 - Use of polymers having sulfur, with or without nitrogen, oxygen or carbon only, in the main chain, as moulding material
B29C 70/20 - Fibrous reinforcements only characterised by the structure of fibrous reinforcements using fibres of substantial or continuous length oriented in a single direction, e.g. roving or other parallel fibres
B29C 70/22 - Fibrous reinforcements only characterised by the structure of fibrous reinforcements using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure
B29C 70/16 - Fibrous reinforcements only characterised by the structure of fibrous reinforcements using fibres of substantial or continuous length
B29C 65/08 - Joining of preformed partsApparatus therefor by heating, with or without pressure using ultrasonic vibrations
B29C 65/34 - Joining of preformed partsApparatus therefor by heating, with or without pressure using heated elements which remain in the joint, e.g. "verlorenes Schweisselement"
B29C 65/50 - Joining of preformed partsApparatus therefor using adhesives using adhesive tape
B29C 65/72 - Joining of preformed partsApparatus therefor by combined operations, e.g. welding and stitching
B29C 45/00 - Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mouldApparatus therefor
This specification discloses an article of manufacture and a process to make the same. The article of manufacture has a continuous thermoplastic matrix material and a thermoset matrix material comprised of oriented fibers. The thermoset matrix material is bonded to the thermoplastic matrix material at a bonded interface. The article of manufacture can take any number of forms for use in industries such as aircraft, automobiles, motorcycles, bicycles, trains or watercraft.
B32B 5/02 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by structural features of a layer comprising fibres or filaments
B29C 65/00 - Joining of preformed partsApparatus therefor
C08J 5/04 - Reinforcing macromolecular compounds with loose or coherent fibrous material
6.
REINFORCED STRUCTURAL COMPONENT AND PROCESS TO MAKE THE SAME
This specification discloses an article of manufacture and a process to make the same. The article of manufacture has a continuous thermoplastic matrix or a metal material and a thermoset matrix material comprised of oriented fibers. The thermoset matrix material is bonded to the thermoplastic matrix or metal material at a bonded interface. The article of manufacture can take any number of forms for use in industries such as aircraft, automobiles, motorcycles, bicycles, trains or watercraft.
B32B 15/08 - Layered products essentially comprising metal comprising metal as the main or only constituent of a layer, next to another layer of a specific substance of synthetic resin
B32B 5/02 - Layered products characterised by the non-homogeneity or physical structure of a layer characterised by structural features of a layer comprising fibres or filaments
7.
MOULDED FIBRE REINFORCED COMPOSITE BLANK WITH GUIDE HOLE
This specification discloses an article of manufacture. The article of manufacture has at least one structural blank and at least one guide. The structural blank has a plurality of oriented fiber plies in a thermoplastic matrix. The guide has a plurality of random dispersed fibers in a thermoplastic matrix. The guide is affixed to the structural blank by injection molding and over molding the guide onto the structural blank. The article of manufacture can take a number of forms for use in industries such as aircraft, automobiles, motorcycles, bicycles, trains or watercraft.
B29C 70/08 - Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, with or without non-reinforced layers
Disclosed in this specification is an article of manufacture comprising at least two longitudinal sections comprising a thermoplastic matrix of randomly dispersed carbon fibers forming the article of manufacture, with the structure reinforced by affixing a pad up of a thermoplastic matrix comprising oriented fibers to at least one of the longitudinal sections. The at least two longitudinal sections are assembled to form the article of manufacture by the interaction of adjoining structures on one longitudinal section with adjoining structures on the other longitudinal section.
B29C 65/02 - Joining of preformed partsApparatus therefor by heating, with or without pressure
B29C 65/48 - Joining of preformed partsApparatus therefor using adhesives
B29C 65/56 - Joining of preformed partsApparatus therefor using mechanical means
B29C 70/08 - Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, with or without non-reinforced layers
A47C 5/12 - Chairs of special materials of plastics, with or without reinforcement
A seat back frame (100) comprising a thermoplastic matrix of randomly dispersed carbon fibers forming the structure, with the structure reinforced by affixing a pad up (150) of a thermoplastic matrix comprising oriented fibers to the structure. And a method of manufacturing the seat back which comprises injection or overmolding the thermoplastic matrix comprised of randomly dispersed fibers onto the pad up (150) which is a compression molded oriented fibers in the thermoplastic matrix.
B29C 45/14 - Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mouldApparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles
B29C 70/08 - Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, with or without non-reinforced layers
10.
SYSTEM AND METHOD FOR FORMING THERMOPLASTIC-COMPOSITE TUBING
A system and method for forming thermoplastic-carbon fiber composite tubing is described. A non-continuous thermoplastic-carbon fiber composite sleeve capable of being formed into a tubular product, a method for forming a tubular product, and a tubular product fabricated from thermoplastic-carbon fiber composite is described. The sleeve may include at least one non-continuous thermoplastic fiber strand that may be interwoven with at least one carbon fiber. The method may include the steps of weaving the material into at least one sleeve to be processed, positioning a bladder within the sleeve to create a work piece, and placing the work piece in a mold. The mold may be heated and the bladder may be pressurized to form a tubular product. The resulting tubular product may be fabricated from thermoplastic carbon fiber composite with improved physical properties.
B29C 70/04 - Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
patents
