飞机制造商相关的专利数据

序号	专利名	申请号	申请日	公开（公告）号	公开（公告）日	发明人
161	"The shoe fly" - multi-purpose shoe carrier	US10857171	2004-06-01	US20060180484A1	2006-08-17	Angela Jones
“The Shoe Fly” Multi-Purpose Shoe Carrier is a revolutionary piece of luggage designed specifically to address the problem of travel with multiple pairs of shoes. Up to this point, luggage manufacturers have tried to address this problem by adding a pocket or two to a standard piece of luggage or by including separate shoe bags with the standard suitcase. The “Shoe Fly” can be carried on to planes, trains, buses etc. for convenience, and can also transport other accessories. Larger versions of the “Shoe Fly can be used in the fashion, theatre, movie and television industries where several pairs of shoes or various accessories may be needed.
162	Manual processing system	US09948764	2001-09-10	US20020032707A1	2002-03-14	Makoto Takeoka
A system is provided for processing a manual such as a maintenance manual of an airplane into a customized manual to provide a user with the manual. The document processing unit inserts insertion data in a manual document by referring to a manufacturer's additional dictionary, a user's additional dictionary, and a translation sentence insertion dictionary. Also, the data conversion unit implements a predetermined processing such as providing a layout to the manual document. Thereby, the system provides a manual of which contents and format are customized to a user company, in either electronic or paper-printed information.
163	Verfahren zur Verwaltung von zu überprüfenden Geräten der Luftfahrtindustrie	EP00109574.4	2000-05-05	EP1151920A1	2001-11-07	Odemann, Christian, Dr. rer.pol.
Gemäß der Erfindung werden teure und technisch hochwertige Geräte (11a, 11b) der Luftfahrtindustrie, welche zum Beispiel bei bestimmten Checks der Flugzeuge überholt und/oder neu kalibriert beziehungsweise zertifiziert werden müssen, mit einem Radiofrequenz Transponder (RFT und/oder bar code) mit oder ohne Kryptographie) (15a, 15b) versehen, welcher eine individuelle Kennung des Gerätes (11a, 11b) maschinenlesbar enthält. Die Zustandsdaten jedes Gerätes werden dann unter dieser Kennung in einer zentralen Datenbank (13) beim Hersteller (12) gespeichert und können bei entsprechender Autorisierung fernabgefragt werden. Hierdurch ist es möglich, den Versand der Geräte ohne Begleitpapiere vorzunehmen und die logistische Zuteilung zu optimieren.
164	Duroplastische Harzmasse und ihre Verwendung	EP83109064.2	1983-09-14	EP0134298A1	1985-03-20	Kümmel, Robert
@ Die Erfindung betrifft eine duroplastiche, härtbare, flammhemmend und selbstverlöschend ausgerüstete Harzmasse auf Basis eines üblichen Aminoplasts oder Reaktionsharzes, das gegebenenfalls ein übliches Kalt- oder Warmhärtersystem enthält und durch einen Gehalt an Melaminborat gekennzeichnet ist, sowie die Verwendung dieser Harzmasse zur Herstellung lagerfähiger Prepregs, zur Imprägnierung und Beschichtung von Filamentgeweben, insbesondere aus Glas-, Kohlenstoff- und Poly-p-phenylenterephthalamid-Fasern, sowie zur Herstellung schwerentflammbarer Laminate und Formkörper, insbesondere für die Luft- und Raumfahrtindustrie.
165	Cargo handling and transportation system	US23522972	1972-03-16	US3802354A	1974-04-09	BATESON N; PRINGLE W
A cargo handling and transportation system includes a truss type of frame on which vehicles are suspended upon leaving the manufacturer''s assembly line. The frame is connected to a longitudinal beam which moves in a track and transports the vehicles from the factory to a means of ground or highway transportation. In loading a railway car, the truss and vehicles thereon are removed from the longitudinal beam by a crane and are lowered through the open roof of the car into connecting relation with brackets disposed within the car so that the frame and cargo are ready for shipment. Similarly, the truss frames may be removed from the highway trailers or railway cars by lift mechanisms which shift the frames into aircraft or into holds of ships for further transportation. The longitudinal beams are movable in tracks below the ground, and may be removably connected to the lower ends of the truss to be transported therewith so that they may be guided in suitable track members in a ramp loading arrangement, such as may be desired for loading aircraft. The frames also may be stored within the hull of a ship or airplane fuselage in similar tracks which are engaged by the longitudinal beams removably connected to the lower ends of the truss frame.
166	Cargo handling and transportation system	US3677192D	1970-08-21	US3677192A	1972-07-18	BATESON NORMAN E; PRINGLE WILLIAM L
A cargo handling and transportation system includes a truss type of frame on which vehicles are suspended upon leaving the manufacturer''s assembly line. The frame is connected to a longitudinal beam which moves in a track and transports the vehicles from the factory to a means of ground or highway transportation. In loading a railway car, the truss and vehicles thereon are removed from the longitudinal beam by a crane and are lowered through the open roof of the car into connecting relation with brackets disposed within the car so that the frame and cargo are ready for shipment. Similarly, the truss frames may be removed from the highway trailers or railway cars by lift mechanisms which shift the frames into aircraft or into holds of ships for further transportation. The longitudinal beams are movable in tracks below the ground, and may be removably connected to the lower ends of the truss to be transported therewith so that they may be guided in suitable track members in a ramp loading arrangement, such as may be desired for loading aircraft. The frames also may be stored within the hull of a ship or airplane fuselage in similar tracks which are engaged by the longitudinal beams removably connected to the lower ends of the truss frame.
167	GPS/sonar display mounting assembly	US14196252	2014-03-04	US09346414B1	2016-05-24	Steven Randy Kuhens
A GPS/sonar display mounting assembly is provided which is mountable to a dashboard console of a vehicle, which may include but is not limited to boat, automobile, aircraft or the like. The mounting structure provides that mounting assembly may be utilized with displays and GPS/sonar equipment of various manufacturers while being adjustable in at least three directions to allow for comfortable use of the display by a user. Further, the mounting assembly provides for retention of the display in a desired position once set by the user despite choppy conditions which typically cause prior art mounting assemblies to slip and move from a preferred position.
168	UNIVERSAL ESPRESSO MAKER	US13480588	2012-05-25	US20120297987A1	2012-11-29	THOMAS M. LEE; ABDELAZIZ BOUBEDDI; TIMOTHY C. MORSE
Embodiments of the present invention relate generally to an espresso or other coffee drink maker that is configured to accept a number of different forms of coffee grounds. It may accept powder/coffee grounds that are loose, coffee capsules, coffee pods, (e.g., “ESE” (easy serving espresso) pods), or any other format. The machine may also be provided with an optional built-in grinder, which allows the machine to accept fresh coffee beans, in order to grind and brew them on-site, in a single machine. Such espresso/coffee drink makers find particular use on-board passenger transport vehicles such as aircraft, but may be useful in a number of other locations.
169	Portable electric cutting and scoring saw	US745412	1991-08-15	US5159870A	1992-11-03	Paul E. Fiala
A portable electric cutting and scoring saw for use on laminated or veneer products is disclosed. The scoring saw is disposed in front of the cutting saw and turns in the opposite direction. The saw is designed primarily for an on-the-job cabinet maker where the use of large industrial bench saws are not feasible. The scoring saw cuts at a fixed depth and the cutting saw depth of cut can be varied by changing the blade with a different diameter. The laminate or veneer to be cut is bonded to the workpiece and the scoring saw eliminates chipping of the laminate or veneer. The scoring saw and the cutting saw lie in the same plane.
170	Aluminium alloy products suited for commercial jet aircraft wing members	EP96306602.2	1996-09-11	EP0829552A1	1998-03-18	Miyasota, Shelly M.; Bray, Gary H.; Liu, John; Staley, James T.
Rolled plate products up to 6 inches thick or more and other products in an aluminum alloy consisting essentially of about 5.2 to 6.8% zinc, 1.7 to 2.4% copper, 1.6 to 2% magnesium, 0.03 to 0.3% zirconium, balance substantially aluminum and incidental elements and impurities, are useful in making structural members for commercial airplanes especially by machining or shaping such members from the plate. Such members include lower wing skins (18) and wing spars (20) and other members. The plate is made by operations comprising homogenization, hot rolling, solution heat treatment, stretching and artificial aging. Alternatively, the plate is shaped after stretching, which may include machining, and is then artificially aged.
171	ALUMINIUM ALLOY PRODUCTS HAVING IMPROVED PROPERTY COMBINATIONS AND METHOD FOR THEIR PRODUCTION	PCT/US2008006253	2008-05-14	WO2008156532A3	2009-01-29	BRAY GARY H; CHAKRABARTI DHRUBA J; DENZER DIANA K; LIN JEN C; NEWMAN JOHN; VENEMA GREGORY B; YANAR CAGATAY; BOSELLI JULIEN
Aluminum alloy products about 4 inches thick or less that possesses the ability to achieve, when solution heat treated, quenched, and artificially aged, and in parts made from the products, an improved combination of strength, fracture toughness and corrosion resistance, the alloy consisting essentially of: about 6.8 to about 8.5 wt.% Zn, about 1.5 to about 2.00 wt.% Mg, about 1.75 to about 2.3 wt.% Cu; about 0.05 to about 0.3 wt. % Zr, less than about 0.1 wt. % Mn, less than about 0.05 wt.% Cr, the balance Al, incidental elements and impurities and a method for making same. The instantly disclosed alloys are useful in making structural members for commercial airplanes including, but not limited to, upper wing skins and stringers, spar caps, spar webs and ribs of either built-up or integral construction.
172	DEVICE FOR DETECTING THE USE OF A BELT AND THE SERVICE LIFE OF THE RESTRAINT SYSTEMS	PCT/DE2001/000611	2001-02-02	WO01064485A1	2001-09-07
The invention relates to a device which supplies a definite proof of the passengers who have not fastened the belt. Said proof discharges the car manufacturer, aircraft manufacturer or the airline company from the claim for compensation and from paying the cost of treatment. The inventive device detects the moment of the accident and the moments of several collisions or several turbulences. The accident data, impact detection elements of the security belts, display lamps and/or security devices provide signs of proof in the case of any accident, regardless if the passengers had fastened their security belts or not. The aim of the invention is to detect the service life. The device detects how often belts have been used, drawn-out and/or detects the number of blockings. When the service life is exceeded, the warning lamp flashes and/or the multi-info display (screen) indicates that exchange of the security belts, belt retractors and/or clamping devices is required. It can thus be detected who is responsible for the failure of the restraint systems.
173	Threaded insert for receiving a threaded fastener in a composite panel	US12152722	2008-05-16	US20080292425A1	2008-11-27	Victor Pineiros; Wilhelm Schepergerdes
A threaded insert for use in a composite and/or honey-comb matrix has a nut member disposed within a plastic housing. The threads of the nut member have a free running thread section and a thread lock section. When a fastener is made up into the nut member, a surface on the nut member engages an opposite-facing surface on the plastic housing, thereby reversing the nut loading from tensile loading to compression loading. A thermoplastic embodiment of the nut member may be fabricated to meet the specifications of aircraft manufacturers required for the SL2334 insert, including thread reusability, tensile loading (pullout load), shear, and interchangeability with the metal component currently in use.
174	Method for the management of aeronautical industry implements to be checked	US10869205	2004-06-16	US20040236755A1	2004-11-25	Christian Odemann
According to the invention, expensive and technical high-quality implements (ha, lIb) of the aeronautical industry which, for certain checks of the airplanes, must be overhauled and/or new calibrated or certified, are provided with a radio frequency transponder (RFT and/or bar code) with or without cryptography (ISa, 15b) which contains an individual machine readable identification characteristic of the implement (ii a, ii b). The status data of each implement are stored at the manufacturer's under this identification characteristic in a central data bank (13) and can be remote called with a corresponding authorization. Thus, it is possible to carry out the sending of the implements without accompanying documents and to optimize the logistic allotment.
175	Display apparatus, control support system, and display method	US13806589	2011-06-24	US09233761B2	2016-01-12	Koichi Yamasaki
A flight path maker (FPM) and a target attitude relative to air display are displayed on a primary flight display (PFD), which is an integrated indicator. The target attitude relative to air display is a mark indicating a target attitude relative to air representing a target angle-of-attack and a target sideslip angle of the aircraft to achieve a target flight path. The PFD displays the relative difference between the FPM and the target attitude relative to air display and shows that the aircraft is flying in the target traveling direction when the FPM matches (is superposed on) the target attitude relative to air display. Thus, controlling with higher trackability than controlling performed based on a target attitude relative to ground is enabled.
176	Aluminum alloy products suited for commercial jet aircraft wing members	US451643	1995-05-26	US5865911A	1999-02-02	Shelly M. Miyasato; Gary H. Bray; John Liu; James T. Staley
Rolled plate products up to 6 inches thick or more and other products in an aluminum alloy consisting essentially of about 5.2 to 6.8% zinc, 1.7 to 2.4% copper, 1.6 to 2% magnesium, 0.03 to 0.3% zirconium, balance substantially aluminum and incidental elements and impurities, are useful in making structural members for commercial airplanes especially by machining or shaping such members from the plate. Such members include lower wing skins and wing spars and other members. The plate is made by operations comprising homogenization, hot rolling, solution heat treatment, stretching and artificial aging. Alternatively, the plate is shaped after stretching, which may include machining, and is then artificially aged.
177	Universal espresso maker	US13480588	2012-05-25	US09101243B2	2015-08-11	Thomas M. Lee; Abdelaziz Boubeddi; Timothy C. Morse
Embodiments of the present invention relate generally to an espresso or other coffee drink maker that is configured to accept a number of different forms of coffee grounds. It may accept powder/coffee grounds that are loose, coffee capsules, coffee pods, (e.g., “ESE” (easy serving espresso) pods), or any other format. The machine may also be provided with an optional built-in grinder, which allows the machine to accept fresh coffee beans, in order to grind and brew them on-site, in a single machine. Such espresso/coffee drink makers find particular use on-board passenger transport vehicles such as aircraft, but may be useful in a number of other locations.
178	Method for the management of aeronautical industry implements to be checked	US10869205	2004-06-16	US07496587B2	2009-02-24	Christian Odemann
According to the invention, expensive and technical high-quality implements (11a, 11b) of the aeronautical industry which, for certain checks of the airplanes, must be overhauled and/or new calibrated or certified, are provided with a radio frequency transponder (RFT and/or bar code) with or without cryptography (15a, 15b) which contains an individual machine readable identification characteristic of the implement (11a, 11b). The status data of each implement are stored at the manufacturer's under this identification characteristic in a central data bank (13) and can be remote called with a corresponding authorization. Thus, it is possible to carry out the sending of the implements without accompanying documents and to optimize the logistic allotment.
179	DEVICE FOR DETECTING THE USE OF A BELT AND THE SERVICE LIFE OF THE RESTRAINT SYSTEMS	PCT/DE0100611	2001-02-02	WO0164485B1	2001-12-13	GO GIOK DJIEN
The invention relates to a device which supplies a definite proof of the passengers who have not fastened the belt. Said proof discharges the car manufacturer, aircraft manufacturer or the airline company from the claim for compensation and from paying the cost of treatment. The inventive device detects the moment of the accident and the moments of several collisions or several turbulences. The accident data, impact detection elements of the security belts, display lamps and/or security devices provide signs of proof in the case of any accident, regardless if the passengers had fastened their security belts or not. The aim of the invention is to detect the service life. The device detects how often belts have been used, drawn-out and/or detects the number of blockings. When the service life is exceeded, the warning lamp flashes and/or the multi-info display (screen) indicates that exchange of the security belts, belt retractors and/or clamping devices is required. It can thus be detected who is responsible for the failure of the restraint systems.
180	Dispositif et procédé de régulation d'un turbomoteur, et aéronef	EP12008276.3	2012-12-12	EP2623750A1	2013-08-07	Beaud, Southdary; Martin, Laurent
Dispositif de régulation (10) pour réduire les risques de pompage d'un turbomoteur (3) comportant un générateur de gaz (4), un moyen de prélèvement d'air (8) et un moyen de prélèvement mécanique (100) d'énergie. Un calculateur moteur (11) comporte un moyen de stockage (16) mémorisant une pluralité de lois de régulation en accélération, chaque loi de régulation en accélération correspondant à une plage de prélèvement d'air et à une plage de prélèvement mécanique, ledit dispositif de régulation (10) comportant un moyen de mesure (20) d'un prélèvement d'air courant et un moyen de mesure (30) d'un prélèvement mécanique courant, ledit calculateur moteur (11) contrôlant une accélération du turbomoteur (3) en mettant en oeuvre la loi de régulation en accélération correspondant au prélèvement d'air courant et au prélèvement mécanique courant.

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