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
101	Diagnostic tool for repairing aircraft and method of using such a tool	US11480367	2006-07-05	US20070010923A1	2007-01-11	Francois Rouyre
A device according to the present invention comprises: a central unit (8) having access to a database (18) in which there are stored not only information on the aircraft fleet to be managed but also an aircraft repair manual, this central unit (8) having means of communicating with the outside, and in particular with a technical center (16) of at least one aircraft manufacturer, at least one portable device equipped with visual display means as well as with means of wireless communication between the said portable device and the central unit (8). Application to the analysis of damage observed in an aircraft during inspection thereof.
102	Modular trim paneling and outfitting system for an aircraft passenger cabin interior	US09882877	2001-06-15	US20020000491A1	2002-01-03	Jan Nieberle
An aircraft passenger cabin includes modular interior components selected from ceiling panels, wall panels, dado panels, window funnels, light covers, and baggage compartments or hat racks. At least one interior component is a standardized modular building block that can be used uniformly and interchangeably in different cabin configurations and sizes, in different aircraft types having different fuselage cross-sectional sizes and configurations. The interior components are modularly combined so as to be adapted to different passenger cabins in the various aircraft types. The multiplicity of distinct interior components among all aircraft types in the entire product range of an aircraft manufacturer is reduced, so that the piece count of each particular type of component is increased, and the manufacturing, installation, maintenance, replacement and inventorying costs are reduced. The time and cost for a new cabin design are reduced.
103	Diagnostic tool for repairing aircraft and method of using such a tool	US11480367	2006-07-05	US08401729B2	2013-03-19	François Rouyre
A device according to the present invention comprises: a central unit (8) having access to a database (18) in which there are stored not only information on the aircraft fleet to be managed but also an aircraft repair manual, this central unit (8) having means of communicating with the outside, and in particular with a technical center (16) of at least one aircraft manufacturer, at least one portable device equipped with visual display means as well as with means of wireless communication between the said portable device and the central unit (8). Application to the analysis of damage observed in an aircraft during inspection thereof.
104	Remote aircraft manufacturing, monitoring, maintenance and management system	EP08075973.1	2003-11-27	EP2042430A3	2009-06-10	Stovner, Steve R.; Gould, Todd W.; Reuter, Rick J.; Engdahl, Stanley W.; Parker, James M.
An aircraft wireless data communication system includes an aircraft computer/server in communication with a plurality of aircraft systems. Access to the aircraft systems via the computer/server is available in real-time via wireless communication with a ground-based computer system. The ground-based computer system includes a computer that can be accessed from one or more networks of computers. Each authorized computer user on an airline, manufacturer, or supplier network has remote real-time access to the aircraft computer/server. Properly authorized remote users can: perform comparisons between the aircraft actual configuration identity and an aircraft authorized configuration identity; perform system diagnostic testing; view system status and parameters; collaborate with users from local and remote organizations using real-time aircraft data; and upload and download software and data to and from aircraft systems.
105	Remote aircraft manufacturing, monitoring, maintenance and management system	EP08075973.1	2003-11-27	EP2042430A2	2009-04-01	Stovner, Steve R.; Gould, Todd W.; Reuter, Rick J.; Engdahl, Stanley W.; Parker, James M.
An aircraft wireless data communication system includes an aircraft computer/server in communication with a plurality of aircraft systems. Access to the aircraft systems via the computer/server is available in real-time via wireless communication with a ground-based computer system. The ground-based computer system includes a computer that can be accessed from one or more networks of computers. Each authorized computer user on an airline, manufacturer, or supplier network has remote real-time access to the aircraft computer/server. Properly authorized remote users can: perform comparisons between the aircraft actual configuration identity and an aircraft authorized configuration identity; perform system diagnostic testing; view system status and parameters; collaborate with users from local and remote organizations using real-time aircraft data; and upload and download software and data to and from aircraft systems.
106	Remote aircraft manufacturing, monitoring, maintenance and management system	EP07012627.1	2003-11-27	EP1840755A2	2007-10-03	Stovner, Steve R.; Gould, Todd W.; Reuter, Rick J.; Engdahl, Stanley W.; Parker, James M.
An aircraft wireless data communication system includes an aircraft computer/server in communication with a plurality of aircraft systems. Access to the aircraft systems via the computer/server is available in real-time via wireless communication with a ground-based computer system. The ground-based computer system includes a computer that can be accessed from one or more networks of computers. Each authorized computer user on an airline, manufacturer, or supplier network has remote real-time access to the aircraft computer/server. Properly authorized remote users can: perform comparisons between the aircraft actual configuration identity and an aircraft authorized configuration identity; perform system diagnostic testing; view system status and parameters; collaborate with users from local and remote organizations using real-time aircraft data; and upload and download software and data to and from aircraft systems.
107	MODULAR GALLEY UNIT INCLUDING BEVERAGE MAKER	PCT/US2008/054290	2008-02-19	WO2008103665A2	2008-08-28	CUNNINGHAM, Craig; DE TISI, Mark; BURD, Peter; WILSON, Jenny; RAMUS, Sebastien; ARNOLD, Geraldine; JOHNSON, Glenn
A galley unit comprising a plurality of mid-level modules and a plurality of high-level modules that are assembled together to form a modular galley unit, wherein at least one of the mid-level modules is a beverage maker unit. A combination comprising an aircraft and a modular galley unit, wherein at least one of the modules is a beverage maker unit.
108	Remote aircraft manufacturing, monitoring, maintenance and management system	EP03078744.4	2003-11-27	EP1426870A2	2004-06-09	Stovner, Steve R.; Gould, Todd W.; Reuter, Rick J.; Engdahl, Stanley W.; Parker, James M.
An aircraft wireless data communication system includes an aircraft computer/server in communication with a plurality of aircraft systems. Access to the aircraft systems via the computer/server is available in real-time via wireless communication with a ground-based computer system. The ground-based computer system includes a computer that can be accessed from one or more networks of computers. Each authorized computer user on an airline, manufacturer, or supplier network has remote real-time access to the aircraft computer/server. Properly authorized remote users can: perform comparisons between the aircraft actual configuration identity and an aircraft authorized configuration identity; perform system diagnostic testing; view system status and parameters; collaborate with users from local and remote organizations using real-time aircraft data; and upload and download software and data to and from aircraft systems.
109	BEVERAGE MAKER	PCT/US2007008081	2007-04-02	WO2007120460A2	2007-10-25	GHASSEMLOU PAUL; EISA VICTOR; SIDHU AMRIK S
The present invention provides a beverage maker having an in-line heating assembly for heating water to make hot beverages such as coffee and tea. The heating assembly defines a flow path that runs past a plurality of heaters for heating water to a desired temperature In this manner, the beverage maker heats water as it travels, alleviating the need for a water tank or vessel, resulting in increased savings in weight and size, as well as reducing brew time. Additionally, an optical sensor assembly is provided to detect when a serving container of the beverage maker has a prescribed capacity of liquid within it. The sensor assembly includes at least one light source aligned to shine into the container and at least one detector aligned to detect light reflected off the liquid surface within the container. A drainage assembly is also provided that can drain liquid through either a connector port into an airplane's wastewater system or through a drainage port into a drainage sump.
110	AMPHIBIOUS LARGE AIRCRAFT WITHOUT AIRSTAIRS	EP10748320.8	2010-03-01	EP2404826A1	2012-01-11	Liu, Shiying
An amphibious large aircraft without airstairs is provided. The fuselage (7) of the amphibious large aircraft is flat, and the shape of its bottom is rectangular. The longitudinal cross-section of the fuselage has a shape of the cross-section of a win, so the lift can be generated by the fuselage during flight, and the flight efficiency is increased by 30-40%. The fuselage has only one floor, wherein the passenger cabin (6) is set in the front of the fuselage, and the cargo hold (21) is mounted above the rear. The wings (8) are suspended towards two sides from upper side of the fuselage. A jet engine (30) is mounted above the rear of the fuselage and adjacent to the tail wing. Because landing gears (4, 9) can be lifted vertically and the landing gear wells (3, 10) mounted in the fuselage are provided with fore-and-aft sliding doors (32, 33), the fuselage can stop close to the ground. It is no need for the passenger to go on and off the aircraft via the airstairs and escape from the aircraft via the inflator slide in en emergency. It can be more convenient for the cargo to enter or exit the aircraft when the aircraft is used as a freight aircraft. Because the fuselage is flat, the gliding capability and the ground effect of the aircraft are better, and the aircraft can takeoff, land and cruise on the wide water. The full-length, wingspan and height of the aircraft are all reduced by 25-30% compared with the current aircraft of the same scale, thus the floor space and the investment of the manufacturer, the maintenance factory, the garage and the aerodrome are all reduced.
111	METHOD AND APPARATUS FOR DETERMINING AIRCRAFT PERFORMANCE	PCT/US1991001874	1991-03-26	WO1991014931A1	1991-10-03	B A ASSOCIATES, INC.; PALM, Michael, Jay; CUPAL, Jerry, J.
Apparatus for providing information to a pilot about the weight and balance and the flight characteristics of an aircraft (2) includes a weighing pad (4) for each landing gear strut of the aircraft (2). The pads (4) transmit coded signals representing the weights to an onboard computer (6) which decodes the signals, calculates several factors, and displays the results. The computer (6) is programmed with equations which fit the performance curves for the aircraft and supplied by the aircraft manufacturer. In one embodiment, the signals are transmitted to the computer (6) through a conductor. In another embodiment, the signals are broadcast to an onboard radio receiver (38) by a digital radio transmitter (32).
112	AIRCRAFT GALLEY	PCT/US2012/030989	2012-03-28	WO2012135371A1	2012-10-04	CUNNINGHAM, Craig; RAMUS, Sebastien A.; PETRY, Sebastian; PIRIE, Christopher I.; BLAAUWHOF, Michiel
An aircraft galley includes a beverage center including one or more hot beverage makers, and one or more combination oven-chiller units for multiple replaceable meal carrier rotables. The beverage center may also include an espresso maker, a milk frothing device, a hot water dispenser, a pull out drip tray, drain pan or sink, and a control panel. The aircraft galley also includes a main work deck with a sliding, pull-out work deck portion, and may include one or more pull-out combination drain-sink drawers including one or more individual drain-sinks
113	Procédé et dispositif pour réaliser un contrôle de santé d'un turbomoteur d'un aéronef pourvu d'au moins un turbomoteur	EP12008238.3	2012-12-10	EP2623748A1	2013-08-07	Camhi, Emmanuel; Borchers, Guido
La présente invention concerne un procédé pour réaliser automatiquement un contrôle de santé moteur d'au moins un turbomoteur d'un aéronef. Durant le vol, on vérifie la stabilité d'au moins un paramètre de surveillance en acquérant un signal de mesure, en effectuant un premier filtrage par un filtre passe haut de chaque signal sur une première durée (TPS1) longue et en vérifiant qu'une première amplitude (A1) du signal ainsi filtré ne dépasse pas un premier seuil défini par le constructeur, en effectuant un deuxième filtrage par un filtre passe haut de chaque signal sur une deuxième durée (TPS2) courte en parallèle dudit premier filtrage par un filtre passe haut, et en vérifiant qu'une deuxième amplitude (A2) du signal ainsi filtré ne dépasse pas un deuxième seuil défini par le constructeur, la deuxième durée (TPS2) étant inférieure à la première durée (TPS1), la deuxième amplitude (A2) étant inférieure à la première amplitude (A1).
114	Flight-management computer smoothing an aircraft path over several sequences	US10169079	2002-07-08	US20030088360A1	2003-05-08	Yann Ikhlef; Patrick Daouphars
The computer according to the present invention makes it possible to compute the transitions between the legs of an aircraft flight plan without discontinuity of trajectory on the basis of the aircraft manufacturer's routines for computing standardized transitions, doing so over an unlimited number of legs. The reliability of the computer is greatly increased thereby.
115	COFFEE MAKER WATER HEATER	PCT/US2013/059183	2013-09-11	WO2014043185A1	2014-03-20	JIMENEZ, Marcos
Embodiments of the present invention provide improved heating methods for use in coffee makers and other beverage makers that use hot water for various beverages and other purposes. These improvements find particular use on-board aircraft or other passenger transport vehicles, where quick heating and reduced power consumption are particularly desirable and beneficial. Further embodiments also relate to improved water level sensing, improved water reservoirs, and improved carafe features.
116	군용기용 메인 랜딩기어 휠의 드라이브 인서트 보스부 가공방법 및 그 장치	KR1020140118931	2014-09-05	KR101486508B1	2015-01-27	이한규
본 발명은 군용기용 메인 랜딩기어 휠의 드라이브 인서트 보스부 가공방법 및 그 장치에 관한 것으로, 보다 상세하게는 가공하고자 하는 메인 랜딩기어 휠을 턴테이블의 상부에 장착되는 클램핑베이스의 상면에 베어링컵이 위로 향하도록 안착시켜 클램핑한 후, 클램핑된 메인 랜딩기어 휠의 상부로부터 커터홀더의 하단부에 장착되는 凹자형상의 절삭커터를 수직으로 상하운동시켜 메인 랜딩기어 휠의 드라이브 인서트 보스부를 절삭가공하도록 구성함으로써, 해외 제작사에 의존하던 군용기용 메인 랜딩기어 휠의 오버홀을 국내에서 수행할 수 있게 하므로 정비 국산화를 실현하여 막대한 외화유출을 방지할 수 있도록 할 뿐만 아니라, 해외수리시 6개월 이상 소요되었던 수리순환품목의 제공기간을 45일 이내로 획기적으로 단축하여 전시 작전태세� �지를 위한 예비품의 수량을 감소시켜 국방비를 대폭 절감할 수 있도록 하는 군용기용 메인 랜딩기어 휠의 드라이브 인서트 보스부 가공방법 및 그 장치에 관한 것이다.
117	COFFEE MAKER WATER HEATER	EP16189996.8	2016-09-21	EP3150091A1	2017-04-05	Jimenez, Marcos
Embodiments of the present invention provide improved heating methods for use in coffee makers and other beverage makers that use hot water for various beverages and other purposes. These improvements find particular use on-board aircraft or other passenger transport vehicles, where quick heating and reduced power consumption are particularly desirable and beneficial. Further embodiments also relate to improved water level sensing, improved water reservoirs, and improved carafe features.
118	Extensible and Scalable Distributed Computing and Communication Remote Services Platform for Telemetry Collection Adaptive Data Driven Application Hosting, and Control Services	US13615467	2012-09-13	US20140075506A1	2014-03-13	Terry L. Davis; Brian Marquardt; Miles B. Miller; David E. Wall; Michelle Selberg; Paul G. Mallasch
A global, broadband communications and computing system Platform for commercial aircraft selects a “current best” communication link from multiple available links. Onboard network access components, such as Wi-Fi and GSM pico-cells, enable wired/wireless devices to use the aircraft's broadband communications links. The Platform uses virtualization and distributed systems computing technology to create a system of systems that extends an airline company's ground communications and computing systems server(s) onboard aircraft in the fleet, regardless of model, age, or manufacturer. The Platform can host airline operational applications and services onboard the aircraft. An onboard system collects data from multiple aircraft systems, tags it with trusted time and origin metadata, and securely transmits it to a ground portion of the Platform in real time (or as links are available), and receives data for distribution to appropriate onboard systems. Core components on an aircraft are not affected by operation of the Platform.
119	Modular aerospace plane	US11007855	2004-12-09	US07234667B1	2007-06-26	Robert N. Talmage, Jr.
This invention relates to the design of a Modular Aerospace Plane (MAP) comprising a forward fuselage section, a main wing section, a tail section and wing attachments. Various sections can be integrated to offer a variety of aircraft characteristics, performance and missions. This modular design offers a new method of aircraft fabrication, maintenance, repair and ground handling to reduce costs for the manufacturers, owners and operators. The forward fuselage and tail sections may utilize a parachute device whereby these sections can separate in an emergency and safely lower the occupants to the ground.
120	적어도 하나의 터빈 엔진을 가지는 항공기의 터빈 엔진의 건강 검사를 수행하기 위한 방법 및 장치	KR1020130013618	2013-02-06	KR1020130090849A	2013-08-14	까미,엠마뉘엘
PURPOSE: A method and apparatus for inspecting the health of at least one turbine engine in an aircraft are provided to optimize health inspection for the turbine engine of the rotary wing aircraft and to easily track the health inspection. CONSTITUTION: A method for inspecting the health of at least one turbine having a gas generator and a turbine assembly having at least one turine in order to monitor an air craft having a rotary wing (300) includes: an obtaining step (STP1) for health inspection of stabilizing the aircraft, and obtaining the monitoring value of at least one monitoring parameter for the turbine engine; and an evaluating step (STP2) for the health inspection of determining at least one operation margin for the turbine engine with comparing the monitoring value with a limit value regulated by a manufacturer. In a generation step (STP0) before the obtaining step and the evaluating step, an effect in mounting the turbine engine in the aircraft is evaluated by multiple test values for the reduced rotational velocity of the gas generator. The reduced rotational velocity is identical to the reduced rotational velocity of the gas generator adjusted by external temperature at the periphery of the aircraft. The test values are in a range from a minimum test value to a maximum test value.

1 2 3 4 5 6 7 8 9 10

IPRDB

热门服务

关于我们

友情链接

联系方式