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
141	Aircraft maintenance records server	US10952038	2004-09-27	US20050055239A1	2005-03-10	Grace Farmer
An apparatus and method for an aircraft maintenance server includes a system in which an electronic package is created for delivery to the maintenance personnel. The electronic package includes all of the specific maintenance process tasks that must be performed to satisfy local, international governmental regulations as well as operator and aircraft manufacturer defined procedures. Additionally, the electronic package includes a list of parts that will be required for the specified tasks and, optionally, a flow chart illustrating the overall process.
142	COFFEE MAKER WATER HEATER	US14862691	2015-09-23	US20160007798A1	2016-01-14	Marcos Jimenez
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.
143	Method and apparatus for managing aircraft maintenance records	US10142200	2002-05-09	US06885921B1	2005-04-26	Grace H. Farmer
An apparatus and method for an aircraft maintenance server includes a system in which an electronic package is created for delivery to the maintenance personnel. The electronic package includes all of the specific maintenance process tasks that must be performed to satisfy local, international governmental regulations as well as operator and aircraft manufacturer defined procedures. Additionally, the electronic package includes a list of parts that will be required for the specified tasks and, optionally, a flow chart illustrating the overall process.
144	Procédé et dispositif pour réaliser un contrôle de l'état de santé d'un turbomoteur d'un aéronef pourvu d'au moins un turbomoteur	EP12008023.9	2012-11-29	EP2623747A1	2013-08-07	Camhi, Emmanuel
La présente invention concerne un procédé pour réaliser un contrôle de santé d'au moins un turbomoteur (3). Durant une étape de développement (STP0), on quantifie des effets d'avionnage dudit aéronef (1) pour une pluralité de valeurs d'essais d'une vitesse de rotation réduite (Ng') d'un générateur de gaz (4) du turbomoteur. Durant une étape d'acquisition (STP1), on augmente la vitesse de rotation dudit générateur de gaz (4) jusqu'à ce que ledit turbomoteur développe une puissance maximale, puis on réduit ladite vitesse de rotation du générateur de gaz (4) jusqu'à ce que la vitesse de rotation réduite (Ng') atteigne une valeur d'essais. On stabilise l'aéronef et on effectue l'acquisition d'au moins une valeur de surveillance. Durant une étape d'évaluation (STP2) du contrôle de santé, on détermine au moins une marge de fonctionnement en utilisant une valeur de surveillance et les effets d'avionnage.
145	Retaining member and method for use with a seat track	US11376682	2006-03-15	US07448822B2	2008-11-11	Michael O Nebeker; Matthew S Olson; Anthony E Anderson; James E Ebner
A retaining component for securing an external structure or panel to a seat track within a mobile platform, such as an aircraft. The retaining component includes a pair of flexible flanges that are adapted to engage an external component or panel, in one example a seat track in a commercial aircraft cabin area. The retaining component also includes a base portion having a flexible portion with at least one locking tab protruding therefrom. One or more hook-shaped engaging tabs also protrude from the base portion. The engaging tabs and the locking tab enable the retaining component to be secured to a flange of a seat track having a plurality of spaced apart holes in a manner that does not require any external threaded or rivet style fastening elements, or the use of separate assembly tools. The retaining component, in one form, is a single piece, lightweight, integrally formed component that is ideally suited for use in mobile platforms such as commercial aircraft where assembly time and costs are important considerations in the manufacture of a commercial aircraft.
146	Retaining member and method for use with a seat track	US11376682	2006-03-15	US20070215769A1	2007-09-20	Michael Nebeker; Matthew Olson; Anthony Anderson; James Ebner
A retaining component for securing an external structure or panel to a seat track within a mobile platform, such as an aircraft. The retaining component includes a pair of flexible flanges that are adapted to engage an external component or panel, in one example a seat track in a commercial aircraft cabin area. The retaining component also includes a base portion having a flexible portion with at least one locking tab protruding therefrom. One or more hook-shaped engaging tabs also protrude from the base portion. The engaging tabs and the locking tab enable the retaining component to be secured to a flange of a seat track having a plurality of spaced apart holes in a manner that does not require any external threaded or rivet style fastening elements, or the use of separate assembly tools. The retaining component, in one form, is a single piece, lightweight, integrally formed component that is ideally suited for use in mobile platforms such as commercial aircraft where assembly time and costs are important considerations in the manufacture of a commercial aircraft.
147	Aircraft engine reliability business model	US10346844	2003-01-15	US06643570B2	2003-11-04	Barry Bangert; Ralph Hawkins
A business model algorithm for maintaining aircraft engines in reliable and safe operating condition without the necessity of performing major engine overhaul in which engine manufacturers' maintenance procedures are enhanced and performed more frequently and supplemented by engine trend analysis, engine oil analysis, engine vibration analysis, borescope inspection and computer algorithm forecasting to identify, repair, and/or replace engine components without necessity of major engine overhaul.
148	Measurement of contaminant components in exhaust gas and reduction of excessive contaminant emissions during cold starts and while driving	US09647313	2000-09-27	US06532793B1	2003-03-18	Michael Palocz-Andresen
This invention pertains to the emission control in motor vehicles but also in ships, airplanes and diesel locomotives. The control system may either be fitted into new vehicles by the manufacturer or be retrofitted by the driver in older vehicles. An adsorption system serves to reduce the vehicle emissions during the cold-start period, in case of malfunctions in the engine or in the exhaust gas after-treatment system and in times of high quantities of pollutants in the atmosphere. To regenerate the adsorbent masses, the pollutants will be desorbed, introduced into the combustion chamber and burned.
149	Aircraft fuel loading management system	US818786	1986-01-14	US4819183A	1989-04-04	Edward M. O'Brien; Donald R. Otto
A computer-controlled aircraft fuel loading management system is disclosed. The system measures fuel loading volumetrically using flow meter devices and gravimetrically using information relating to the density (specific gravity) of the fuel being loaded entered prior to a fuel loading operation, changes in the temperature of the fuel being loaded and stored information relating to the densities (specific gravities) of a number of fuels and changes thereto with temperature which are derived from American Petroleum Institute information. The system automatically computes and displays the distribution of fuel by tank from stored aircraft tank and fuel load distribution information derived from aircraft manufacturer information. The system also converts a total fuel volume as measured by the system to a standardized fuel volume normalized to a given temperature, for example 60.degree. F.
150	PARTS MANUFACTURING METHODS, SYSTEMS AND USES	US12816668	2010-06-16	US20100319502A1	2010-12-23	Arthur Harrison
A method for manufacturing a part selected from a plurality of part types is disclosed. The method involves the step of selecting, from a supply of workpieces, a workpiece of a type that is associated with the type of part selected, the workpiece having a void and a substantially annular outer surface. Using a lathe, the selected workpiece is machined into the selected part. The workpiece, during the machining step, is mounted to the lathe by a collet associated with the type of part selected. The collet is an expanding collet which, during machining, is received by the void and engages the workpiece in gripping relation. The part can be a bushing for an aircraft landing gear and the workpiece can be an oversized bushing. The method can be carried out at an aircraft repair facility and the oversized bushings can be procured from specialist fabricators.
151	최적화된 외부 가시성을 구비한 조종실을 가지는 항공기와 방법	KR1020140029871	2014-03-13	KR1020140117276A	2014-10-07	보드리장-피에르; 서튼니콜라스
The present invention relates to an aircraft having a control compartment including a canopy provided with transparent surfaces fixed at bars; a central console; and two seats provided horizontally at one side of the central console. The aircraft includes at least one support (31, 33) connected to the central console; and at least one display unit to display multiple signs to help the operation of the aircraft. Each of the display units is supported by at least one support (31, 32, 33, 34) positioned between a theoretical position of eyes of a person sitting at one of the two seats and the bar. Each of the supports (31, 32, 33, 34) visually covers at least partially the bar to optimize visibility outside the control compartment to be used by people, and the theoretical position is determined by a manufacturer.
152	BEVERAGE MAKER	US11695538	2007-04-02	US20070272085A1	2007-11-29	Paul Ghassemlou; Victor Eisa; Amrik Sidhu
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.
153	Method and a device for performing a check of the health of a turbine engine of an aircraft provided with at least one turbine engine	US13737260	2013-01-09	US09222412B2	2015-12-29	Emmanuel Camhi; Guido Borchers
A method of automatically performing an engine health check for checking the health of at least one turbine engine of an aircraft. During flight, the stability of at least one monitoring parameter is verified by acquiring a measurement signal, by performing first filtering of each signal by a high-pass filter over a long first duration (TPS1) and by verifying that a first amplitude (A1) of the signal filtered in this way does not exceed a first threshold defined by the manufacturer, by performing second filtering of each signal by a high-pass filter over a short second duration (TPS2) in parallel with said first filtering by a high-pass filter, and by verifying that a second amplitude (A2) of the signal filtered in this way does not exceed a second threshold defined by the manufacturer, the second duration (TPS2) being less than the first duration (TPS1), and the second amplitude (A2) being less than the first amplitude (A1).
154	Beverage maker	US11695538	2007-04-02	US07861644B2	2011-01-04	Paul Ghassemlou; Victor Eisa; Amrik S. Sidhu
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.
155	METHOD AND A DEVICE FOR PERFORMING A CHECK OF THE HEALTH OF A TURBINE ENGINE OF AN AIRCRAFT PROVIDED WITH AT LEAST ONE TURBINE ENGINE	US13737260	2013-01-09	US20130199204A1	2013-08-08	Emmanuel Camhi; Guido Borchers
A method of automatically performing an engine health check for checking the health of at least one turbine engine of an aircraft. During flight, the stability of at least one monitoring parameter is verified by acquiring a measurement signal, by performing first filtering of each signal by a high-pass filter over a long first duration (TPS1) and by verifying that a first amplitude (A1) of the signal filtered in this way does not exceed a first threshold defined by the manufacturer, by performing second filtering of each signal by a high-pass filter over a short second duration (TPS2) in parallel with said first filtering by a high-pass filter, and by verifying that a second amplitude (A2) of the signal filtered in this way does not exceed a second threshold defined by the manufacturer, the second duration (TPS2) being less than the first duration (TPS1), and the second amplitude (A2) being less than the first amplitude (A1).
156	METHOD FOR LOCATING AIRCRAFT WIRING	PCT/EP2011061308	2011-07-05	WO2012004260A3	2012-06-07	BIGOT PHILIPPE; KIM SEBASTIEN; PERJU CATALIN
The invention relates to a method for locating the wiring in an aircraft provided with a harness database (11) containing data relating to the aircraft wiring, said method comprising the following steps: placing a set of radio frequency markers (7) on a harness (3a) of the wiring in pre-determined positions in order to mark said positions in relation to the harness, each of the radio frequency markers (7) being identified by a unique identifier; reading the identifiers of the radio frequency makers along the length of the harness (3a); and recording said identifiers in the harness database (11), linking same to the relative positions of the radio frequency markers (7) on the harness (3a), the radio frequency markers (7) and the database (11) being configured to be interfaced with one another via a read means.
157	Combi-supersonic-adjusting-nozzle	EP06005007.7	2006-03-11	EP1710426A2	2006-10-11	Kaniut, Herbert Maximilian
The filed application is a supplement to a basic conception for a novel internal combustion engine with the name:, Injector-Centrifuge-Turbine-Engine (ICT-Engine) for road vehicles, and Injector-Centrifuge-Jet-Engine (ICJ-Engine) for aircraft. The introduction of a supersonic injector in place of the turbine and the rotary compressor, and the introduction of a gas-centrifuge for decomposing of the mixed gases is disclosed. In particular for aircraft, our presently used turbine-engines suffer from fatal turbine-blades crackings, which often results in aircraft crashes. This can be eliminated by the novel engine. - But also the automobilists would have a profit, by ca. 30 % reduction in fuel consumption, arising from removal of the engine cooling and engine friction. The herewith filed application improves an essential component of the above mentioned novel engine, which is the Combi-Supersonic-Adjusting-Plug-Nozzle, fixing for it the following aims: 1) focusing of the jet stream; 2) increasing of the suction effect; 3) improvement of the design; 4) addition of a four-dimensional (4 - D) vectoring; 5) suppression of the engine sound. Also the conventional plug-nozzle will be improved in the same manner, making it compatible with the novel Injector-Centrifuge-Turbine/Jet-Engine.
158	UNIVERSAL ESPRESSO MAKER	PCT/US2012/039525	2012-05-25	WO2012162588A1	2012-11-29	LEE, Thomas, M.; BOUBEDDI, Abdelaziz; MORSE, Thomas, C.
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.
159	개선된 성질 조합을 갖는 알루미늄 합금 제품 및 이를 인공 노화시키는 방법	KR1020097025898	2008-05-14	KR1020100017775A	2010-02-16	브래이게리에이치; 차크라바티드루바제이; 덴저다이애나케이; 린젠씨; 뉴맨존; 베네마그레고리비; 야나르카가테이; 보젤리줄리엔
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.
160	Manual processing system	US09948764	2001-09-10	US06883139B2	2005-04-19	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.

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