Patents for B64D 41 - Power installations for auxiliary purposes (1,346)
12/2011
12/19/2011DE202011104751U1 "Hybrid-Flugzeug" zur Minimierung der Flughafenprobleme u. des CO2-Ausstoßes, weltweit. "Hybrid aircraft" and to minimize the problems Airport. CO2 emissions worldwide.
12/15/2011WO2011154645A1 Power supply circuit for an aircraft de-icing system
12/15/2011US20110303786 Silencer for an auxiliary power unit of an aircraft
12/15/2011CA2802159A1 Power supply circuit for an aircraft de-icing system
12/14/2011EP2394309A1 Thermoelectric generation for a gas turbine
12/08/2011WO2011151160A1 Aircraft and corresponding power supply unit
12/08/2011DE102010022548A1 Luftfahrzeug und Stromversorgungseinheit hierfür Aircraft and power supply unit for this
12/01/2011WO2011113696A3 Energy-regulating device for regulating hybrid energy sources for an aircraft
12/01/2011DE102011050646A1 Messung transienter elektrischer Aktivität in Flugzeug-Energieverteilungssystemen Measurement of transient electrical activity in aircraft power distribution systems
11/2011
11/29/2011CA2533394C Dual action inlet door and method for use thereof
11/26/2011CA2741382A1 Measuring transient electrical activity in aircraft power distribution systems
11/24/2011WO2011146021A1 Self-powered yaw control and anti-spin device for fixed wing aircraft
11/22/2011US8061650 Automatic control systems for aircraft auxiliary power units, and associated methods
11/16/2011CN102245471A Emergency power system for an aircraft
11/09/2011CN101385175B A combination of a heat generating system with a fuel cell system
10/2011
10/27/2011US20110259998 Configuration of a rear fuselage tail cone of an aircraft with an auxiliary power unit
10/26/2011EP2381080A2 Accessory gearbox with a starter/generator
10/26/2011EP2153040B1 Device for mechanically decoupled attachment of an aircraft component having hot gas flowing through the same
10/19/2011EP2013080B1 Electricity distribution system and method inside an aircraft
10/19/2011CN102224076A Remote device control and power supply
10/13/2011WO2011089016A3 Self-sufficient monument in the aircraft pressure cabin having a decentralized operating resource supply and efficient energy conversion
10/13/2011WO2011023678A3 Power grid for an aircraft, and method for operating the power grid
10/13/2011DE102010014838A1 Method for generating electric energy on aircrafts, involves installing aircrafts airflow turbines or wind turbines or propellers, which are attached by screwing and brought into rotation by wind and also by air flow
10/06/2011US20110240795 Emergency power system for an aircraft
10/06/2011DE102010013956A1 Kompressor/Turbinen-Anordnung, Klimaaggregat und Verfahren zum Betreiben einer Kompressor/Turbinen-Anordnung Compressor / turbine arrangement, air conditioning unit and method for operating a compressor / turbine arrangement
10/05/2011CN102210094A Power distribution device for distributing power and a method for distributing power
10/05/2011CN101272955B Energy supply system for supplying energy to aircraft systems
10/04/2011CA2555070C Support system for auxiliary power unit
09/2011
09/28/2011EP2369175A2 Hybrid ram air turbine
09/27/2011CA2638648C Generator for gas turbine engine having dc bus fault short circuit control using a battery
09/22/2011WO2011113696A2 Energy-regulating device for regulating hybrid energy sources for an aircraft
09/15/2011DE102010011416A1 Energieregelvorrichtung zum Regeln hybrider Energiequellen für ein Flugzeug Power control apparatus for controlling a hybrid energy sources for an aircraft
09/13/2011US8016228 Combined fuel cell aircraft auxiliary power unit and environmental control system
09/07/2011CN102177068A Auxiliary power unit (APU) of an aircraft
08/2011
08/31/2011CN102167160A Miniature flapping wing aircraft launching in jumping mode
08/18/2011WO2011071602A3 Thermoelectric generator on an aircraft bleed system
08/17/2011EP2356026A2 Emergency power system for an aircraft
08/16/2011US7997532 Airborne power station
08/04/2011US20110186096 Aircraft maintenance unit
08/02/2011US7988102 Aircraft with a fluid-duct-system
07/2011
07/28/2011WO2011089196A1 Device and method for regulating the humidity of a fuel cell
07/28/2011DE102009048394B4 Kühlsystem für Brennstoffzellensysteme, Verfahren zum Kühlen von Brennstoffzellensystemen A cooling system for fuel cell systems, method of cooling of fuel cell systems
07/27/2011EP2347956A2 Auxiliary power unit (apu) of an aircraft
07/21/2011WO2011037855A3 Method for managing power boost in a fuel cell powered aerial vehicle
07/21/2011DE102007061588B4 Flugzeugkühlsystem Aircraft cooling system
07/20/2011EP2345149A1 Power distribution device for distributing power and a method for distributing power
07/19/2011US7980509 Aircraft taxiing systems
07/12/2011CA2580276C Mechanical flight control auxiliary power assist system
07/06/2011CN101128967B Electric supply for an aircraft gas turbine engine equipment
06/2011
06/30/2011WO2011037850A3 Method for managing power and energy in a fuel cell powered aerial vehicle based on secondary operation priority
06/30/2011US20110155853 Interface Element, Aircraft Interior Equipment Component And Method For Installing An Aircraft Interior Equipment Component
06/29/2011CN101146712B Supply system for an aircraft
06/23/2011WO2011072366A1 Electric accumulator utilizing an ultra-capacitor array
06/22/2011EP2334558A2 Sound absorber for an auxiliary engine of an aircraft
06/22/2011CN102105356A Assembly of actuators and of a system for supplying electrical power from a network
06/16/2011CA2782972A1 Thermoelectric generator on an aircraft bleed system
06/15/2011EP2331406A1 Remote device control and power supply
06/15/2011CA2688671A1 Electric accumulator utilizing an ultra-capacitor array
06/09/2011DE202009002559U1 Die Antinoteinrichtung der Flugzeuge The Antinoteinrichtung the aircraft
06/07/2011CA2464188C Passive cooling system for auxiliary power unit installation
06/02/2011US20110127372 Automatic control systems for aircraft auxiliary power units, and associated methods
05/2011
05/31/2011US7950606 Electric-based secondary power system architectures for aircraft
05/18/2011CN1950255B Boundary layer suction arrangement
05/12/2011WO2010105744A4 Cooler for an aircraft cooling system, aircraft cooling system and method for operating an aircraft cooling system
05/11/2011EP2318270A2 Assembly of actuators and of a system for supplying electrical power from a network
05/05/2011WO2011051210A1 Fuel cell system and method for drying exhaust gas of a fuel cell system
05/05/2011CA2781710A1 Fuel cell system and method for drying exhaust gas of a fuel cell system
05/04/2011EP2316735A1 Power distribution apparatus
04/2011
04/28/2011DE102008031933B4 Radantriebssystem für ein Flugzeug mit einer Brennstoffzelle als Energiequelle Wheel drive system for an aircraft with a fuel cell as an energy source
04/21/2011DE102009048393B3 Cooling system for cooling a fuel cell system in a vehicle, comprises a first heat transfer carrier, which forms a thermal connection between the fuel cell system and a fuel from a fuel tank of the vehicle, and a cooling circuit
04/19/2011CA2631758C Control channel for vehicle systems using the vehicle's power distribution system
04/14/2011WO2011042215A1 Cooling system for fuel cell systems, method for cooling fuel cell systems, and a fuel cell system
04/14/2011CA2776550A1 Cooling system for fuel cell systems, method for cooling fuel cell systems, and a fuel cell system
04/13/2011CN102015449A Bearing device for supporting a power supply device on a structural part of an aircraft and aircraft comprising said bearing device
04/13/2011CA2722402A1 Piloting network for single- or multi-engine actuators, specifically adapted to aeronautical applications such as feeding latching assembly motors
04/12/2011US7922117 Primary panel and motor controller integration for aircraft power distribution system
04/07/2011DE102009048394A1 Cooling system for cooling fuel cell system in airplane, has cooling circuit with heat exchanger that forms thermal connection between fuel cell system and fuel from fuel tank of vehicle, where heat exchanger is connected to fuel outlet
04/06/2011EP1984970B1 A combination of a heat generating system with a fuel cell system
03/2011
03/31/2011WO2011037855A2 Method for managing power boost in a fuel cell powered aerial vehicle
03/31/2011WO2011037850A2 Method for managing power and energy in a fuel cell powered aerial vehicle based on secondary operation priority
03/29/2011CA2516884C Engine power extraction control system
03/22/2011US7909286 Support system for auxiliary power unit
03/17/2011WO2010105744A3 Cooler for an aircraft cooling system, aircraft cooling system and method for operating an aircraft cooling system
03/17/2011US20110062280 Electromagnetic landing gear brakes
03/17/2011DE102007057536B4 Klimaanlage mit Hybrid-Zapfluft-Betrieb Air conditioning with hybrid bleed air operation
03/15/2011CA2466581C Off loading clutch for gas turbine engine starting
03/09/2011EP1976759B1 Emergency supply unit with a ram-air turbine adapted to be driven by an air stream and with an energy converter for aircraft
03/03/2011WO2011023678A2 Power grid for an aircraft, and method for operating the power grid
03/03/2011US20110049291 Mounting device for mounting an energy supply device on a structural component of an aicraft and aircraft with a mounting device
03/03/2011CA2772160A1 Electrical network of an aircraft and method of operation of the electrical network
03/02/2011EP2289802A2 Supply system and method for energy supply in an aircraft
02/2011
02/24/2011WO2010146291A3 Aircraft provided with a fuel cell system
02/24/2011US20110045370 Aircraft Fuel Cell System
02/22/2011US7891605 Automatic control systems for aircraft auxiliary power units, and associated methods
02/09/2011EP2280870A2 Bearing device for supporting a power supply device on a structural part of an aircraft and aircraft comprising said bearing device
02/06/2011CA2711065A1 Permanent magnet machine and rotor
02/03/2011DE102009048459A1 Sandwich-type heat exchanger for use in cooling system for aircraft, has plate forming gap at shell and/or bulkhead, where gap allows inflow of air from slits into exterior shell of aircraft, and slits are arranged adjacent to exchanger
02/02/2011EP2279946A1 Configuration of the pneumatic unit in the tail area of an aircraft
01/2011
01/27/2011WO2011010033A1 Electric power supply circuit for a turbojet engine nacelle
01/27/2011CA2767632A1 Electric power supply circuit for a turbojet engine nacelle
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