Patents for B64D 33 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for (2,926) |
---|
08/14/2007 | CA2424497C Turboprop aircraft engine |
08/09/2007 | WO2007090011A2 Engine air intake barrier filter system for aircraft |
08/08/2007 | EP1816072A1 Exhaust system for a turbofan engine |
08/08/2007 | EP1816071A2 Aircraft auxiliary gas turbine engine and method for operating the same |
08/02/2007 | US20070176052 Air inlet for a turbofan engine |
08/02/2007 | CA2576683A1 Aircraft auxiliary gas turbine engine and method for operating |
08/01/2007 | EP1813529A1 Air intake of a turbofan engine |
08/01/2007 | EP1257467B1 Improved aerobatic aircraft |
07/25/2007 | EP1809892A1 An outlet device for a jet engine and a jet engine comprising such an outlet device |
07/25/2007 | EP1809891A1 Propulsion system, aircraft comprising the propulsion system and an outlet device for a jet engine |
07/25/2007 | CN101003305A Fuel deoxygenator with non-planar fuel channel and oxygen permeable membrane |
07/19/2007 | US20070164160 Support device for fire-detection system |
07/11/2007 | EP1806495A2 Exhaust duct flow splitter system |
07/04/2007 | EP1685025B1 Aircraft fluid cooling system and an aircraft provided with said system |
06/28/2007 | US20070145186 Air guiding flap of an aircraft comprising control of the pressure forces impinging thereon, process for adjusting the position of an air guiding flap and ram air system including such an air guiding flap |
06/26/2007 | US7234294 Outlet nozzle and a method for manufacturing an outlet nozzle |
06/21/2007 | US20070138337 Rear suspension for an aircraft engine with shackle in waiting and spring for such a hinge pin in waiting |
06/20/2007 | EP1797311A2 Quiet chevron/tab exhaust eductor system |
06/20/2007 | CN2913183Y Booster low-pressure de-watering ring-control apparatus with ice proof cavity |
06/20/2007 | CN1984812A Airplane with multi-motor |
06/19/2007 | US7232097 Fire shield method |
06/19/2007 | US7231767 Forced air cooling system |
06/12/2007 | US7229029 Propulsion system |
06/12/2007 | CA2266936C Thermal protection structure |
06/07/2007 | US20070125906 Ram air channel for the supply of ambient air in an aircraft |
06/05/2007 | US7225622 Turbine engine nozzle |
05/31/2007 | US20070120009 Aircraft ram air inlet with multi-member closure flap |
05/31/2007 | US20070120008 Engine airframe J-seal damper |
05/30/2007 | CA2569293A1 Engine airframe j-seal damper |
05/29/2007 | US7222819 Aircraft ram air inlet with multi-member closure flap |
05/18/2007 | WO2007055088A1 Energy-saving jet aircraft |
05/18/2007 | WO2007053932A1 Method and system for taxiing an aircraft |
05/18/2007 | CA2628440A1 Method and system for taxiing an aircraft |
05/15/2007 | US7217184 Electrical generator fluid-flow-coolant filtration method |
05/15/2007 | CA2401649C Inlet vortex bustor and ice protector for auxiliary power units |
05/15/2007 | CA2329343C Jet engine exhaust nozzle |
05/10/2007 | US20070102234 Duct for reducing shock related noise |
05/09/2007 | CN1314894C Maintenance and inhibition plate for a thrust reverser |
05/09/2007 | CN1314893C Electromechanical thrust reverser for a turboreactor used to control door movement |
05/03/2007 | WO2007001372A9 Ducted spinner for engine cooling |
05/02/2007 | EP1440004B1 Passive cooling system for auxiliary power unit installation |
05/01/2007 | US7210897 Actively-controlled sound absorption panel system using movement-controlled reflective plate |
05/01/2007 | US7210652 Dual action inlet door and method for use thereof |
05/01/2007 | US7210283 Maintenance and inhibition plate for a thrust reverser |
04/25/2007 | CA2565216A1 Eductor swirl buster |
04/24/2007 | US7207772 Compressor for an aircraft engine |
04/24/2007 | US7207520 System, method, and apparatus for designing streamline traced, mixed compression inlets for aircraft engines |
04/24/2007 | CA2247176C Laminar flow jet engine bay |
04/19/2007 | US20070084964 Thrust reversers including support members for inhibiting deflection |
04/10/2007 | US7200999 Arrangement for bleeding the boundary layer from an aircraft engine |
04/05/2007 | WO2007037725A1 An arrangement for propelling an aircraft, aircraft and outlet nozzle for a jet engine |
04/05/2007 | WO2007036523A1 Engine assembly for an aircraft comprising an engine as well as an engine mounting structure for such an engine |
04/05/2007 | WO2007036522A1 Engine assembly for an aircraft comprising an engine as well as an engine mounting structure for such an engine |
04/05/2007 | CA2624010A1 Aircraft engine assembly comprising an engine and a suspension pylon for such an engine |
04/05/2007 | CA2624005A1 Engine assembly for an aircraft comprising an engine as well as an engine mounting structure for such an engine |
03/29/2007 | DE102005039042A1 Drive system for e.g. aircraft, has adjustment device controlling angle of incidence of blade, where drive impulse vector is controlled by adjustability of angle of inclination of blade together with controlling of drive power of propeller |
03/28/2007 | EP1767455A2 Auxiliary power unit inlet door position control system and method |
03/28/2007 | EP1765669A1 Multi-engine aircraft |
03/22/2007 | WO2007031616A1 Dynamically self-locking catching device |
03/22/2007 | US20070063098 Passive cooling system for auxiliary power unit installation |
03/22/2007 | US20070063097 Air input device for a turboprop engine |
03/22/2007 | CA2620494A1 Dynamically self-locking catching device |
03/20/2007 | US7192462 usable in existing aircraft without substantial modifications; seal permits relative movement between the duct and the assembly in any direction while maintaining a seal between the duct and the assembly |
03/15/2007 | DE102005039043A1 Drive system for vertical starting and landing aircraft, has arrangement of air guiding channels and air screws for generation of impulse, and driving unit controlled such that different strong air flow is produced in each channel |
03/13/2007 | US7188417 Advanced L-channel welded nozzle design |
03/07/2007 | EP1646560B1 Dual action inlet door and method for use thereof |
02/22/2007 | US20070039328 Turbine engine nozzle |
02/08/2007 | WO2007016086A1 Engine intake sealing system |
02/08/2007 | WO2007016085A1 Control of engine intake door |
02/08/2007 | WO2007015447A1 Unmanned helicopter |
02/08/2007 | CA2546714A1 A method of operating an aircraft system |
02/07/2007 | EP1750001A2 An exhaust nozzle for a gas turbine engine |
02/07/2007 | EP1749993A2 Auxiliary power unit intake duct with aero-acoustic guide vanes |
02/03/2007 | CA2554385A1 One-piece baffle infrared suppressor apparatus and method |
02/03/2007 | CA2554151A1 Infrared suppressor apparatus and method |
02/01/2007 | US20070026268 Aircraft having a fuel cell |
02/01/2007 | US20070025838 Control of engine intake door |
01/31/2007 | EP1748177A1 Compact, light weight eductor oil cooler plenum and surge flow plenum design |
01/24/2007 | EP1206384B1 Supersonic external-compression diffuser and method for designing same |
01/24/2007 | CN1902094A Ram air channel for the supply of ambient air in an aircraft |
01/24/2007 | CN1902093A Air guiding flap of an aircraft comprising control of the pressure forces impinging thereon, process for adjusting the position of an air guiding flap and ram air system including such an air guiding |
01/23/2007 | US7165744 Turbine engine arrangements |
01/23/2007 | CA2226441C Turboprop engine with an air-oil cooler |
01/23/2007 | CA2226424C Aircraft gas turbine engine with a liquid-air heat exchanger |
01/19/2007 | CA2551767A1 Engine heat exchanger with thermoelectric generation |
01/11/2007 | US20070007385 Electric flight control surface actuation system electronic architecture |
01/09/2007 | US7159818 Multi-spectral air inlet shield and associated inlet structure |
01/09/2007 | CA2239462C Bypass turbojet thrust reverser with doors fitted with a movable spoiler with optimized drive |
01/04/2007 | WO2007001372A2 Ducted spinner for engine cooling |
01/03/2007 | CN1890502A Holding device for fire detection system |
12/30/2006 | CA2551306A1 Helicopter with an auxiliary lubricating circuit |
12/21/2006 | US20060284015 Fire shield method |
12/19/2006 | US7150432 Horizontal augmented thrust system and method for creating augmented thrust |
12/19/2006 | US7150431 Electrical generator fluid-flow-coolant filtration |
12/19/2006 | US7150255 Engine including electrical interference shield |
12/14/2006 | DE102005022943B3 Unmanned aircraft external pressure determination unit has static pressure sensor recessed into hole in aircraft |
12/14/2006 | DE102005022942B3 Unmanned aircraft external pressure determination unit has static pressure sensor recessed into hole in aircraft |
12/13/2006 | CN1878695A Aircraft fluid cooling system and an aircraft provided with said system |
12/07/2006 | DE19600936B4 Hybrid-Wasserflugzeug mit Flüssigwasserstoff-Kraftstoffanlage für Flüssigwasserstoff-gekühlten-HTSL-Linearmotor-Katapult-Start und HTSL-MHD-Wasserung mit Fortbewegung auf dem Wasser Hybrid Water aircraft with liquid hydrogen fuel system for liquid hydrogen cooled-HTSC linear motor catapult launch and HTSC MHD splashdown with locomotion on the water |
12/02/2006 | CA2548138A1 Methods and apparatus for operating gas turbine engines |