Patents for B64D 41 - Power installations for auxiliary purposes (1,346)
05/2003
05/08/2003CA2703108A1 Passive cooling system for auxiliary power unit installation
05/01/2003WO2002040347A9 Mounting assembly for an aircraft auxiliary power unit
05/01/2003US20030080244 Passive cooling system for auxiliary power unit installation
04/2003
04/24/2003US20030078704 Aircraft energy systems management method
04/17/2003US20030070418 Variable cycle boost propulsor
04/16/2003EP1302640A2 Variable cycle boost propulsor
03/2003
03/27/2003WO2002066324A3 Improved aircraft system architecture
03/13/2003US20030047997 Aircraft electrical power distribution network
02/2003
02/18/2003US6520738 Plenum entry bulk swirl generator
01/2003
01/29/2003EP1279595A1 Flame arrestor for an aircraft engine compartment
01/23/2003US20030014963 Flame arrestor to cover aircraft engines
01/16/2003US20030011198 Ram air turbine with high power density generator and self-contained fluid cooling loop
01/08/2003EP0975862B1 Improved integrated environmental and secondary power system
12/2002
12/17/2002US6494047 Airflow sharing
12/12/2002WO2002098736A1 Ram air turbine with high power density generator and self-contained fluid cooling loop
11/2002
11/27/2002EP1259991A1 Thermoelectric power generator for an aircraft
11/20/2002EP1257468A2 Inlet vortex bustor and ice protector for auxiliary power units
11/07/2002WO2002034621A3 High-pressure aircraft pneumatic deicer
11/07/2002US20020165696 Aircraft synthesis and systems evaluation method for determining and evaluating electrical power generation and distribution system components
11/07/2002US20020162914 Aircraft system architecture
11/05/2002CA2127261C Exhaust eductor cooling system
10/2002
10/22/2002US6470224 Configurable aircraft power system
10/10/2002WO2002079631A1 Tortuous path exhaust eductor system
10/10/2002WO2002040347A3 Mounting assembly for an aircraft auxiliary power unit
10/03/2002US20020139120 Tortuous path quiet exhaust eductor system
10/02/2002EP1245076A1 Auxiliary electrical power generation system and method of operating same
10/02/2002EP1056643B1 Aircraft electrical power system including air conditioning system generator
09/2002
09/26/2002WO2002074621A1 Plenum entry bulk swirl generator
09/19/2002US20020131862 Plenum entry bulk swirl generator
09/17/2002US6450447 Auxiliary power unit for an aircraft
08/2002
08/29/2002WO2002066324A2 Improved aircraft system architecture
08/08/2002US20020104707 Acoustic muffler for turbine engine
08/06/2002US6427471 Air cycle machine and air conditioning system using the same
08/01/2002WO2002023688A3 Aircraft electrical power distribution network
07/2002
07/16/2002US6418714 Accumulator utilizing housing case pressure
07/11/2002US20020088900 Aircraft fluid delivery device
07/04/2002US20020084381 Mounting assembly for an aircraft auxiliary power unit and method
06/2002
06/27/2002WO2002049913A1 Flow limiting apparatus
06/27/2002WO2002016805A3 Idg hydraulic control pressure system for adverse ''g'' flight conditions
06/18/2002US6407535 System for beaming power from earth to a high altitude platform
06/13/2002WO2002046040A1 Airflow sharing
06/13/2002US20020069646 Airflow sharing
05/2002
05/23/2002WO2002040347A2 Mounting assembly for an aircraft auxiliary power unit
05/02/2002WO2002034621A2 High-pressure aircraft pneumatic deicer
04/2002
04/24/2002EP0923488B1 Detachable integral aircraft tailcone and power assembly
03/2002
03/28/2002WO2001062592A3 Inlet vortex bustor and ice protector for auxiliary power units
03/21/2002WO2002023688A2 Aircraft electrical power distribution network
03/14/2002US20020030956 Power switching device in an electrical power distribution system on board a helicopter
02/2002
02/28/2002WO2002016805A2 Idg hydraulic control pressure system for adverse ''g'' flight conditions
02/26/2002US6349899 Aircraft auxiliary air intake with ram and flush opening door
12/2001
12/18/2001US6331099 Flexible hoses communicating with a deployable hydraulic power assembly
10/2001
10/30/2001US6308915 Detachable integral aircraft tailcone and power assembly
10/25/2001DE10045446C1 Energy switching device for helicopter electrical energy distribution system uses optical fibre cable for transmission of control signals from overhead console for preventing electromagnetic interference
10/02/2001US6296957 Energy supply unit on board an aircraft
09/2001
09/05/2001EP1129941A2 Air cycle environmental control system
09/04/2001US6283410 Secondary power integrated cabin energy system for a pressurized aircraft
08/2001
08/30/2001WO2001062592A2 Inlet vortex bustor and ice protector for auxiliary power units
08/23/2001WO2001061768A1 Thermoelectric power generator for an aircraft
08/21/2001US6278262 Auxiliary power unit system and method of operating an auxiliary power unit
07/2001
07/24/2001US6264137 Inlet vortex bustor and ice protector for auxiliary power units
07/17/2001US6260351 Controlled spring rate gearbox mount
06/2001
06/28/2001WO2001047100A1 Auxiliary electrical power generation system and method of operating same
06/19/2001US6247668 Auxiliary power and thrust unit
06/13/2001EP1106870A2 Method and apparatus for driving an aircraft generator at constant speed
06/12/2001US6244539 Detachable integral aircraft tailcone and power assembly
06/12/2001US6244036 Control for augment mode JP-air emergency power unit
06/07/2001US20010003108 Method and apparatus of driving aircraft generator at a constant-speed
05/2001
05/17/2001WO2001034464A2 Aircraft absolute safety landing device
05/17/2001CA2424691A1 Aircraft absolute safety landing device
05/16/2001EP1099630A2 Power supply system for an aircraft
03/2001
03/08/2001WO2000059780A3 Flywheel peaking unit for an aircraft hydraulic system
02/2001
02/20/2001US6189324 Environment control unit for turbine engine
02/06/2001US6182435 Thermal and energy management method and apparatus for an aircraft
01/2001
01/17/2001EP1069044A2 Auxiliary power and thrust unit
12/2000
12/27/2000EP1062155A1 Apu compartment drain system
12/06/2000EP1056643A1 Aircraft electrical power system including air conditioning system generator
11/2000
11/07/2000US6142418 Multi-path secondary power system for an aircraft
10/2000
10/12/2000WO2000059780A2 Flywheel peaking unit for an aircraft hydraulic system
10/03/2000US6127758 Ram air turbine system
09/2000
09/13/2000EP1035016A1 Auxiliary Power Unit for Aircraft
08/2000
08/31/2000DE19911018C1 Unit for supplying auxiliary power to aircraft includes a gas turbine with a combustion chamber, a blower, a turbine coupled to a compressor to generate compressed air and a fuel cell to generate electrical energy.
07/2000
07/25/2000US6092360 Auxiliary power unit passive cooling system
06/2000
06/28/2000EP1012038A1 Multiple mode environmental control system for pressurized aircraft cabin
06/21/2000EP1010618A2 Integrated muffler and exhaust cone for aircraft tailcone
06/14/2000EP1008738A2 Controlled spring rate gearbox mount
03/2000
03/21/2000US6039287 Detachable integral aircraft tailcone and power assembly
02/2000
02/02/2000EP0975862A1 Improved integrated environmental and secondary power system
01/2000
01/05/2000EP0968918A2 Auxiliary power unit passive cooling system
12/1999
12/29/1999EP0967676A1 Jet engine with integral fuel cell
12/07/1999US5996938 APU compartment drain system
11/1999
11/18/1999DE19821952A1 Energieversorgungseinheit an Bord eines Luftfahrzeugs Power supply unit on board an aircraft
11/17/1999EP0957026A2 Power supply unit on board an aircraft
09/1999
09/28/1999US5956960 Multiple mode environmental control system for pressurized aircraft cabin
09/16/1999WO1999046167A1 Apu compartment drain system
08/1999
08/19/1999WO1999041146A1 Aircraft electrical power system including air conditioning system generator
08/17/1999US5939800 Aircraft electrical power system including air conditioning system generator
06/1999
06/23/1999EP0923488A1 Detachable integral aircraft tailcone and power assembly
06/15/1999US5911388 Environmental control system with energy recovery and bleed air assist
03/1999
03/25/1999WO1999014116A1 Ram air turbine system
03/18/1999WO1999012810A1 Multiple mode environmental control system for pressurized aircraft cabin
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