Patents for B64D 33 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for (2,926)
11/2005
11/29/2005US6969028 Scarf nozzle for a jet engine and method of using the same
11/29/2005US6968701 Engine integrated auxiliary power unit
11/24/2005US20050258307 Jet engine nacelle for a supersonic aircraft
11/22/2005US6966524 Aircraft engine nacelles and methods for their manufacture
11/22/2005CA2225608C A thrust reverser system for a dual flow bypass turbojet with upstream clamshells
11/16/2005EP1595068A2 Ventilated confluent exhaust nozzle
11/16/2005EP1594738A1 Apparatus and method for providing fireproofing to an oil cooler in an aircraft auxiliary power unit compartment
11/15/2005US6964169 Hollow tapered body flattened in the transverse direction, wall being divided transversely into four adjacent parts, trapezoidal wall, made of refractory fibers embedded in another refractory matrics; vapor deposit refractory matrics; durability
11/15/2005CA2234436C Device for closing and locking the blockers of a thrust reverser
10/2005
10/27/2005US20050235628 Ejector cooled nozzle
10/26/2005EP1071608B1 Biplanar scarfed nacelle inlet
10/20/2005US20050229602 Forced air cooling system
10/16/2005CA2502816A1 Forced air cooling system
10/13/2005US20050224635 Dual action inlet door and method for use thereof
10/13/2005US20050223693 Engine cooling
10/06/2005US20050217271 Turbine engine nozzle
10/06/2005US20050217239 Methods and apparatus for exhausting gases from gas turbine engines
10/05/2005EP1582730A1 Apparatus for exhausting gases from gas turbine engines
09/2005
09/30/2005CA2502374A1 Methods and apparatus for exhausting gases from gas turbine engines
09/29/2005WO2005090156A1 Annular acoustic panel
09/29/2005US20050214113 Compressor for an aircraft engine
09/29/2005US20050211824 Turbine engine arrangements
09/28/2005EP1580399A1 Compressor for an aircraft engine.
09/28/2005CN2728911Y Warming-up machine
09/27/2005US6948317 Methods and apparatus for flade engine nozzle
09/22/2005WO2005063564A3 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
09/20/2005US6945494 Variable position intake for an aircraft mounted gas turbine engine
09/20/2005CA2243099C Turbofan thrust reverser with axially guided blockers attached to the primary cowling
09/13/2005US6942462 Gas turbine engine nose cone
09/13/2005US6942181 Passive cooling system for auxiliary power unit installation
09/01/2005US20050188676 Ventilated confluent exhaust nozzle
09/01/2005DE102004004980A1 Air intake for turboprop engine, especially aircraft engine, has fixed cutting blades inside air duct to chop ingested items into sufficiently small pieces to prevent turbine damage
08/2005
08/30/2005US6935118 Exhaust nozzle segmented basesheet and production method thereof
08/30/2005US6935097 Lock assembly that inhibits thrust reverser movement at or near the stowed position
08/24/2005EP1163151B1 Modular air intake duct for aircraft
08/18/2005US20050178891 Electrical generator fluid-flow-coolant filtration
08/17/2005CN2718234Y Superman flying motorcycle
08/16/2005US6928916 Infrared friend or foe identification system
08/11/2005WO2005073600A1 Reversible driving apparatus for pcu pumps
08/11/2005WO2005021934A3 Ventilated confluent exhaust nozzle
08/11/2005DE10361644A1 Luftleitklappe eines Luftfahrzeuges mit Regelung der auf sie wirkenden Druckkräfte, Verfahren zur Stellungsregelung einer Luftleitklappe und Stauluftsystem mit einer solchen Luftleitklappe Air guiding an aircraft with control of the pressure forces acting on them, methods for controlling the position of a flow-rate control and ram air system with such a flow-rate control
08/11/2005CA2554264A1 Reversible driving apparatus for pcu pumps
08/09/2005US6926234 Electromechanical turbojet thrust reverser with continuous position control
08/04/2005US20050166705 Reversible driving apparatus for PCU pumps
08/04/2005DE10361722A1 Stauluftkanal zur Umgebungsluftzufuhr in einem Flugzeug Ram air duct to the ambient air in an aircraft
07/2005
07/27/2005EP1368228B1 Plenum entry bulk swirl generator
07/26/2005US6920958 Annular acoustic panel
07/26/2005US6920890 Airflow controller
07/26/2005CA2223529C Thrust reverser for jet turbine engine with doors held within nacelle lines
07/21/2005WO2005066536A1 Support device for fire-detection system
07/21/2005CA2544484A1 Support device for fire-detection system
07/14/2005WO2005063579A1 Ram air channel for the supply of ambient air in an aircraft
07/14/2005WO2005063564A2 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
07/14/2005US20050151026 Laminar flow nacelle for an aircraft engine
07/14/2005US20050151017 Fire shield apparatus and method
07/12/2005CA2222470C Device for linking a thrust reverser to a turbine engine
07/07/2005WO2005061323A1 Aircraft fluid cooling system and an aircraft provided with said system
06/2005
06/30/2005US20050138932 Aircraft protection method and system
06/28/2005US6911158 Ceramics with porosities of 75% to 85%; material retains strength while maintaining prescribed sound absorbing effect; efficiently absorbs noises over wide range of sound frequencies, such as from jet engines
06/28/2005US6910327 Apparatus and methods for varying inlet lip geometry of a jet engine inlet
06/23/2005US20050132709 Exhaust nozzle segmented basesheet and production method thereof
06/22/2005EP1544448A2 Exhaust nozzle segmented basesheet and production method thereof
06/07/2005US6901737 Air intake for an auxiliary power unit in an aircraft
06/02/2005US20050115245 Device for reducing the jet noise of a turbomachine
05/2005
05/17/2005US6892981 Stealthy duffel bag airplane
05/06/2005WO2005039978A2 Aircraft protection method and system
05/05/2005US20050091982 Methods and apparatus for flade engine nozzle
05/04/2005EP1528248A1 Methods and apparatus for flade engine nozzle
05/04/2005EP1527997A2 Flade gas turbine engine with fixed geometry inlet
05/04/2005EP1527268A1 Thrust reverser system with a pass-through torque activated brake
04/2005
04/26/2005US6883751 Apparatus and method for preventing foreign object damage to an aircraft
04/21/2005US20050082112 Annular acoustic panel
04/21/2005US20050081530 Arrangement for bleeding the boundary layer from an aircraft engine
04/21/2005US20050081509 Flade gas turbine engine with fixed geometry inlet
04/20/2005EP1524190A2 Engine cooling
04/14/2005DE10340690A1 Sensor for measuring gas pressure in air inlet in front of compressor stage of a driving mechanism of an aircraft jet engine has pressure measuring line for introducing gas from chamber, and surrounded by water-repelling sensor core
04/07/2005US20050072876 Variably angled propulsion/steering system
04/07/2005DE19721429B4 Verfahren zur Verminderung der Zielsignatur von Luftfahrzeugen A method for reducing the target signature of aircraft
04/05/2005US6874728 Superman air motor
03/2005
03/29/2005US6871797 Turbine engine nozzle
03/24/2005US20050060982 Method and system for reduction of jet engine noise
03/23/2005EP1517022A2 Method and system for reduction of jet engine noise
03/17/2005US20050056724 Stress releiving; computer for data storage; input temperature profile; measuring starup temperature; calibration; injecting water, alcohol in response to signal
03/15/2005CA2236044C Thrust reverser with protection in the event of accidental shutter release
03/11/2005CA2479275A1 Helicopter turbine engine protection system
03/10/2005WO2005021934A2 Ventilated confluent exhaust nozzle
03/02/2005EP1509447A2 Bifurcated turbofan nozzle
03/01/2005CA2410838C Apparatus for reducing noise in the jet engine
02/2005
02/24/2005WO2005016748A2 Dual action inlet door and method for use thereof
02/23/2005EP1507971A1 Variable area thrust reverser nozzle
02/22/2005US6857597 Control system for vertical take off and land (VTOL) aircraft
02/10/2005DE102004032709A1 Turbinenmaschinendüse Turbinenmaschinendüse
02/09/2005CN1576560A Fluidic chevrons and configurable thermal shield for jet noise reduction
02/08/2005CA2204823C Turbofan reverse thruster with obstructions connected to primary cowling
02/03/2005US20050023412 Nacelle inlet lip anti-icing with engine oil
02/03/2005US20050022866 Apparatus and methods for varying inlet lip geometry of a jet engine inlet
02/01/2005US6848656 Ice protection system
01/2005
01/25/2005US6845945 Thrust reverser with sliding pivot joints
01/20/2005US20050011195 Turbine engine nozzle
01/13/2005US20050006529 Method and apparatus for noise abatement and ice protection of an aircraft engine nacelle inlet lip
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