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