Patents for B64D 33 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for (2,926)
05/2008
05/14/2008EP1921291A2 Gas turbine engine providing simulated boundary layer thickness increase
05/13/2008US7370468 Turbojet electromechanical thrust reverser with servo-controlled door displacement
05/07/2008EP1918202A2 Exhaust eductor system with a recirculation baffle
05/07/2008EP1918201A1 Auxiliary power unit assembly
05/07/2008EP1918200A1 Auxiliary power unit assembly
05/07/2008EP1918199A2 Aicraft airframe architecture
05/01/2008US20080099632 Aircraft airframe architectures
05/01/2008US20080099631 Tandem air inlet apparatus and method for an airborne mobile platform
05/01/2008US20080099630 Air inlet and method for a highspeed mobile platform
04/2008
04/30/2008EP1916185A2 Air inlet and method for a highspeed mobile platform
04/30/2008CA2607051A1 Auxiliary power unit assembly
04/30/2008CA2606739A1 Auxiliary power unit assembly
04/29/2008US7364118 Propulsion arrangement
04/29/2008US7364117 Passive cooling system for auxiliary power unit installation
04/24/2008WO2008049054A1 System and method for controlling an environment in an aircraft using a vortex cooler
04/24/2008WO2008047357A2 Temperature controlled valve for regulating cooling gas flow
04/17/2008WO2008045108A2 Isentropic compression inlet for supersonic aircraft
04/17/2008CA2634012A1 Isentropic compression inlet for supersonic aircraft
04/16/2008EP1910168A1 Control of engine intake door
04/10/2008WO2008040877A1 Removable air intake structure for turbojet engine nacelle
04/10/2008CA2664034A1 Removable air intake structure for turbojet engine nacelle
04/03/2008US20080078612 Integrated Inlet Attachment
04/03/2008DE10335482B4 Staulufteinlass eines Flugzeuges Ram air inlet of an aircraft
04/01/2008US7350619 Auxiliary power unit exhaust duct with muffler incorporating an externally replaceable acoustic liner
03/2008
03/27/2008US20080073459 Multi-Engine Aircraft
03/26/2008EP1902953A1 Device for soundproofing a gas turbine helicopter engine and engine obtained using same
03/20/2008CA2602179A1 Gas turbine helicopter engine soundproofing device and the resulting engine
03/20/2008CA2602168A1 Gas turbine helicopter engine with noise emission reduced through acoustical treatment of an eductor
03/05/2008EP1340736B1 Porous sound absorbing material and method of manufacturing the material
03/04/2008US7337875 High admittance acoustic liner
03/04/2008US7337605 Thermal management for aircraft auxiliary power unit compartment
02/2008
02/29/2008CA2598304A1 Fan exhaust nozzle for turbofan engine
02/27/2008CN101131123A Multifunctional air inlet of turbine engine
02/27/2008CN100371580C Long service life jet deflection plate for turbine jet motor of aircraft
02/19/2008US7331421 Flow restrictors for aircraft inlet acoustic treatments, and associated systems and methods
02/14/2008WO2008017567A1 Air inlet for a jet engine
02/12/2008US7328771 Zero acoustic splice fan case liner
02/09/2008CA2839333A1 Jet engine nozzle exit configurations and associated systems and methods
02/09/2008CA2813533A1 Jet engine nozzle exit configurations and associated systems and methods
02/09/2008CA2756214A1 Jet engine nozzle exit configurations and associated systems and methods
02/07/2008WO2008016341A2 Engine intake system with accessible, interchangeable air filters
01/2008
01/29/2008US7322179 Air intake and method for breathing air using an air intake
01/24/2008US20080016873 Outlet Device for a Jet Engine and a Jet Engine Comprising Such an Outlet Device
01/23/2008EP1880941A2 System for joining acoustic cellular panel sections in edge-to-edge relation
01/10/2008US20080006743 Long endurance hydrogen powered vehicle
01/09/2008EP1874626A2 Integrated engine air particle filter assembly
01/08/2008CA2305927C Universal joint-type vectoring turbojet exhaust nozzle
01/03/2008US20080001039 Thrust vectorable fan variable area nozzle for a gas turbine engine fan nacelle
01/03/2008US20080001038 Fuel cell/combustor systems and methods for aircraft and other applications
01/03/2008US20080000717 Anechoic visco-thermal liner
12/2007
12/27/2007WO2007106188A3 Infrared suppression system with spiral septum
12/25/2007US7310939 Device for reducing the jet noise of a turbomachine
12/20/2007DE102006027728A1 Wärmedämmschicht Thermal barrier coating
12/18/2007US7308966 Device for reducing jet engine exhaust noise using oscillating jets
12/18/2007CA2276544C Particle traps for turbo-prop engine
12/13/2007US20070284477 Vertical Tail Unit For Aircraft And Aircraft Equipped With Same
12/12/2007EP1595068B1 Ventilated confluent exhaust nozzle
12/06/2007US20070278345 Device for articulating a door of a nacelle of an aircraft and nacelle provided with said articulation device
12/04/2007US7302794 Rocket engine member and a method for manufacturing a rocket engine member
11/2007
11/22/2007US20070267539 Hinged device for doors of an aircraft nacelle and nacelle equipped with said hinged device
11/22/2007US20070267246 Multi-splice acoustic liner
11/21/2007CN100350147C Electromechanical turbojet thrust reverser with containuous position control
11/21/2007CN100350146C Turbojet engine electromechanical thrust reverse with synchronous locking device
11/20/2007US7296656 Acoustic mechanical retainer
11/20/2007US7296655 Duct liner acoustic splice
11/15/2007WO2007108787A3 Pre-hung inlet door system
11/08/2007US20070256889 Sound-absorbing exhaust nozzle center plug
11/05/2007CA2587068A1 Power and control system for electrical equipment of an aircraft engine or its environment
11/01/2007WO2007122307A1 Air inlet lip for a pod with electric defrosting
11/01/2007CA2643023A1 Air inlet lip for a pod with electric defrosting
10/2007
10/31/2007EP1849985A1 Twisted elbow-shaped propelling gas exhaust assembly in an aircraft
10/31/2007EP1849984A1 Propelling gas exhaust assembly in an aircraft with two elbow-shaped channels
10/31/2007EP1849983A1 Elbow-shaped propelling gas exhaust assembly in an aircraft
10/31/2007CN200967562Y High subsonic speed unmanned plane
10/28/2007CA2585920A1 Exhaust assembly forming a horizontal elbow for propulsion gases in an aircraft
10/28/2007CA2585879A1 Exhaust assembly for propulsion gases in an aircraft with twist elbow
10/28/2007CA2585878A1 Exhaust assembly for propulsion gases in an aircraft forming an elbow
10/24/2007EP1847458A2 Diffusing air inlet door assembly
10/18/2007WO2006057653A3 Integrated air inlet system for multi-propulsion aircraft engines
10/17/2007EP1845018A2 Acoustic nacelle inlet lip having composite construction and an integral electric ice protection heater disposed therein
10/10/2007EP1843022A2 System and method for providing air to a compresssor of an aircraft auxiliary gas turbine engine
10/10/2007EP1699697B1 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
10/09/2007US7278257 Turbojet electromechanical thrust reverser with synchronized locking devices
10/09/2007CA2394296C Air intake for large-size nacelle with enhanced transportability
10/05/2007CA2582806A1 System and method for providing air to a compressor of an aircraft auxiliary gas turbine engine
10/04/2007WO2007110494A1 Structure for an air inlet lip of an electric de-icing pod comprising an acoustic attenuation zone
10/04/2007WO2007110491A1 Air inlet shroud structure
10/04/2007CA2644592A1 Structure for an air inlet lip of an electric de-icing pod comprising an acoustic attenuation zone
10/04/2007CA2637901A1 Air inlet shroud structure
09/2007
09/27/2007WO2007108787A2 Pre-hung inlet door system
09/27/2007WO2007090011A3 Engine air intake barrier filter system for aircraft
09/27/2007US20070221790 Ducted Fan Air Data System
09/27/2007CA2581822A1 Auxiliary gas turbine engine assembly, aircraft component and controller
09/26/2007CN101041385A De-icing system for the inlet cone of an aircraft turboengine
09/25/2007CA2292914C Air intake structure for aircraft engine
09/16/2007CA2581827A1 Low noise exhaust ducting system
09/12/2007CN101033007A Airplane intake lip
09/11/2007US7267297 Integrated axially varying engine muffler, and associated methods and systems
09/06/2007US20070205323 Engine assembly for aircraft
08/2007
08/15/2007EP1818257A2 Integrated inward turning inlets and nozzles for hypersonic air vehicles
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