Patents for B64D 33 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for (2,926)
07/2009
07/02/2009CA2709766A1 Aircraft cooling system
07/02/2009CA2709331A1 Acoustic processing structure particularly adapted to the air inlet of an aircraft nacelle
07/02/2009CA2705598A1 Aircraft nacelle guidance system installation
07/01/2009CN100507252C Fluidic chevrons and configurable thermal shield for jet noise reduction
06/2009
06/25/2009WO2009077690A2 Aircraft nacelle including an optimised ice treatment system
06/25/2009WO2009077689A2 Air outlet system for aircraft leading edge
06/25/2009WO2009077688A2 Aircraft nacelle including hot air discharge means
06/25/2009WO2009077666A2 Piezoelectric de-icing of an air inlet
06/25/2009CA2707655A1 Aircraft nacelle including an optimised ice treatment system
06/25/2009CA2707636A1 Air outlet system for aircraft leading edge
06/25/2009CA2707501A1 Aircraft nacelle including hot air discharge means
06/25/2009CA2700187A1 Piezoelectric de-icing of an air inlet
06/24/2009EP2072779A2 Fan nacelle flow control and method of controlling a boundary layer at the inlet of a fan nacelle
06/24/2009EP2072398A2 Nacelle assembly having inlet bleed
06/21/2009CA2647570A1 Heat exchange system in a turbomachine
06/21/2009CA2646663A1 Recirculation valve in an aircraft engine
06/18/2009US20090152406 Rotating auxiliary power unit air inlet door
06/17/2009EP2069624A1 Removable air intake structure for turbojet engine nacelle
06/11/2009WO2009055041A3 Low shock strength propulsion system
06/10/2009DE10361722B4 Stauluftkanal zur Umgebungsluftzufuhr in einem Flugzeug Ram air duct to the ambient air in an aircraft
06/10/2009CN100497092C Backpack S-shaped inlet channel
06/09/2009US7543777 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
06/09/2009CA2382390C Air inlet duct and flying apparatus, especially a missile, equipped with such duct
06/03/2009EP2065305A1 Air intake for a turboshaft engine equipped with a controlled filtering system
05/2009
05/28/2009US20090133376 Combined gearbox breather and drain mast for jet aircraft engine
05/27/2009EP2061964A1 Turbofan engine having inner fixed structure including ducted passages
05/20/2009EP2060489A2 Nacelle flow assembly
05/14/2009WO2009060137A2 Air intake structure to be mounted upstream of a nacelle middle structure for aircraft engine, and nacelle equipped with such air intake structure
05/14/2009CA2700087A1 Air intake structure to be mounted upstream of a nacelle middle structure for aircraft engine, and nacelle equipped with such air intake structure
05/07/2009US20090114774 Multi-path inlet for aircraft engine
05/06/2009CN101426681A Integrated engine exhaust systems and methods for drag and thermal stress reduction
05/06/2009CN100484836C Air guiding flap, process for adjusting the position of the air guiding flap and ram air system including the air guiding flap
04/2009
04/30/2009WO2009055041A2 Low shock strength propulsion system
04/29/2009EP2052970A2 Aero-acoustic aviation engine inlet for aggressive noise abatement
04/29/2009EP2052967A1 Improvement for rotorcraft equipped with turboshaft engines
04/22/2009EP2050948A2 A gas turbine engine assembly with a variable area nozzle and a method of controlling this nozzle
04/22/2009CN101415607A Air inlet lip for a pod with electric defrosting
04/21/2009US7520465 Aircraft fluid cooling system and aircraft provided with said system
04/16/2009WO2009048713A1 Ceramic heat shield
04/16/2009WO2009047399A1 Nacelle comprising at least one surge trap
04/16/2009WO2009024662A3 Coupling system connecting an internal structure and an external structure of a jet engine nacelle
04/16/2009CA2696779A1 Nacelle comprising at least one surge trap
04/15/2009EP1943419A4 Infrared suppression system
04/15/2009CN101410300A Air inlet shroud structure
04/08/2009CN201217501Y Suspending type aviation camera shooting self-determination aircraft system
04/08/2009CN101405184A Structure for an air inlet lip of an electric de-icing pod comprising an acoustic attenuation zone
04/02/2009US20090084889 Aircraft having a reduced acoustic signature
04/01/2009EP2040818A2 Aircraft engine inlet pivotable barrier filter
03/2009
03/25/2009CN100472116C Holding device for fire detection system
03/24/2009US7506839 Engine airframe J-seal damper
03/24/2009CA2635565A1 Flexible fitting for rigid tubing assembly
03/19/2009US20090072095 Smoke generation device for aircraft and aircraft fitted with such a device
03/19/2009US20090072044 Convergent Divergent Nozzle With Slot Cooled Nozzle Liner
03/17/2009US7503425 Integrated inlet attachment
03/12/2009US20090065297 Dual action inlet door and method for use thereof
03/12/2009DE202008015934U1 Triebwerk Frontschutzabdeckung Engine Front cover
03/11/2009EP2034159A2 Active flow control for nacelle air intake
03/11/2009EP2032829A1 Engine exhaust system with directional nozzle
03/11/2009EP2032828A2 Engine exhaust system
03/11/2009EP2032433A2 Airfoil having a movable control surface
03/11/2009CN101384486A Isentropic compression inlet for supersonic aircraft
03/05/2009WO2009027591A1 Jet engine nacelle equipped with a system for mechanically inhibiting a thrust reverser
03/05/2009CA2696393A1 Jet engine nacelle equipped with a system for mechanically inhibiting a thrust reverser
03/04/2009CN201201716Y Protector for propeller type airplane turbine engine
02/2009
02/26/2009WO2009024662A2 Coupling system connecting an internal structure and an external structure of a jet engine nacelle
02/26/2009WO2009024660A1 Nacelle with an adaptable outlet section
02/26/2009WO2009024461A1 Nacelle equipped with at least one excess pressure flap
02/26/2009WO2008143696A3 Ram air inlets for use with aircraft environmental control systems and other aircraft and non-aircraft systems
02/26/2009CA2696792A1 Nacelle with an adaptable outlet section
02/26/2009CA2696712A1 Nacelle equipped with at least one excess pressure flap
02/26/2009CA2696359A1 Coupling system connecting an internal structure and an external structure of a jet engine nacelle
02/25/2009EP2028359A2 Gas turbine engine with axial movable fan variable area nozzle
02/25/2009EP2028104A2 Generator for gas turbine engine having DC bus fault short circuit control using a battery
02/25/2009EP1699698B1 Ram air channel for the supply of ambient air in an aircraft
02/17/2009US7491253 Engine intake system with accessible, interchangeable air filters
02/17/2009CA2359239C Aircraft propulsive power unit
02/05/2009US20090032615 Arrangement for controlling fluid jets injected into a fluid stream
01/2009
01/29/2009WO2008142289A3 Air intake arrangement for a vehicle, in particular an aircraft
01/29/2009US20090025362 Infrared suppression system with spiral septum
01/22/2009WO2008142242A3 Nacelle rear assembly for turbojet engine
01/15/2009WO2009007564A2 Turbojet engine for aircraft
01/15/2009US20090014598 Aircraft engine nacelle inlet having access opening for electrical ice protection system
01/15/2009US20090014597 Supersonic aircraft jet engine
01/15/2009US20090014234 Acoustic Panel
01/15/2009CA2690601A1 Turboreacteur pour aeronef
01/14/2009EP2014551A1 Device and method for protecting an aircraft component from collision with flying objects
01/08/2009US20090008509 Aircraft engine nacelle inlet having access opening for electrical ice protection system
01/08/2009US20090008508 Variable contour nacelle assembly for a gas turbine engine
01/06/2009CA2628519A1 Electric motor driven lubrication pump control system and method that accommodates turbomachine windmill operation
12/2008
12/31/2008WO2009001002A1 Coating for acoustic treatment including a rime hot-air treating function
12/31/2008WO2008130725A3 Comb for inlet barrier filter system
12/31/2008CA2689495A1 Coating for acoustic treatment including a rime hot-air treating function
12/30/2008US7469528 Aircraft braking method and ducted fan jet engine for implementing the method
12/25/2008US20080315043 Emergency Ram Air Inlet Valve of an Aircraft
12/25/2008US20080315042 Thrust generator for a propulsion system
12/25/2008US20080315012 Method and System for Regulating Internal Fluid Flow Within an Enclosed or Semi-enclosed Environment
12/25/2008CA2626926A1 Cooling systems for use on aircraft
12/24/2008EP1797311B1 Quiet chevron/tab exhaust eductor system
12/18/2008WO2008152259A2 Acoustic panel having a variable acoustic characteristic
12/18/2008US20080308684 Nacelle with articulating leading edge slates
1 ... 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 ... 30