Patents
Sitemap › B64 - Aircraft; Aviation; Cosmonautics › B64D - Equipment for fitting in or to aircraft; Flying suits; Parachutes; Arrangements or mounting of power plants or propulsion transmissions › B64D 33 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
Patents for B64D 33 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for (2,926)
12/2010
12/08/2010CN101910000A Nacelle for turbojet engine
12/08/2010CN101909998A Aircraft nacelle guidance system installation
12/07/2010US7845188 System for the preparation of compressed air
12/02/2010WO2010136369A1 Aircraft engine nacelle comprising a mobile cowl moved by electric motors
12/02/2010US20100301161 Acoustic coating for an aircraft incorporating a frost treatment system by joule effect
12/02/2010CA2761761A1 Aircraft engine nacelle comprising a mobile cowl moved by electric motors
12/01/2010EP2254795A1 Engine inlet flap for mounting on the housing of an air inlet of an aircraft engine and engine fitted with such an engine inlet flap and aircraft system
12/01/2010CN101903245A Aircraft cooling system
12/01/2010CN101903244A Device for cooling hot gas to be discharged from an aircraft
12/01/2010CN101903241A Ice protection system for a multi-segment aircraft component
12/01/2010CN101041385B De-icing system for the inlet cone of an aircraft turboengine
11/2010
11/25/2010WO2010089498A3 Turbojet engine nacelle
11/25/2010WO2010086560A3 Aircraft nacelle including an optimised acoustic processing system
11/25/2010US20100294882 Aircraft leading edge
11/24/2010EP2252512A2 Device for reducing turboprop infrared emissions
11/23/2010US7837142 Supersonic aircraft jet engine
11/19/2010CA2664559A1 Jet engine protector screen
11/18/2010US20100290892 Intake duct liner for a turbofan gas turbine engine
11/17/2010EP2251261A2 An intake duct liner for a turbofan gas turbine engine
11/17/2010EP2250357A1 Air intake structure for an aircraft nacelle
11/17/2010EP2250090A2 Icing protection for aircraft air inlet scoops
11/16/2010US7832684 Ram air channel for the supply of ambient air in an aircraft
11/10/2010EP2247787A2 Core having a high shear strength and articles made from same
11/10/2010EP2247501A2 Wing-propulsion unit combination, airplane and wing section of an airplane comprising a propulsion unit tap air channel arrangement
11/09/2010CA2486172C Variable area thrust reverser nozzle
11/04/2010US20100276548 Acoustic processing structure particularly adapted to the air inlet of an aircraft nacelle
11/03/2010EP2245332A1 Device for supporting and securing a piece of equipment on an aircraft engine or nacelle case
11/03/2010EP2244939A1 Acoustic processing structure particularly adapted to the air inlet of an aircraft nacelle
11/02/2010US7823624 Heat exchanger, propulsion unit, and aircraft comprising such a propulsion unit
10/2010
10/21/2010WO2010119210A1 Actuator system for a mobile panel of a nacelle of a turbojet
10/21/2010WO2009118470A8 Device for supporting and securing a piece of equipment on an aircraft engine or nacelle case
10/21/2010DE102009017039A1 Stauluftauslasskanal Ram air outlet
10/21/2010CA2758134A1 Actuator system for a mobile panel of a nacelle of a turbojet
10/20/2010EP2241504A2 Nacelle for aircraft engines
10/19/2010CA2389525C Variable cycle propulsion device employing exhaust bypass for supersonic aircraft, and operating process
10/14/2010DE202010010427U1 Vorrichtung zur Verringerung von Schäden durch Vogelschlag an Triebwerken Apparatus for reducing damage caused by bird strikes on engines
10/13/2010EP2238031A1 Air intake for aircraft nacelle, and propulsion assembly including such air intake
10/12/2010CA2510218C Hingeless flapper valve for flow control
10/07/2010US20100252688 Device and method for converting supplied electrical power into mechanical power to start at least one engine
10/06/2010EP2234886A1 Nacelle for turbojet engine
10/06/2010CN101855135A Air intake structure to be mounted upstream of a nacelle middle structure for aircraft engine, and nacelle equipped with such air intake structure
10/06/2010CN101253095B Dynamically self-locking catching device
09/2010
09/30/2010WO2010109152A2 Aircraft nacelle comprising a reinforced outer wall
09/30/2010US20100243370 Aero-acoustic aviation engine inlet for aggressive noise abatement
09/30/2010US20100242484 Apparatus and method for cooling gas turbine engine combustors
09/29/2010EP2233727A2 Fuel-cooled flexible heat exchanger with thermoelectric device compression
09/29/2010EP2231474A2 Aircraft nacelle including an optimised ice treatment system
09/29/2010CN101844621A Airborne combined cooling and heating and power system of multi-electric aircraft
09/28/2010US7802752 Jet engine noise suppressor
09/28/2010CA2398422C Compressor air drawing off system
09/23/2010WO2010107802A1 Co-polymer based polyimide articles and their uses in an aircraft
09/23/2010US20100237200 Turbojet engine for aircraft, propulsion unit comprising such a turbojet engine and aircraft comprising such a propulsion unit
09/23/2010DE102009013159A1 Radiator for aircraft cooling system, has matrix body including coolant channels extending from surface of matrix body to another surface of matrix body so that coolant flows through matrix body
09/23/2010CA2752047A1 Co-polymer based polyimide articles and their uses in an aircraft
09/21/2010US7798285 Acoustic barrel for aircraft engine nacelle including crack and delamination stoppers
09/21/2010CA2551932C 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 includingsuch an air guiding flap
09/16/2010US20100230530 Helicopter
09/14/2010CA2389531C Variable cycle propulsion device employing mechanical transmission for supersonic aircraft
09/09/2010DE102009011635A1 Luftleitelement eines Laufspalteinstellungssystems einer Fluggasturbine Air directing a running gap adjustment system of an aircraft gas turbine
09/08/2010EP2226486A1 Method for manufacturing an ejector nozzle tube
09/08/2010EP2225157A1 Device for cooling hot gas to be discharged from an aircraft
09/08/2010EP2225156A1 Aircraft propulsion assembly comprising hot air bleed systems
09/07/2010CA2475208C Control system for vertical take off and land (vtol) aircraft
09/02/2010DE102009010524A1 Turbopropantrieb mit Druckpropeller Turboprop engine with pusher propeller
09/02/2010DE102009010243A1 Leistungserzeugungs-Vorrichtung sowie Rumpf-Bauteil mit einer solchen Leistungserzeugungs-Vorrichtung Power generation device and inflatable component with such a power generating device
09/01/2010EP2223856A2 Turboprop engine with pusher propeller
09/01/2010EP2222561A1 Aircraft cooling system
09/01/2010EP2222560A1 Aircraft nacelle guidance system installation
09/01/2010CN101821165A Coating for acoustic treatment including rime hot-air treating function
08/2010
08/25/2010EP2219948A2 Air outlet system for aircraft leading edge
08/25/2010EP2219947A2 Ice protection system for a multi-segment aircraft component
08/20/2010CA2692745A1 Compressor wash nozzle integrated in an inlet case strut
08/19/2010US20100206664 Acoustic panel
08/12/2010WO2010089498A2 Turbojet engine nacelle
08/12/2010WO2010089497A1 Method for making a network of drainage pipes and acoustic processing panel including such a network of drainage pipes
08/12/2010WO2010089496A1 Acoustic processing panel, more particularly adapted for an air intake in an aircraft nacelle
08/12/2010CA2751121A1 Turbojet engine nacelle
08/10/2010CA2455222C Methods and apparatus for operating gas turbine engines
08/05/2010WO2010086560A2 Aircraft nacelle including an optimised acoustic processing system
08/05/2010DE102009006579A1 Sound absorber for auxiliary engine of aircraft, has inlet, outlet, housing, and flow channel which has porous wall material and is arranged in housing
08/04/2010EP2212532A2 Low shock strength inlet
07/2010
07/29/2010WO2009085380A3 Low shock strength inlet
07/29/2010WO2009060137A3 Air intake structure to be mounted upstream of a nacelle middle structure for aircraft engine, and nacelle equipped with such air intake structure
07/29/2010CA2690780A1 Dual channel regulated fuel-oil heat exchanger
07/27/2010CA2389529C Variable cycle propulsion device employing compressed air bleed for supersonic aircraft
07/22/2010WO2010059301A3 Integrated inlet design
07/22/2010US20100181436 Relating to air-breathing flight vehicles
07/22/2010US20100181420 Coating for acoustic treatment that integrates the function of hot-air treatment of frost
07/22/2010US20100181416 Unmanned helicopter
07/21/2010CN201530477U Exhausting equipment of unmanned aircraft
07/21/2010CN101784449A Nacelle with an adaptable outlet section
07/21/2010CN101784444A Jet engine nacelle equipped with a system for mechanically inhibiting a thrust reverser
07/21/2010CN101575008B Airborne combined cooling and heating system for multi-electric aircraft
07/15/2010WO2009156120A8 Air duct for supplying ambient air in an aircraft
07/14/2010CN101778765A Coupling system connecting an internal structure and an external structure of a jet engine nacelle
07/14/2010CN101778761A Nacelle equipped with at least one excess pressure flap
07/13/2010US7753311 Propulsion system, aircraft comprising the propulsion system and an outlet device for a jet engine
07/08/2010WO2010077241A1 Engine air particle separator
07/08/2010WO2010040837A3 Sound absorber for an auxiliary engine of an aircraft
07/08/2010CA2748257A1 Method and systems for an engine starter/generator
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