| Patents for B64D 33 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for (2,926) |
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| 03/27/2013 | EP2572984A1 Tiltrotor vectored exhaust system |
| 03/27/2013 | EP2571765A2 Aerodynamic element for an aircraft nacelle |
| 03/27/2013 | EP2571686A1 Ceramic matrix composite structures, components formed therewith, and methods of producing |
| 03/27/2013 | CN103003872A Acoustic panel for a turbojet engine nacelle, with in-built fasteners |
| 03/27/2013 | CN103003151A Aerodynamic element for an aircraft nacelle |
| 03/21/2013 | CA2790062A1 Ram air turbine with integrated heat exchanger |
| 03/20/2013 | CN102985677A Aircraft turbo jet engine fan casing |
| 03/20/2013 | CA2789329A1 Tiltrotor vectored exhaust system |
| 03/14/2013 | US20130062425 System and method for damping combustor nozzle vibrations |
| 03/14/2013 | US20130062424 Low shock strength propulsion system |
| 03/13/2013 | CN202783786U Aircraft air duct isolation channel |
| 03/07/2013 | WO2011144567A3 Method and device for supplying cooling air to an engine, in particular an aircraft engine, gas turbine, or the like |
| 03/07/2013 | DE102011112254A1 Jet engine for aircraft, has accessory gearbox that is coupled to auxiliary units for maintaining temperature of lubrication and cooling agent in tank device integrated in intermediate housing |
| 03/06/2013 | EP2563667A1 Reverser having doors |
| 02/27/2013 | CN102947182A Air inlet duct for a turbojet nacelle |
| 02/21/2013 | US20130042922 Air inlet arrangement and method of making the same |
| 02/20/2013 | EP2559618A2 Ice protection system for a multi-segment aircraft component |
| 02/20/2013 | CN202743482U Unmanned space fighter |
| 02/13/2013 | CN102933462A Turbojet engine nacelle |
| 02/13/2013 | CN102926888A Stealth exhaust system |
| 02/13/2013 | CN102923310A Aircraft supplemental liquid cooler and method |
| 02/13/2013 | CN102923309A Invisible air intake system |
| 02/12/2013 | CA2502374C Methods and apparatus for exhausting gases from gas turbine engines |
| 02/07/2013 | WO2013017680A1 Aircraft propulsion architecture integrating an energy recovery system |
| 02/07/2013 | US20130032642 Secondary-air nozzle of a two-flow jet engine having separated flows including a grid thrust reverser |
| 02/07/2013 | CA2843802A1 Aircraft propulsion architecture integrating an energy recovery system |
| 02/06/2013 | EP2554822A2 Linking device more specifically suited to providing the link between an air intake and an engine of an aircraft nacelle |
| 02/06/2013 | EP2554481A2 Linking device more specifically suited to providing the link between an air intake and an engine of an aircraft nacelle |
| 02/06/2013 | EP2554480A2 Linking device more specifically suited to providing the link between an air intake and an engine of an aircraft nacelle |
| 02/06/2013 | EP2554479A2 Linking device more specifically suited to providing the link between an air intake and an engine of an aircraft nacelle |
| 02/06/2013 | CN102910293A APU selective cool down cycle |
| 01/29/2013 | US8360358 Ram air duct flap arrangement and ram air duct |
| 01/26/2013 | CA2783790A1 Gas turbine engine with ejector |
| 01/24/2013 | US20130020433 Reduced flow field velocity for a propulsor |
| 01/24/2013 | CA2772334A1 Reduced flow field velocity for a propulsor |
| 01/23/2013 | EP2548805A2 Fan motor cooling and method |
| 01/23/2013 | EP2548804A1 Nacelle for propulsion assembly with variable ejector nozzle |
| 01/23/2013 | CN102887230A Re-improved inlet for third-generation light fighter |
| 01/23/2013 | CN102887229A Anti-buckling connection device for piping system |
| 01/22/2013 | CA2703108C Passive cooling system for auxiliary power unit installation |
| 01/22/2013 | CA2502816C Forced air cooling system |
| 01/20/2013 | CA2783156A1 Anti-buckling connecting device for piping |
| 01/18/2013 | CA2783253A1 Aircraft versatile power system |
| 01/16/2013 | CN102883872A Seamless acoustic liner |
| 01/15/2013 | CA2703166C Passive cooling system for auxiliary power unit installation |
| 01/09/2013 | EP2543600A2 Sound absorber for an auxiliary engine of an aircraft |
| 01/09/2013 | EP2542401A2 Seamless acoustic liner |
| 01/09/2013 | CN101678898B Nacelle rear assembly for turbojet engine |
| 01/03/2013 | WO2013000036A1 An air cooling system for an unmanned aerial vehicle |
| 01/03/2013 | US20130001369 Auxiliary power unit inlet |
| 01/03/2013 | US20130001321 Hybrid exhaust component |
| 01/03/2013 | US20130001319 Impingement cooled nozzle liner |
| 01/02/2013 | CN102858636A Reverser having doors |
| 01/02/2013 | CN102849216A Auxiliary power unit inlet |
| 01/02/2013 | CN101960166B Device for supporting and securing a piece of equipment on an aircraft engine or nacelle case |
| 12/26/2012 | EP2537754A1 Method for producing an acoustic treatment panel including channels adjacent to a cellular structure |
| 12/26/2012 | EP2537753A1 Method for producing an acoustic treatment panel including the function of de-icing with hot air |
| 12/26/2012 | CN102844527A Exhaust gas diffuser of gas turbine |
| 12/26/2012 | CN102837827A Process for the production of an acoustic treatment panel that integrates channels juxtaposed with an alveolar structure |
| 12/19/2012 | EP2535271A1 Air intake of an aircraft nacelle including a reinforced lip with a Joule effect de-icing system |
| 12/19/2012 | CN102826229A Air inlet partition of air vehicle |
| 12/19/2012 | CN102826228A Air intake of aircraft nacelle |
| 12/19/2012 | CN102826227A Unmanned space fighter |
| 12/18/2012 | US8333344 Aircraft nacelle guidance system installation |
| 12/18/2012 | US8333343 Jet engine nacelle intended to equip an aircraft |
| 12/18/2012 | CA2654751C Engine exhaust system |
| 12/18/2012 | CA2652685C Engine exhaust system with directional nozzle |
| 12/12/2012 | CN102817715A Third-generation heavy fighter novel gas inlet channel lip |
| 12/06/2012 | WO2012164187A1 Air inlet structure for turbojet engine nacelle |
| 12/06/2012 | WO2012118516A8 Ceramic matrix composite structures, components formed therewith, and methods of producing |
| 12/06/2012 | DE102011103163A1 Gasturbinentriebwerk mit teleskopartigem Lufteinlass der Triebwerksverkleidung Gas turbine engine with telescopic air intake of the engine cowling |
| 12/06/2012 | CA2837605A1 Air inlet structure for turbojet engine nacelle |
| 12/05/2012 | EP2530017A2 Laminate thermal insulation blanket for aircraft applications and process therefor |
| 12/05/2012 | EP2528813A1 Electrothermal heater mat |
| 11/30/2012 | CA2777999A1 Laminate thermal insulation blanket for aircraft applications and process therefor |
| 11/29/2012 | WO2012160375A1 A structural element of an air vehicle air intake composed of an array of passages with a hexagonal cross section |
| 11/28/2012 | EP2527253A1 De-icing device for an aviation gas turbine engine |
| 11/22/2012 | US20120292455 Auxiliary power unit inlet duct screen assembly |
| 11/22/2012 | US20120292440 Mass flow increase at takeoff in supersonic airliner |
| 11/22/2012 | US20120291416 Crack and Delamination Stoppers For Aircraft Propulsion System Components |
| 11/21/2012 | CN101772454B Nacelle comprising at least one surge trap |
| 11/15/2012 | US20120286066 Variable geometry turbomachine |
| 11/14/2012 | EP2522831A2 Turbojet engine with oil cooler in the engine nacelle |
| 11/14/2012 | CN101622174B Acoustic lining for an aircraft, including a frost treatment system using the joule effect |
| 11/13/2012 | US8307659 Nozzle with guiding elements |
| 11/13/2012 | CA2531699C Auxiliary power unit intake duct with aero-acoustic guide vanes |
| 11/13/2012 | CA2491260C Fire shield apparatus and method |
| 11/01/2012 | WO2012148394A1 Self-aligning inlet plenum system for rotorcraft |
| 11/01/2012 | WO2012148318A1 Adjustable supersonic air inlet |
| 11/01/2012 | CA2830938A1 Self-aligning inlet plenum system for rotorcraft |
| 10/31/2012 | EP2517955A2 Aircraft configuration |
| 10/31/2012 | EP2516271A1 Nacelle incorporating an element for connecting a lip and an acoustic attenuation panel together |
| 10/31/2012 | EP2516270A1 Acoustic treatment panel having scalable thickness |
| 10/31/2012 | CN102758667A Integrated tailcone muffler assemblies and methods |
| 10/31/2012 | CN101267986B Aircraft engine assembly comprising an engine and a suspension pylon for such an engine |
| 10/24/2012 | EP2512927A2 Aircraft nacelle air intake incorporating optimized ice-treatment hot air injection means |
| 10/24/2012 | CN102745332A Pneumatic type power augmenting device |
| 10/23/2012 | US8292217 Hypersonic inlet systems and methods |
| 10/18/2012 | US20120261522 Modular externally accessible batteries for an aircraft |
| 10/11/2012 | US20120256045 Airborne cooling system |