| Patents for B64D 33 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for (2,926) |
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| 05/18/2011 | EP2321510A2 Assembly of components connected by a device that maintains the integrity of the surface of one of the components |
| 05/18/2011 | CN102066198A Aircraft engine nacelle air intake assembly |
| 05/17/2011 | US7941923 Drilled and integrated secondary fuel nozzle and manufacturing method |
| 05/12/2011 | WO2010105744A4 Cooler for an aircraft cooling system, aircraft cooling system and method for operating an aircraft cooling system |
| 05/12/2011 | US20110108676 Air inlet for an aircraft turbine engine, an aircraft provided with such an air inlet, and a method of optimizing the operation of an aircraft turbine engine with the help of an air inlet |
| 05/12/2011 | CA2720521A1 Air inlet of an aircraft turbine engine, aircraft equipped with such an air inlet and process for optimizing the operation of an aircraft turbine engine through an air inlet |
| 05/11/2011 | EP2318679A1 Inner wall for the nacelle of a turbine engine |
| 05/11/2011 | EP2178751B1 Nacelle equipped with at least one excess pressure flap |
| 05/11/2011 | EP1924498B1 Dynamically self-locking catching device |
| 05/11/2011 | CN102057144A Method of depositing a coating for improving laminar flow |
| 05/11/2011 | CN102056803A Measurement instrument support interposed between a drive unit and an air intake of an aircraft nacelle |
| 05/10/2011 | US7938224 Coating for acoustic treatment integrating the function of frost treatment with hot air |
| 05/10/2011 | US7938214 Motor cooling system |
| 05/03/2011 | US7934582 Engine silencing and vibration reduction system and method |
| 04/28/2011 | WO2011002886A3 Aircraft fluid check valve assembly with indexing |
| 04/28/2011 | WO2011002879A3 Aircraft low clearance fluid check valve |
| 04/21/2011 | WO2011046580A2 Bird deflector and air replacement system |
| 04/20/2011 | EP2311731A1 Thurst reverser actuation |
| 04/20/2011 | EP2310267A1 Method for making deicing system on a nacelle panel |
| 04/19/2011 | CA2648765C Jet engine nozzle exit configurations, including projections oriented relative to pylons, and associated systems and methods |
| 04/13/2011 | EP2307276A2 Air duct for supplying ambient air in an aircraft |
| 04/13/2011 | CN102015450A Wave attenuation panel inserted between the motor and air inlet of an aircraft nacelle |
| 04/12/2011 | US7923668 Acoustic nacelle inlet lip having composite construction and an integral electric ice protection heater disposed therein |
| 04/12/2011 | US7921966 Linear acoustic liner |
| 04/12/2011 | CA2464830C Fluidic chevrons and configurable thermal shield for jet noise reduction |
| 04/06/2011 | EP2305985A2 Containment casing for an aero engine |
| 04/06/2011 | EP2304204A1 Method of depositing a coating for improving laminar flow |
| 04/06/2011 | EP2303689A1 Personal flight device incorporating radiator cooling passage |
| 03/31/2011 | US20110073716 Ram Air Duct Flap Arrangement And Ram Air Duct |
| 03/30/2011 | EP2301845A2 Thrust reverser actuation |
| 03/30/2011 | CN101998922A Acoustic treatment panel with integral connecting reinforcement |
| 03/24/2011 | US20110068222 Propulsion unit for an aircraft and air intake structure for such a unit |
| 03/24/2011 | DE102009029540A1 Device for protection of turbo engines from impact of external bodies, e.g. bird strike, is provided at air inlet of turbo engine and has aerodynamic protection elements |
| 03/23/2011 | EP2178754B1 Nacelle comprising at least one overpressure valve |
| 03/17/2011 | WO2010105744A3 Cooler for an aircraft cooling system, aircraft cooling system and method for operating an aircraft cooling system |
| 03/17/2011 | US20110062290 Supersonic aircraft jet engine installation |
| 03/16/2011 | EP2295778A2 Energy absorbing fan blade spacer |
| 03/16/2011 | EP2231474B1 Aircraft nacelle including an optimised ice treatment system |
| 03/15/2011 | US7905449 Multi-engine aircraft |
| 03/10/2011 | DE102009035293A1 Aircraft safety device has flexible rod mounted in front direction of flight with radial sensors, which makes birds to swing to side, where one type of formed or rejuvenated semi-spherical dome is attached at front side |
| 03/09/2011 | EP2291310A2 Coupling for inducing high temperature drops between connected parts on an aircraft |
| 03/08/2011 | US7900460 Outlet device for a jet engine and a jet engine comprising such an outlet device |
| 03/02/2011 | EP2288797A1 Propulsion unit for an aircraft and air intake structure for such a unit |
| 03/02/2011 | EP2288543A1 Aircraft engine nacelle air intake assembly |
| 03/02/2011 | EP1910168B1 Control of engine intake door |
| 02/24/2011 | WO2010077766A3 Method and systems for an engine starter/generator |
| 02/23/2011 | EP2285682A2 Measurement instrument support interposed between a drive unit and an air intake of an aircraft nacelle |
| 02/23/2011 | EP2148815B1 Air intake arrangement for a vehicle, in particular an aircraft |
| 02/22/2011 | US7891671 Panel assembly including deformable seal |
| 02/16/2011 | CN101977814A Device for reducing turboprop infrared emissions |
| 02/16/2011 | CN101549758B Intake and exhaust device of air breathing supersonic/hypersonic aerocraft |
| 02/09/2011 | EP2282031A1 Filtering device with integrated bypass for an air inlet |
| 02/09/2011 | CN101970296A Air intake lip for turbojet nacelle |
| 02/08/2011 | US7883053 Heat exchanger systems and associated systems and methods for cooling aircraft starter/generators |
| 02/03/2011 | WO2010018314A8 Inner wall for the nacelle of a turbine engine |
| 02/02/2011 | CN101965425A Core having a high shear strength and articles made from same |
| 01/27/2011 | US20110017426 Aircraft cooling system |
| 01/26/2011 | EP2278672A2 Electrical cable shroud |
| 01/26/2011 | CN1384794B Supersonic external-compression air ducts, diffuser and air ducts system |
| 01/26/2011 | CN101960166A Device for supporting and securing a piece of equipment on an aircraft engine or nacelle case |
| 01/20/2011 | WO2011007074A1 Leading edge structure, in particular for the air intake of the nacelle of an aircraft engine |
| 01/20/2011 | DE102009032841A1 Geräuschreduziertes Flugzeugtriebwerk sowie Verfahren zur Verminderung von Geräuschemissionen eines Flugzeugtriebwerks Reduced noise aircraft engine and method for reducing noise emissions of an aircraft engine |
| 01/20/2011 | CA2767870A1 Leading edge structure, in particular for the air intake of the nacelle of an aircraft engine |
| 01/19/2011 | EP2275347A2 Low-noise aircraft engine and method for minimising noise emissions from an aircraft engine |
| 01/19/2011 | EP2274205A2 Wave attenuation panel inserted between the motor and air inlet of an aircraft nacelle |
| 01/19/2011 | EP2274204A1 Fluid dynamic device with thrust control shroud |
| 01/19/2011 | CN201712791U Aircraft opening cover with exhaust function |
| 01/19/2011 | CN101952573A Air intake structure for an aircraft nacelle |
| 01/19/2011 | CN101952171A Aircraft propulsion assembly comprising hot air bleed systems |
| 01/19/2011 | CN101952170A Air outlet system for aircraft leading edge |
| 01/19/2011 | CN101952168A Acoustic processing structure particularly adapted to the air inlet of an aircraft nacelle |
| 01/19/2011 | CN101602407B Hypersonic speed aircraft cooling system based on ammonia water Rankine cycle |
| 01/18/2011 | US7870929 Engine assembly, acoustical liner and associated method of fabrication |
| 01/18/2011 | US7870720 Inlet electromagnetic flow control |
| 01/13/2011 | DE102009061028A1 Cooler for use in aircraft cooling system, has coolant channels extending from one of surfaces of matrix body to another surface of body to allow coolant to flow through body, where body is designed to form section of outer skin of aircraft |
| 01/11/2011 | US7866599 Integrated inward turning inlets and nozzles for hypersonic air vehicles |
| 01/11/2011 | US7866440 System for joining acoustic cellular panel sections in edge-to-edge relation |
| 01/11/2011 | CA2478198C Methods and apparatus for flade engine nozzle |
| 01/06/2011 | WO2011002886A2 Aircraft fluid check valve assembly with indexing |
| 01/06/2011 | WO2011002879A2 Aircraft low clearance fluid check valve |
| 01/06/2011 | US20110001019 Ram door assemblies |
| 01/06/2011 | CA2774628A1 Aircraft low clearance fluid check valve |
| 01/06/2011 | CA2766895A1 Aircraft fluid check valve assembly with indexing |
| 01/05/2011 | EP2102060B1 Acoustic lining for an aircraft, including a frost treatment system using the joule effect |
| 01/05/2011 | CN101939222A Engine intake flap for being arranged on the housing of an air intake of an aircraft engine, as well as engine with such an engine intake flap and aircraft system |
| 01/04/2011 | US7861823 Duct for reducing shock related noise |
| 01/04/2011 | CA2646629C Integrated engine exhaust systems and methods for drag and thermal stress reduction |
| 01/04/2011 | CA2638645C Engine having power bus fault short circuit control with a disconnection switch |
| 01/04/2011 | CA2618661C Infrared suppression system |
| 12/30/2010 | US20100327078 Nozzle with an adjustable throat |
| 12/29/2010 | CN101932509A Wing-propulsion unit combination, airplane and wing section of an airplane comprising a propulsion unit tap air channel arrangement |
| 12/28/2010 | US7857257 Aircraft thermal management system with reduced exhaust re-ingestion |
| 12/28/2010 | US7857093 Engine inlet deep acoustic liner section |
| 12/23/2010 | WO2010109152A3 Aircraft nacelle comprising a reinforced outer wall |
| 12/23/2010 | US20100320316 Air intake for aircraft nacelle, and propulsion assembly including such air intake |
| 12/22/2010 | EP2262686A2 Acoustic treatment panel with integral connecting reinforcement |
| 12/21/2010 | US7854395 Rocket combustion chamber with jacket |
| 12/16/2010 | US20100313545 Gas turbine engine nozzle configurations |
| 12/15/2010 | CN101918276A Air intake for aircraft nacelle, and propulsion assembly including such air intake |
| 12/14/2010 | US7849702 Combined cabin air and heat exchanger RAM air inlets for aircraft environmental control systems, and associated methods of use |