| Patents for B64D 33 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for (2,926) |
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| 01/06/2010 | EP2140120A2 Method for making an acoustic treatment coating including a cellular structure with a complex shape, and acoustic treatment coating thus obtained |
| 01/06/2010 | CN101622174A Acoustic lining for an aircraft, including a frost treatment system using the joule effect |
| 12/31/2009 | US20090321585 Nacelle inlet lip |
| 12/30/2009 | WO2009157780A1 Personal flight device incorporating radiator cooling passage |
| 12/30/2009 | WO2009136062A3 Acoustic treatment panel with integral connecting reinforcement |
| 12/30/2009 | WO2009115674A3 Air intake for aircraft engine nacelle, and nacelle equipped with such air intake |
| 12/30/2009 | CA2731205A1 Personal flight device incorporating radiator cooling passage |
| 12/30/2009 | CA2729473A1 Air duct for supplying ambient air in an aircraft |
| 12/29/2009 | US7637455 Inlet distortion and recovery control system |
| 12/24/2009 | US20090314899 Structural element of an aircraft |
| 12/24/2009 | DE102008028987A1 Turboproptriebwerk mit einer Vorrichtung zum Erzeugen eines Kühlluftstroms Turboprop engine with a device for generating a cooling air flow |
| 12/23/2009 | EP2136052A1 Turboprop engine comprising a device for creating a cooling air flow |
| 12/23/2009 | EP1928743B1 Engine assembly for an aircraft comprising an engine as well as an engine mounting structure for such an engine |
| 12/16/2009 | EP2133265A1 Helicopter |
| 12/16/2009 | CN101602407A Hypersonic speed aircraft cooling system based on ammonia water Rankine cycle |
| 12/15/2009 | US7631836 Jet engine nacelle for a supersonic aircraft |
| 12/15/2009 | US7631483 Method and system for reduction of jet engine noise |
| 12/09/2009 | EP2129580A1 Lockable guiding system for a mobile part of a nacelle |
| 12/03/2009 | WO2009125157A3 Turbofan engine nacelle |
| 12/02/2009 | CN100564159C Low-noise aircraft, particularly at take-off and landing |
| 12/01/2009 | US7624944 Tandem air inlet apparatus and method for an airborne mobile platform |
| 11/26/2009 | WO2009142793A2 Ice shed reduction for leading edge structures |
| 11/26/2009 | WO2009122066A3 Air intake lip for turbojet nacelle |
| 11/26/2009 | US20090288902 Hot compressed gas vehicle |
| 11/26/2009 | US20090288711 Microjet creation and control of shock waves |
| 11/26/2009 | CA2722099A1 Ice shed reduction for leading edge structures |
| 11/24/2009 | US7621370 Sound increase apparatus |
| 11/20/2009 | CA2659944A1 Mixed carbon foam/metallic heat exchanger |
| 11/19/2009 | US20090283631 Engine assembly for aircraft comprising an aerodynamic coupling fairing mounted on two separate elements |
| 11/18/2009 | CN101580127A Movement device |
| 11/17/2009 | US7618006 Ram air inlets for use with aircraft environmental control systems and other aircraft and non-aircraft systems |
| 11/13/2009 | CA2665303A1 Starting and generating apparatus for engine |
| 11/12/2009 | WO2009136096A2 Bypass turbojet engine nacelle |
| 11/12/2009 | WO2009136062A2 Acoustic treatment panel with integral connecting reinforcement |
| 11/12/2009 | WO2009135260A1 Fluid dynamic device with thrust control shroud |
| 11/12/2009 | CA2719898A1 Acoustic treatment panel with integral connecting reinforcement |
| 11/12/2009 | CA2719155A1 Bypass turbojet engine nacelle |
| 11/11/2009 | EP2116714A1 Low noise aircraft |
| 11/11/2009 | EP2115290A2 Nacelle for aircraft jet engine and aircraft including such nacelle |
| 11/11/2009 | CN101575008A Airborne combined cooling and heating system for multi-electric aircraft |
| 11/04/2009 | EP2113459A2 Aft inlet duct mounted door actuator |
| 10/29/2009 | WO2009085843A3 Ice protection system for a multi-segment aircraft component |
| 10/28/2009 | EP2112353A1 Aircraft engine nacelle inlet |
| 10/28/2009 | CN100554086C Engine assembly for an aircraft comprising an engine as well as an engine mounting structure for such an engine |
| 10/22/2009 | WO2009108672A3 Core having a high shear strength and articles made from same |
| 10/22/2009 | US20090261208 Aircraft engine inlet pivotable barrier filter |
| 10/20/2009 | US7604199 Aerofoil containment structure |
| 10/20/2009 | US7603843 Combustion chamber comprising a cooling unit and method for producing said combustion chamber |
| 10/15/2009 | WO2009125157A2 Turbofan engine nacelle |
| 10/14/2009 | CN101554924A Device for feeding combustion air to an air craft engines |
| 10/13/2009 | US7600714 Diffusing air inlet door assembly |
| 10/13/2009 | US7600713 Pre-hung inlet door system |
| 10/08/2009 | WO2009122066A2 Air intake lip for turbojet nacelle |
| 10/08/2009 | WO2009122037A2 Device for reducing turboprop infrared emissions |
| 10/08/2009 | CA2718318A1 Air intake lip for turbojet nacelle |
| 10/08/2009 | CA2717357A1 Device for reducing turboprop infrared emissions |
| 10/07/2009 | CN101549758A Intake and exhaust device of air breathing supersonic/hypersonic aerocraft |
| 10/06/2009 | US7597283 Auxiliary power unit intake duct with aero-acoustic guide vanes |
| 10/06/2009 | US7596951 Exhaust nozzle for a gas turbine engine |
| 10/01/2009 | WO2009118470A1 Device for supporting and securing a piece of equipment on an aircraft engine or nacelle case |
| 10/01/2009 | WO2009095257A3 Wing-propulsion unit combination, airplane and wing section of an airplane comprising a propulsion unit tap air channel arrangement |
| 10/01/2009 | WO2009083074A4 Device for cooling hot gas to be discharged from an aircraft |
| 10/01/2009 | CA2716014A1 Device for supporting and securing a piece of equipment on an aircraft engine or nacelle case |
| 09/30/2009 | CN100545037C Annular acoustic panel |
| 09/24/2009 | WO2009115674A2 Air intake for aircraft engine nacelle, and nacelle equipped with such air intake |
| 09/23/2009 | EP2102062A2 Aircraft leading edge |
| 09/23/2009 | EP2102060A2 Acoustic lining for an aircraft, including a frost treatment system using the joule effect |
| 09/17/2009 | WO2009112695A1 Air intake structure for an aircraft nacelle |
| 09/17/2009 | CA2713471A1 Air intake structure for an aircraft nacelle |
| 09/15/2009 | US7588212 Method and apparatus for noise abatement and ice protection of an aircraft engine nacelle inlet lip |
| 09/11/2009 | WO2009109712A1 Air intake for aircraft nacelle, and propulsion assembly including such air intake |
| 09/11/2009 | CA2708106A1 Air intake for aircraft nacelle, and propulsion assembly including such air intake |
| 09/03/2009 | WO2009108672A2 Core having a high shear strength and articles made from same |
| 09/01/2009 | US7581694 Vertical tail unit for aircraft and aircraft equipped with same |
| 09/01/2009 | US7581692 Fluidic chevrons and configurable thermal shield for jet noise reduction |
| 09/01/2009 | CA2371326C Procedure for de-icing a jet engine air inlet cowl by means of forced circulation of a fluid, and device for applying the said procedure |
| 08/25/2009 | US7578452 Ablative composite assemblies and joining methods thereof |
| 08/25/2009 | CA2552166C Ram air channel for the supply of ambient air in an aircraft |
| 08/20/2009 | WO2009077689A3 Air outlet system for aircraft leading edge |
| 08/13/2009 | WO2009098044A1 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 |
| 08/13/2009 | CA2713579A1 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 |
| 08/06/2009 | WO2009095257A2 Wing-propulsion unit combination, airplane and wing section of an airplane comprising a propulsion unit tap air channel arrangement |
| 08/06/2009 | DE102008007469A1 Verlängerungsteil für eine Einlaufklappe, Einlaufklappe mit einem solchen Verlängerungsteil und Triebwerk mit einer Einlaufklappe Extension piece for intake flap, intake flap with such extension part and engine with an intake valve |
| 08/06/2009 | CA2712625A1 A wing-engine combination, an aircraft, and a wing section of an aircraft comprising an engine bleed-air duct arrangement |
| 08/04/2009 | US7568347 Method for designing flowfield molded hypersonic inlet for integrated turbojet and ram-scramjet applications |
| 07/30/2009 | CA2651151A1 Data recorder and storage system for line replaceable unit |
| 07/28/2009 | CA2425982C Uninterruptible oil supply system |
| 07/16/2009 | DE102007061995A1 Vorrichtung zum mechanischen Entkoppeln von Heißgasanschlüssen Device for mechanical decoupling of hot gas connections |
| 07/16/2009 | DE102007061994A1 Vorrichtung zum Kühlen von aus einem Flugzeug abzuführendem Heißgas Device for cooling hot gas to be discharged from an aircraft |
| 07/15/2009 | EP2077963A2 Gas turbine nacelle comprising a passive boundary layer bleed system and method of controlling turbulent airflow |
| 07/09/2009 | WO2009085843A2 Ice protection system for a multi-segment aircraft component |
| 07/09/2009 | WO2009083691A1 Aircraft propulsion assembly comprising hot air bleed systems |
| 07/09/2009 | WO2009083074A1 Device for cooling hot gas to be discharged from an aircraft |
| 07/09/2009 | DE102007061588A1 Flugzeugkühlsystem Aircraft cooling system |
| 07/09/2009 | CA2710445A1 Aircraft propulsion assembly comprising hot air bleed systems |
| 07/09/2009 | CA2690287A1 Device for mechanically decoupled fastening of an aircraft component perfused by hot gas |
| 07/08/2009 | EP2076439A1 System and method for controlling an environment in an aircraft using a vortex cooler |
| 07/02/2009 | WO2009081020A1 Acoustic processing structure particularly adapted to the air inlet of an aircraft nacelle |
| 07/02/2009 | WO2009080904A1 Aircraft nacelle guidance system installation |
| 07/02/2009 | WO2009080168A1 Aircraft cooling system |