| Patents for B64D 33 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for (2,926) |
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| 01/09/2014 | WO2012056155A3 Leading edge structure, in particular for an air inlet of an aircraft engine nacelle |
| 01/09/2014 | US20140008497 Appartus and method for preventing gas turbine engine freezing |
| 01/07/2014 | US8622339 Mass flow increase at takeoff in supersonic airliner |
| 01/03/2014 | WO2014001696A1 Electrical heating unit for a de-icing device |
| 01/03/2014 | CA2876959A1 Electrical heating unit for a de-icing device |
| 01/01/2014 | EP2678226A1 Self-aligning inlet plenum system for rotorcraft |
| 01/01/2014 | CN103492267A Aircraft tail region with a cooling system installed in aircraft tail region |
| 01/01/2014 | CN103482074A Volute cushion boosting propeller |
| 12/25/2013 | EP2675712A1 Aircraft with improved aerodynamic performance |
| 12/25/2013 | CN103476675A Aircraft with improved aerodynamic performance |
| 12/25/2013 | CN103466094A Airplane air inlet pipe capable of preventing birds |
| 12/25/2013 | CN101910000B Nacelle for turbojet engine |
| 12/25/2013 | CN101580127B Movement device |
| 12/18/2013 | CN203345203U Firewall with asymmetric air inlet channels |
| 12/18/2013 | CN203345202U Air inlet channel blocking cover of propeller plane |
| 12/18/2013 | CN203345201U Aircraft ejection system |
| 12/18/2013 | CN103459087A Method of inspecting impacts observed in fan casings |
| 12/17/2013 | US8608106 Aircraft cooling system |
| 12/11/2013 | EP2670663A1 Method for manufacturing an air-intake structure for a turbojet-engine nacelle |
| 12/11/2013 | CN102216158B Air intake for an aeroplane engine with unducted propellers |
| 12/11/2013 | CN102083688B Fluid dynamic device with thrust control shroud |
| 12/11/2013 | CN101952168B Acoustic processing structure particularly adapted to the air inlet of an aircraft nacelle |
| 12/11/2013 | CA2818066A1 Control process and regulation system for supplying compressed air to a compressed air network, specifically in an aircraft |
| 12/10/2013 | US8602156 Multi-splice acoustic liner |
| 12/10/2013 | US8602088 Cooling air supply for the cooling of different systems requiring cooling air in an aircraft |
| 12/04/2013 | CN101554924B Device for feeding combustion air to an air craft engines |
| 12/03/2013 | US8596573 Nacelle flow assembly |
| 11/28/2013 | WO2013177263A1 Engine inlet |
| 11/28/2013 | US20130313371 Engine inlet |
| 11/28/2013 | US20130313337 Thrust Reverser System |
| 11/27/2013 | EP2665909A2 Nacelle for an aircraft bypass turbojet engine |
| 11/27/2013 | EP2665908A2 Nacelle for an aircraft bypass turbojet engine |
| 11/26/2013 | US8590832 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 |
| 11/20/2013 | EP2663777A1 Turbofan engine |
| 11/19/2013 | CA2671648C Auxiliary power unit inlet duct with acoustic silencing |
| 11/12/2013 | US8578697 Fan section |
| 11/12/2013 | CA2637901C Air inlet shroud structure |
| 11/07/2013 | WO2013166419A1 Mounting system for a nacelle fire detection system |
| 11/07/2013 | US20130291553 Integrated thermal protection and leakage reduction in a supersonic air intake system |
| 11/06/2013 | EP2660442A2 Integrated thermal protection and leakage reduction in a supersonic air intake system |
| 11/06/2013 | CN101646601B Lockable guiding system for a mobile part of a nacelle |
| 11/02/2013 | CA2814469A1 Air cooler system for gas turbine engines |
| 10/31/2013 | US20130284279 Air intake system for an air vehicle |
| 10/30/2013 | EP2655191A1 Inner structure for an aircraft nacelle |
| 10/23/2013 | CN203246593U High-flow and low-flow-velocity air conduit in very narrow area |
| 10/22/2013 | CA2542717C Aircraft engine exhaust nozzle |
| 10/22/2013 | CA2499675C Methods and apparatus for operating gas turbine engines |
| 10/18/2013 | CA2806099A1 Anti-vortex shedding generator for apu support |
| 10/16/2013 | EP2650211A2 Thermal insulation support |
| 10/16/2013 | EP2527253B1 De-icing device for an aviation gas turbine engine |
| 10/10/2013 | WO2013149936A1 Craft outer skin heat exchanger and method for manufacturing a craft outer skin heat exchanger |
| 10/09/2013 | EP2646321A1 An air intake system for an air vehicle |
| 10/09/2013 | CN101918276B Air intake for aircraft nacelle, and propulsion assembly including such air intake |
| 10/08/2013 | US8550208 High pressure muffling devices |
| 10/01/2013 | US8544793 Adjustable angle inlet for turbojet engines |
| 10/01/2013 | US8544598 Soundproofing panel for turbomachine and turbomachine comprising such a panel |
| 09/26/2013 | US20130248657 Deployable inlet scoop for an inboard ram air turbine |
| 09/25/2013 | EP2640640A2 Aircraft outer skin heat exchanger, aircraft cooling system and method for operating an aircraft outer skin heat exchanger |
| 09/25/2013 | EP2640639A1 Turbojet engine nacelle reinforcing structure |
| 09/25/2013 | CN103328800A Nacelle for an aircraft bypass turbojet engine |
| 09/25/2013 | CN103328330A Method for manufacturing an air-intake structure for a turbojet-engine nacelle |
| 09/24/2013 | US8540185 Modular air inlet lip with electric defrosting for a turbojet pod |
| 09/24/2013 | CA2692745C Compressor wash nozzle integrated in an inlet case strut |
| 09/24/2013 | CA2523195C Pressure lubrication for inverted flight |
| 09/18/2013 | CN103314206A Nacelle for an aircraft bypass turbojet engine |
| 09/17/2013 | CA2761761C Aircraft engine nacelle comprising a mobile cowl moved by electric motors |
| 09/11/2013 | CN103299084A Turbofan engine |
| 09/11/2013 | CN102057144B Method of depositing a coating for improving laminar flow |
| 09/11/2013 | CN102015450B Wave attenuation panel inserted between the motor and air inlet of an aircraft nacelle |
| 09/11/2013 | CN101952170B Air outlet system for aircraft leading edge |
| 09/10/2013 | US8529188 Fan nacelle flow control |
| 09/10/2013 | US8528317 Method and system for detecting the ingestion of an object by an aircraft turbine engine during a mission |
| 09/05/2013 | US20130228648 Auxiliary power unit inlet |
| 09/04/2013 | EP2632798A1 Turbojet engine nacelle with variable ventilation outlet cross section |
| 09/04/2013 | EP2632797A2 Leading edge structure, in particular for an air inlet of an aircraft engine nacelle |
| 09/04/2013 | CN103282278A Aircraft outer skin heat exchanger, aircraft cooling system and method for operating an aircraft outer skin heat exchanger |
| 09/03/2013 | US8522529 Propulsion unit for aircraft with heat exchanger having front inlet faces for cooling air flow and hot air flow |
| 09/03/2013 | CA2546714C A method of operating an aircraft system |
| 09/02/2013 | CA2805192A1 Liquid level monitoring and reporting system |
| 08/29/2013 | WO2013103416A3 Filter systems for air intakes of aircraft engines and related methods |
| 08/28/2013 | CN101939222B 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 |
| 08/28/2013 | CA2807676A1 Gas turbine exhaust having reduced jet noise |
| 08/24/2013 | CA2806068A1 Air-cooled oil cooler for turbofan engine |
| 08/21/2013 | CN103261026A Inner structure for an aircraft nacelle |
| 08/21/2013 | CN103253372A Flying saucer spacecraft |
| 08/15/2013 | US20130206920 Driven Aircraft, in Particular to an Aircraft Designed as a Flying Wing and/or Having a Low Radar Signature |
| 08/14/2013 | CN101200220B Systems and methods for passively directing aircraft engine nozzle flows |
| 08/13/2013 | US8505852 Reversible space plane |
| 08/13/2013 | US8505679 Panel for the acoustic treatment with a progressive thickness |
| 08/13/2013 | DE202013005040U1 Das Schutzstab-Gitter bietet einen Schutz, für Flugzeuge mit Strahltriebwerk und einem zusätzlichen Sicherheit für den Flugverkehr The protection bar grille provides protection for aircraft jet engine and an additional security for air travel |
| 08/13/2013 | CA2624005C Engine assembly for an aircraft comprising an engine as well as an engine mounting structure for such an engine |
| 08/08/2013 | CA2797073A1 Drainage circuit for a fluid coming from an engine group equipping a rotorcraft including a device for monitoring excessive fluid flow |
| 08/07/2013 | EP2454154B1 Leading edge structure, in particular for the air intake of the nacelle of an aircraft engine |
| 08/07/2013 | CA2804675A1 Interface and mounting process between an item of equipment and a rotary drive source for an engine group equiping a rotorcraft |
| 08/01/2013 | WO2013112331A1 Turbomachine fan clutch |
| 07/31/2013 | CN102066198B Aircraft engine nacelle air intake assembly |
| 07/31/2013 | CN101410300B Air inlet shroud structure |
| 07/30/2013 | US8496201 High capacity heat sink |
| 07/26/2013 | CA2803511A1 Drainage mast of the compartment of the auxiliary power unit of an aircraft |
| 07/25/2013 | WO2013108999A1 Blended wing body provided with canard |