| Patents for B64D 33 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for (2,926) |
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| 07/24/2013 | CN102216159B Air intake arrangement for an aircraft |
| 07/17/2013 | EP2615400A2 Multi-channel cooling bond pad and corresponding cooling method |
| 07/17/2013 | CN103209893A Turbojet engine nacelle reinforcing structure |
| 07/17/2013 | CN103209892A Aircraft with an integral aerodynamic configuration |
| 07/17/2013 | CN101952573B Air intake structure for an aircraft nacelle |
| 07/17/2013 | CA2802060A1 Gas turbine engine with pylon mounted accessory drive |
| 07/16/2013 | US8485467 Air intake, in particular for an aircraft chaff dispenser |
| 07/11/2013 | WO2013102739A1 Seal for a turbojet engine pylon and nacelle, and turbojet engine pylon-nacelle assembly incorporating such a seal |
| 07/10/2013 | CA2801518A1 Air recovery system for precooler heat-exchanger |
| 07/08/2013 | DE202013001098U1 Staustrahltriebwerk mit veränderbarer Einlaufgeometrie Ramjet engine with variable intake geometry |
| 07/04/2013 | US20130169036 Aircraft power distribution network |
| 07/04/2013 | US20130168180 Gas turbine inlet system |
| 07/03/2013 | EP2610462A2 Gas turbine engine with low stage count low pressure turbine |
| 07/03/2013 | EP2610179A2 Aircraft air inlet diverter assemblies with improved aerodynamic characteristics |
| 07/02/2013 | CA2766010C Passive cooling system for auxiliary power unit installation |
| 06/29/2013 | CA2800049A1 Seal for a variable area fan nozzle |
| 06/27/2013 | WO2013093256A1 Acutator for aircraft turbine engine nacelle with notably one-piece annular rear part |
| 06/27/2013 | WO2013092279A1 Sound insulation device and engine provided therewith and provision method |
| 06/27/2013 | DE102011056826A1 Schallschutzvorrichtung und damit versehenes Triebwerk und Verfahren zur Bereitstellung The sound insulation device and thus provided the engine and method for providing |
| 06/27/2013 | CA2856210A1 Acutator for aircraft turbine engine nacelle with notably one-piece annular rear part |
| 06/26/2013 | EP2607656A2 Gas turbine engine particle separator |
| 06/26/2013 | CN103180209A Turbojet engine nacelle with variable ventilation outlet cross section |
| 06/23/2013 | CA2798754A1 Airfoils including compliant tip |
| 06/21/2013 | CA2798787A1 Variable area fan nozzle with drive system health monitoring |
| 06/20/2013 | WO2013088088A1 Fluid discharge vibration damping strips for acoustic protection of aircraft turbomachine fan casing |
| 06/20/2013 | WO2013088033A1 Air intake structure for turbojet engine nacelle |
| 06/20/2013 | CA2858503A1 Air intake structure for turbojet engine nacelle |
| 06/20/2013 | CA2858165A1 Fluid discharge vibration damping strips for acoustic protection of aircraft turbomachine fan casing |
| 06/20/2013 | CA2799100A1 Energy management on board an aircraft |
| 06/19/2013 | CN101778761B Nacelle equipped with at least one excess pressure flap |
| 06/18/2013 | CA2665303C Starting and generating apparatus for engine |
| 06/13/2013 | WO2013084308A1 Installation boss and fan case |
| 06/13/2013 | CA2857938A1 Attachment boss and fan case |
| 06/12/2013 | CN102358428B Air inlet bulge construction for auxiliary power device of airplane |
| 06/12/2013 | CN101903245B Aircraft with aircraft cooling system |
| 06/12/2013 | CN101405184B Structure for an air inlet lip of an electric de-icing pod comprising an acoustic attenuation zone |
| 06/08/2013 | CA2797327A1 Ballistic materials for enhanced energy absorption and fan casings including the same |
| 06/06/2013 | WO2013079100A1 System and method for cooling an aircraft wing |
| 06/06/2013 | US20130140405 Integral Powered Wing Aircraft Utilizing Full Rotary Disc Stacking With Aeronautical Enhancements |
| 06/06/2013 | CA2854050A1 System and method for cooling an aircraft wing |
| 06/05/2013 | EP2599719A1 Aircraft with an integral aerodynamic configuration |
| 06/05/2013 | EP2599078A2 Acoustic panel for a turbojet engine nacelle, with in-built fasteners |
| 05/30/2013 | US20130134776 Energy supply system, aircraft or spacecraft and method |
| 05/30/2013 | US20130134265 Aircraft |
| 05/29/2013 | EP2597038A2 An Aircraft |
| 05/29/2013 | EP2597037A2 An Aircraft |
| 05/29/2013 | CN101626953B Aircraft leading edge |
| 05/28/2013 | US8452516 Variable vane scheduling based on flight conditions for inclement weather |
| 05/28/2013 | CA2554264C Reversible driving apparatus for pcu pumps |
| 05/23/2013 | US20130126265 Engine inlet varying impedance acoustic liner section |
| 05/21/2013 | US8444083 Auxiliary power unit inlet |
| 05/16/2013 | WO2013068671A1 Composite panel having a built-in sampling scoop |
| 05/16/2013 | CA2853394A1 Composite panel having a built-in sampling scoop |
| 05/15/2013 | CN103101617A Method for improving aero-engine air injection reverse thrust efficiency |
| 05/14/2013 | US8439308 Spring loaded pressure relief door |
| 05/14/2013 | US8439298 Device for shrouding an aircraft nacelle |
| 05/14/2013 | US8439297 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 |
| 05/14/2013 | US8439296 Aircraft huffer coupling adapter and methods of use |
| 05/14/2013 | US8439295 Aircraft engine inlet pivotable barrier filter |
| 05/14/2013 | US8439061 Emergency ram air inlet valve of an aircraft |
| 05/08/2013 | EP2589537A1 Heat transfer devices |
| 05/08/2013 | CN202923889U Comprehensive heat energy management electric environment control system |
| 05/08/2013 | CN202923885U Device of strengthening air jet reverse thrust of aeroengine |
| 05/01/2013 | CN103072698A Method for improving reaction thrust efficiency of aero-engine by directional expansion and pressurization |
| 04/30/2013 | US8430202 Compact high-pressure exhaust muffling devices |
| 04/30/2013 | US8429890 Bird and debris deflector for aircraft jet engines |
| 04/25/2013 | US20130099560 Multiple source electrical power distribution in aircraft |
| 04/24/2013 | EP2582959A1 Aircraft turbo jet engine fan casing |
| 04/24/2013 | EP2582581A2 Driven aircraft, in particular an aircraft designed as a flying wing and/or having a low radar signature |
| 04/24/2013 | CN101909998B Aircraft nacelle guidance system installation |
| 04/24/2013 | CA2792589A1 Thermal electrical power generation for aircraft |
| 04/18/2013 | US20130092798 Filter Systems For Air Intakes Of Aircraft Engines and Related Methods |
| 04/17/2013 | EP2580121A1 Turbojet engine nacelle |
| 04/16/2013 | US8419815 Bird deflector and air replacement system |
| 04/16/2013 | US8418953 Gas turbine engine nacelle |
| 04/11/2013 | US20130087663 Self-aligning inlet plenum system for rotorcraft |
| 04/11/2013 | US20130087661 Propulsive unit for an aircraft |
| 04/10/2013 | EP2578842A2 Aircraft nacelle comprising a device for supplying hot air to a panel combining acoustic and ice treatments |
| 04/10/2013 | EP2578496A2 Acoustic treatment panel including hot-air channels and at least one annular channel |
| 04/10/2013 | EP2578495A2 Acoustic treatment panel including hot-air channels and at least one stabilising chamber |
| 04/10/2013 | EP2578490A2 A propulsion unit for an aircraft |
| 04/10/2013 | CN103038484A Multi-layer acoustic treatment panel |
| 04/10/2013 | CN103038132A Driven aircraft, in particular an aircraft designed as a flying wing and/or having a low radar signature |
| 04/10/2013 | CN103029844A Air intake with double inlet door |
| 04/10/2013 | CN103029843A Aircraft nacelle comprising a hot air supply device for a panel combining acoustic and frost treatments |
| 04/10/2013 | CN103029842A Acoustic treatment panel including hot-air channels and at least one annular channel |
| 04/10/2013 | CN103029841A Acoustic treatment panel including hot-air channels and at least one stabilising chamber |
| 04/10/2013 | CN103029840A Aircraft engine system and design method for fan section mechanical interface thereof |
| 04/10/2013 | CN103029826A Aircraft heat protection and electric energy extraction integrated structure |
| 04/09/2013 | US8413924 Motor assisted fine pitch startup Ram Air Turbine |
| 04/09/2013 | US8413922 Acoustic processing structure particularly adapted to the air inlet of an aircraft nacelle |
| 04/04/2013 | WO2013045783A1 Lip unit for an electrically deiced turbojet engine nacelle |
| 04/04/2013 | CA2847806A1 Lip unit for an electrically deiced turbojet engine nacelle |
| 04/03/2013 | CN103010468A Bleed air duct joint insulation means |
| 04/02/2013 | US8408491 Nacelle assembly having inlet airfoil for a gas turbine engine |
| 04/02/2013 | US8408281 System, method, and apparatus for pulsed-jet-enhanced heat exchanger |
| 03/28/2013 | US20130076120 Aircraft emergency power system |
| 03/28/2013 | US20130075539 Composite aerospace structure with integrated conveyance element |
| 03/28/2013 | DE102011086786B3 Cooling housing useful for accommodating electronic components, comprises heat pipes for cooling the electronic components, and are integrated with the cooling housing, and contain a liquid fluid that evaporates under heat absorption |
| 03/27/2013 | EP2572987A2 A fluid management apparatus and method |