| Patents for B64C 5 - Stabilising surfaces (949) |
|---|
| 09/26/2012 | EP2502826A1 A flying saucer |
| 09/20/2012 | US20120234968 Aircraft with freewheeling engine |
| 09/19/2012 | EP2499042A2 Aircraft |
| 09/12/2012 | CN202429346U Empennage of small unmanned aerial vehicle |
| 09/04/2012 | US8256710 Live trim tabs |
| 08/29/2012 | EP2490934A2 Aircraft horizontal stabiliser fitted with leading-edge strake |
| 08/21/2012 | CA2713162C Winglets with recessed surfaces, and associated systems and methods |
| 08/16/2012 | WO2012109355A2 Vortex-induced vibration suppression device and mating collar system |
| 08/16/2012 | US20120205490 Aircraft horizontal stabiliser fitted with leading-edge strake |
| 08/15/2012 | CN202379089U Novel unmanned aerial vehicle |
| 08/08/2012 | CN102627144A Shape memory alloy actuated torsion lock |
| 08/07/2012 | CA2509427C Process or device for detecting design load exceedances of aircraft drift |
| 08/02/2012 | WO2012101645A1 Dynamic limitation of monoblock flight control surfaces inclinations during stall susceptibility conditions |
| 08/02/2012 | US20120193473 Torsion box skin stiffened with non parallel stringers |
| 07/25/2012 | EP2477890A1 Removable horizontal stabilizer for helicopter |
| 07/11/2012 | CN202320774U 未来救援隐身航母所载短体飞机 Short-body aircraft coming out of stealth aircraft rescue |
| 07/11/2012 | CN102574570A Removable horizontal stabilizer for helicopter |
| 07/05/2012 | US20120168559 Removable Horizontal Stabilizer for Helicopter |
| 07/04/2012 | EP2470426A2 Aircraft having at least two electrical propulsion groups mounted at a rear portion thereof |
| 07/03/2012 | US8210467 Method and apparatus for hurricane surveillance from the eye |
| 06/21/2012 | WO2011144210A9 Device for sandblasting uses exhaust gas from a jet engine for blasting |
| 06/21/2012 | US20120153083 Optimization of structures subjected to hot gas streams |
| 06/20/2012 | EP2465769A2 Optimization of structures subjected to hot gas streams |
| 06/20/2012 | CN102501973A Small-sized multipurpose unmanned machine |
| 06/12/2012 | US8196860 Aircraft having reduced environmental impact |
| 06/07/2012 | US20120138739 Aircraft provided with a tail plane including means for combating flutter |
| 06/07/2012 | US20120138738 System for increasing controllability for an aircraft |
| 06/07/2012 | US20120138736 Airplane with a tailcoat tail assembly and rear engine |
| 06/05/2012 | US8191833 Aircraft and missile afterbody flow control device and method of controlling flow |
| 06/05/2012 | US8191826 Device which is subject to fluid flow |
| 06/05/2012 | US8191820 Flying wing aircraft |
| 05/24/2012 | US20120126060 Method of fabricating an aircraft part by infusing resin |
| 05/24/2012 | DE102010044048A1 Verbindungsanordnung, Luft- oder Raumfahrzeug, Verfahren zum Abwerfen von Last sowie Verfahren zum Landen Connection arrangement, aircraft or spacecraft, procedures for dropping load and methods for landing |
| 05/23/2012 | CN101559832B Fast hybrid helicopter with large range |
| 05/22/2012 | US8181908 Control surface failsafe drop link |
| 05/16/2012 | CN102452476A Cantilevered differential motion sensor and associated frame |
| 05/09/2012 | CN102442428A Active flow control on vertical stabilizer and rudder |
| 05/09/2012 | CN102442422A Winglet for increasing pneumatic efficiency of horizontal tail of time-domain airplane |
| 05/03/2012 | WO2011144210A3 Device for sandblasting uses exhaust gas from a jet engine for blasting |
| 04/25/2012 | CN102428000A 提高航空器垂直尾翼的空气动力学效率的方法 Improve the aerodynamic efficiency of aircraft vertical tail method |
| 04/25/2012 | CN102424107A Manufacture method of solar airplane |
| 04/19/2012 | US20120091266 Active Flow Control on a Vertical Stabilizer and Rudder |
| 04/19/2012 | DE102008012275B4 Hubschrauber-Rettungssystem für Heckrotorausfall Helicopter rescue system for tail rotor failure |
| 04/18/2012 | EP2441669A2 Active flow control on a vertical stabilizer and rudder |
| 04/18/2012 | CN102421666A System for increasing controllability for an aircraft |
| 04/18/2012 | CN102417035A 全按钮控制变换飞速的共轴直升机 Full-button control coaxial helicopter rapid transformation |
| 04/15/2012 | CA2748875A1 Forward swept winglet |
| 04/12/2012 | WO2012045783A1 Device and method for increasing the aerodynamic lift of an aircraft |
| 04/12/2012 | DE102010048266A1 Flügel mit einem Strömungszaun und Flugzeug mit solchen Tragflügeln Wing with a flow fence and aircraft wings with such |
| 04/10/2012 | US8152109 Method and system for controlling fluid flow in relation to a foil and harnessing energy therefrom |
| 03/28/2012 | EP2432684A1 Method for enhancing the aerodynamic efficiency of the vertical tail of an aircraft |
| 03/08/2012 | US20120056038 Mechanism for Changing the Shape of a Control Surface |
| 03/01/2012 | WO2012026846A1 Aircraft with an integral aerodynamic configuration |
| 03/01/2012 | US20120048995 Method For Enhancing The Aerodynamic Efficiency Of The Vertical Tail Of An Aircraft |
| 02/23/2012 | WO2011089458A4 Airplane with aerodynamic stall-prevention layout and pertinent longitudinal stability arrangement |
| 02/21/2012 | US8118254 Flap actuator |
| 02/09/2012 | WO2012017152A1 Method and device for the lateral stabilization of an aircraft |
| 02/09/2012 | WO2012016717A1 Auxiliary flap arrangement and aerodynamic body exhibiting such an auxiliary flap |
| 02/09/2012 | US20120032033 Wing piercing airplane |
| 02/07/2012 | CA2491357C Method for improving the landing of an aircraft |
| 02/02/2012 | US20120025013 Aerospace vehicle yaw generating tail section |
| 02/01/2012 | EP2412628A2 Aerospace vehicle yaw generating tail section |
| 01/18/2012 | EP2407376A1 System for increasing controllability for an aircraft |
| 01/10/2012 | CA2427357C Aircraft with wing active wash control |
| 12/29/2011 | US20110315809 Three wing, six-tilt propulsion unit, vtol aircraft |
| 12/27/2011 | US8083179 Composite material for geometric morphing wing |
| 12/27/2011 | US8083178 Method and device for piloting an aircraft optimizing the control of the ailerons in an enhanced-lift configuration |
| 12/20/2011 | US8079810 Turbine airfoil cooling system with divergent film cooling hole |
| 12/15/2011 | US20110303796 Morphing control surface transition |
| 12/14/2011 | CN102282070A 飞机水平稳定面 Aircraft horizontal stabilizer surface |
| 12/13/2011 | US8074925 Aircraft attitude control configuration |
| 12/01/2011 | WO2011089458A3 Airplane with aerodynamic stall-prevention layout and pertinent longitudinal stability arrangement |
| 11/24/2011 | WO2011144210A2 Heating and cleaning apparatus for surface treatment |
| 11/23/2011 | CN102256871A Mobile surfaces for aircraft with sealed slots |
| 11/22/2011 | CA2489794C Process for reducing aerodynamic loads applied to aircraft elevators during take-off |
| 11/10/2011 | US20110272521 Flight unit control system, flight control device including such a system, and use of such a system |
| 11/09/2011 | CN102239083A Aircraft directional control and stabilizing surface |
| 11/03/2011 | DE102010028311A1 System und Verfahren zur Minimierung von Buffeting System and method for minimizing buffeting |
| 11/02/2011 | CN102229357A Empennage with installing angle and adjustable horizontal tail |
| 11/01/2011 | CA2489799C Process for improving the manoeuvrability of an aircraft during pull-out |
| 10/20/2011 | WO2011068659A3 Active winglet |
| 10/13/2011 | US20110248123 Unmanned aerial vehicle having an improved aerodynamic configuration |
| 10/13/2011 | DE102010014633A1 Wing assembly for airplane e.g. cargo aircraft, has wing adaptor section whose V-angle increases in specific degree from outer rib of wing base section to outer rib of wing adaptor section, where angle is produced along local span direction |
| 10/05/2011 | EP2371707A2 Aircraft directional control and stabilizing surface |
| 10/05/2011 | EP2371705A2 Horizontal stabilising surface of an aircraft |
| 09/28/2011 | EP2368793A2 Manned aircraft |
| 09/28/2011 | CN102202965A Fitting for trimming the horizontal stabiliser of an aircraft |
| 09/22/2011 | US20110226899 Autonomous plane architecture for the transport and the replacement of propulsion engines |
| 09/15/2011 | US20110220758 Architecture d'avion a fuselage large |
| 09/07/2011 | EP2038171B1 Aircraft comprising a trimmable horizontal stabilizer |
| 08/24/2011 | EP2360092A2 Fitting for trimming the horizontal stabiliser of an aircraft. |
| 08/18/2011 | WO2011048064A3 Aircraft horizontal stabiliser fitted with leading-edge strake |
| 08/10/2011 | EP2353997A2 Joining arrangement for the lateral boxes of a horizontal tail stabiliser with a tubular central box and manufacturing method for said box |
| 08/03/2011 | CN201914457U Horizontal tail I-shaped tube beam of helicopter |
| 08/02/2011 | US7988099 Winglet |
| 07/28/2011 | US20110180672 Airplane with aerodynamic stall-prevention layout and pertinent longitudinal stability arrangement |
| 07/28/2011 | DE102010005887A1 Winglet for wing of aircraft, is hinged around folding axis and is fixed by folding device, where folding device releases winglet for turning down around folding axis by exceeding certain side load acting on winglet |
| 07/27/2011 | EP2346734A1 Active winglet |
| 07/27/2011 | CN102137768A Combined air, water and road vehicle |
| 07/27/2011 | CN102133925A Airplane without vertical tail |