| Patents for B64C 9 - Adjustable control surfaces or members, e.g. rudders (2,586) |
|---|
| 10/06/2005 | US20050218262 Process for improving the landing of an aircraft |
| 09/22/2005 | DE102005009349A1 Flugzeugflügel mit elektrothermischer Enteisungs- und/oder Anti-Vereisungsvorrichtung Airplane wing with electrothermal deicing and / or anti-icing device |
| 09/15/2005 | WO2005084156A2 Hydrogen powered aircraft |
| 09/14/2005 | CN1218859C Manipulator of power-boosting ground effect aircraft for ground effect transition region |
| 09/08/2005 | DE102004006940A1 Landing flap guide for an aircraft has slide that is connected to the landing flap and extends and retract the landing flap guided along the flap carrier through glide guides |
| 09/06/2005 | US6938856 Empennage assembly and attachment mechanism for a model airplane |
| 08/31/2005 | EP1568605A1 Method and device for the optimization of the deployment of the spoiler of an aircraft during flight |
| 08/30/2005 | US6935592 Aircraft lift device for low sonic boom |
| 08/25/2005 | WO2005077756A1 Landing flap guide for aircraft |
| 08/18/2005 | US20050178925 Deployment system for a moveable wing surface |
| 08/18/2005 | US20050178899 Process for reducing the aerodynamic loads applied to the elevators of an aircraft during takeoff |
| 08/18/2005 | US20050178898 Method and apparatus for controlling an airplane |
| 08/18/2005 | US20050178897 Mechanism for eliminating limit cycle oscillations on servocontrolled aerodynamic control surfaces |
| 08/16/2005 | US6929216 Method and apparatus for installing and actuating movable airfoils, including canards |
| 08/16/2005 | US6928895 Ballscrew locking nut |
| 08/16/2005 | US6928715 Method for producing lattice fin for missiles or other fluid-born bodies |
| 08/11/2005 | US20050175406 Joint for connecting a longitudinal side to an upper side of components and flexible strip for use in such a joint |
| 08/11/2005 | US20050175399 Joint for connecting components together on opposite longitudinal sides in addition to a flexible strip used for said joint |
| 08/11/2005 | US20050173593 Forward pivoted full flying control tail boom |
| 08/10/2005 | EP1562091A1 Method for improving the landing of an aircraft |
| 08/09/2005 | US6926233 Automatic formation flight control system (AFFCS)—a system for automatic formation flight control of vehicles not limited to aircraft, helicopters, or space platforms |
| 08/04/2005 | WO2005070762A1 Mobile leading edge flap for a main wing of the aerofoils of an aircraft and main wing provided with such a flap |
| 08/04/2005 | US20050171652 Vehicle control systems and corresponding sizing methods |
| 08/03/2005 | CN1649894A A method for identification, isolation and production of antigens to a specific pathogen |
| 08/02/2005 | US6923404 Apparatus and methods for variable sweep body conformal wing with application to projectiles, missiles, and unmanned air vehicles |
| 07/26/2005 | US6921045 Supersonic aircraft with channel relief control |
| 07/14/2005 | WO2005062743A2 Supersonic aircraft with aerodynamic tail structure |
| 07/14/2005 | WO2005023643A3 Aircraft with topside only spoilers |
| 07/14/2005 | US20050151031 Aircraft wing structure and a method for decreasing flight speed of the aircraft |
| 07/14/2005 | US20050151030 Lifting surface provided with at least one rotary flap |
| 07/14/2005 | US20050151029 Lift and twist control using trailing edge control surfaces on supersonic laminar flow wings |
| 07/06/2005 | EP1550607A1 Mechanism for eliminating limit cycle oscillations on servocontrolled aerodynamic control surfaces |
| 07/05/2005 | CA2204445C System for controlling aircraft control surface trim tabs |
| 07/05/2005 | CA2148393C Cargo plane with front empennage |
| 06/30/2005 | US20050139726 Head wind against the transports converting into lift & air driven down force to save fuels & ecology |
| 06/22/2005 | EP1544101A1 Method for ameliorating the maneuverability of an aircraft during pitch up |
| 06/22/2005 | EP1544100A1 Method for reducing the aerodynamic forces on an elevator of an aircraft during takeoff |
| 06/15/2005 | EP1540264A1 Braking device for a trajectory-correctable spin-stabilized artillery projectile |
| 06/15/2005 | CN2704539Y Wind pressure steering rudders |
| 06/14/2005 | CA2146812C Protective device for a control surface hinge, as for an aircraft |
| 06/09/2005 | US20050123400 Rotor blade pitch control assembly |
| 06/09/2005 | US20050120538 Lattice fin for missiles or other fluid-born bodies and method for producing same |
| 06/08/2005 | EP1538075A1 An aircraft wing structure and a method for decreasing flight speed of the aircraft |
| 06/08/2005 | CN1623853A Method for controlling tail rudder of model aircraft |
| 06/02/2005 | WO2005049424A2 Aircraft lift device for low sonic boom |
| 06/02/2005 | US20050116116 Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance |
| 06/02/2005 | US20050116115 Actuation apparatus for a control flap arranged on a trailing edge of an aircraft airfoil |
| 06/02/2005 | US20050116094 Method making it possible to prevent vibration of a rudder of an aircraft and aircraft using this method |
| 06/02/2005 | US20050116085 Aircraft spiralling mechanism - c |
| 06/01/2005 | EP1535836A1 Method for avoiding aircraft rudder vibration and aircraft using said method |
| 05/19/2005 | WO2005044660A2 Wing gull integration for nacelle clearance, compact landing gear stowage, and sonic boom reduction |
| 05/19/2005 | US20050106987 Empennage assembly and attachment mechanism for a model airplane |
| 05/19/2005 | US20050103945 Adjustment mechanism for a variable-shape wing |
| 05/19/2005 | US20050103929 Supersonic aircraft with channel relief control |
| 05/17/2005 | US6892982 Aircraft with forward opening inlay spoilers for yaw control |
| 05/10/2005 | US6890470 Method for producing a fiber composite structural component |
| 05/06/2005 | WO2005044661A2 Supersonic aircraft with aerodynamic control |
| 04/27/2005 | EP1438230B1 Carrying or guiding device for aircraft components |
| 04/26/2005 | US6883806 Notched blade seal for high performance aircraft |
| 04/21/2005 | US20050082434 Carrying or guiding device for aircraft components |
| 04/21/2005 | US20050082425 Empennage assembly and attachment mechanism for a model airplane |
| 04/20/2005 | EP1071607A4 Single surface multi axis aircraft control |
| 04/14/2005 | US20050077435 Profiled wing unit of an aircraft |
| 04/13/2005 | EP1522492A1 Wing unit airfoil structure |
| 04/13/2005 | EP1521951A2 Apparatus for monitoring an aircraft flap and application of a dynamometric rod |
| 03/31/2005 | US20050067526 Wing gull integration nacelle clearance, compact landing gear stowage, and sonic boom reduction |
| 03/31/2005 | US20050067525 Aircraft thickness/camber control device for low sonic boom |
| 03/31/2005 | DE10339030A1 Tragstruktur für eine ein- und ausfahrbare Klappe und deren Verwendung Support structure for an extendable and retractable flap and its use |
| 03/24/2005 | US20050061922 Method and spoiler system for ensuring the aerodynamic continuity of the upper surface of an aircraft |
| 03/23/2005 | EP1516813A1 Spoiler and its deployment method for improving the aerodynamic quality of a wing surface |
| 03/23/2005 | CN1597447A Improved design for raising fighter plane maneuverability in air and strengthening fighting abibity in airbattle |
| 03/22/2005 | US6869050 Profiled wing unit of an aircraft |
| 03/17/2005 | WO2005023643A2 Aircraft with topside only spoilers |
| 03/17/2005 | WO2005005251B1 Wing of aircraft |
| 03/17/2005 | CA2528405A1 Aircraft with topside only spoilers |
| 03/10/2005 | WO2005021375A1 Support structure for a retractable and extendable flap, and use of said structure |
| 03/10/2005 | WO2004092013A3 Winged spacecraft |
| 03/08/2005 | US6863242 Method and system for controlling an aircraft control surface |
| 03/03/2005 | US20050045764 Canard position and dihedral for boom reduction and pitch/directional control |
| 03/03/2005 | US20050045763 Aircraft lift device for low sonic boom |
| 02/24/2005 | US20050040294 Lift-flap mechanism |
| 02/17/2005 | US20050037444 Method for identification isolation and production of antigens to a specific pathogen |
| 02/10/2005 | US20050029407 Aircraft flap or slat drive system with redundant drives and shaft drive lines |
| 02/10/2005 | DE10328540A1 Operating device for elevator flap installed on trailing edge of wing of aircraft has several extendable box-form telescopic supports with support elements connected by respective ends to support structure of wing and elevator flap |
| 02/08/2005 | US6851646 Method and apparatus for actuating movable components, including canards, over multiple ranges |
| 01/27/2005 | US20050017126 Slotted aircraft wing |
| 01/20/2005 | WO2005005251A1 Wing of aircraft |
| 01/20/2005 | US20050011994 Multi-function trailing edge devices and associated methods |
| 01/20/2005 | CA2555880A1 Wing of an aircraft |
| 01/18/2005 | US6843452 Variable trailing edge geometry and spanload control |
| 01/18/2005 | US6843450 Method and apparatus for rotatably supporting movable components, including canards |
| 01/13/2005 | WO2005002962A1 Slotted aircraft wing |
| 01/06/2005 | WO2005000672A1 Rigid wing with variable sustentation due to deployment of a flexible wing |
| 01/06/2005 | US20050001104 Rotary flap |
| 01/06/2005 | US20050001103 Variable trailing edge geometry and spanload control |
| 01/06/2005 | CA2534404A1 Rigid wing with variable sustentation due to deployment of a flexible wing |
| 12/29/2004 | EP1491442A1 Aircraft flap actuation mechanism |
| 12/22/2004 | EP1488998A1 Wing trailing edge geometry control mechanism |
| 12/16/2004 | WO2004108526A1 Aircraft with forward opening inlay spoilers for yaw control |
| 12/16/2004 | US20040251383 Use of aerodynamic forces to assist in the control and positioning of aircraft control surfaces and variable geometry systems |