| Patents for B64C 5 - Stabilising surfaces (949) |
|---|
| 04/09/2008 | EP0965048B1 On-the-fly accuracy enhancement for civil gps receivers |
| 04/03/2008 | WO2008037847A1 Curved element, wing, control surface and stabilizer for aircraft |
| 03/26/2008 | CN201040583Y Unmanned airplane empennage |
| 03/20/2008 | WO2008031620A2 Aerodynamic body and carrier wing comprising an aerodynamic body, actuating drive control module, computer, computer program, and method for influencing post-turbulences |
| 03/20/2008 | CA2663437A1 Aerodynamic element and wing with aerodynamic element, actuator-activation module, computer, computer program, and method for influencing wake eddies |
| 02/19/2008 | US7331548 Control linkage for T-tail aircraft elevator surfaces |
| 01/24/2008 | DE102006032003A1 Trimmbares Höhenleitwerk Trimmable horizontal stabilizer |
| 01/23/2008 | CN201010045Y Ground-effect aircraft |
| 01/17/2008 | WO2008006831A1 Trimmable horizontal stabilizer |
| 01/17/2008 | CA2656794A1 Trimmable horizontal stabilizer |
| 01/08/2008 | US7316371 Method and device for steepening a landing approach of an aircraft |
| 12/27/2007 | DE102006027599A1 Profile shaped aerodynamic effective component e.g. airplane wings, airplane control, rotor blade and rotor of wind energy plant, has double walled vane shell and composition is almost free from raw material |
| 12/18/2007 | US7308762 Method and apparatus for rotatably supporting movable components, including canards |
| 12/12/2007 | EP1863705A2 Aerofoil surface for controlling spin |
| 11/29/2007 | US20070272795 Wing-In-Ground-Effect Craft |
| 11/21/2007 | EP1857360A2 Sealing system for the gap existing between the fuselage and the elevator of the orientable horizontal stabiliser of an aircraft, extended with an aerodynamic fairing for sealing of the opening existing between the fuselage and the orientable horizontal stabiliser |
| 11/21/2007 | EP1857359A2 Sealing system for the gap existing between the fuselage and the elevator of an aircraft with orientable horizontal stabiliser |
| 11/21/2007 | CN200977409Y Plane tail wing |
| 11/15/2007 | US20070262207 Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance |
| 11/13/2007 | CA2339208C An aircraft fin and rudder |
| 11/06/2007 | US7290738 Dual jet emerging lift augmentation system for airfoils and hydrofoils |
| 10/31/2007 | CN200967563Y Passenger-cargo airplane movable wings |
| 10/09/2007 | US7278606 Helicopter having a fusilage section and a tail section coupled thereto |
| 09/27/2007 | WO2007107521A1 Bolted joint |
| 09/27/2007 | WO2007107520A2 Bolted joint |
| 09/27/2007 | DE10117721B4 Flügelspitzenverlängerung für einen Flügel Wing tip extension for a wing |
| 09/27/2007 | CA2640693A1 Bolted joint |
| 09/19/2007 | EP1834873A1 Elastic pre-deformed fairings for aircraft |
| 09/05/2007 | EP1829782A2 Lifting-type aeroplane fuselage |
| 09/04/2007 | US7264201 Process for reducing the aerodynamic loads applied to the elevators of an aircraft during takeoff |
| 07/17/2007 | US7243879 Lattice fin for missiles or other fluid-born bodies and method for producing same |
| 07/04/2007 | CN1990346A Rotation fitting for the empennage of an aircraft |
| 06/21/2007 | DE102005060958A1 Aircraft structure protection, against damage from birds in flight, is an outer skin of glass fiber reinforced aluminum with a hollow zone to allow skin distortion through an impact |
| 06/14/2007 | US20070136030 Method and device for detecting an overstepping of design loads of the fin of an aircraft |
| 06/14/2007 | US20070131821 Wing/winglet configuration and aircraft including it |
| 06/06/2007 | CN1974323A Ground effect flyer |
| 06/05/2007 | US7226015 Aircraft and missile forebody flow control device and method of controlling flow |
| 04/10/2007 | US7201347 Process for improving the landing of an aircraft |
| 04/04/2007 | CN1942363A Fairing for an aircraft structure |
| 03/29/2007 | WO2007034094A1 Turbojet for aircraft, aircraft equipped with such a turbojet, and method for mounting such a turbojet on an aircraft |
| 03/29/2007 | US20070069067 Aircraft spiraling mechanism with jet assistance - A |
| 03/29/2007 | CA2622151A1 Turbojet for aircraft, aircraft equipped with such a turbojet, and method for mounting such a turbojet on an aircraft |
| 03/27/2007 | US7195210 Fiber matrix for a geometric morphing wing |
| 03/15/2007 | US20070057115 Control system for craft and a method of controlling craft |
| 02/14/2007 | EP1751432A1 Method and apparatus employing eccentric bushing |
| 02/13/2007 | US7175132 Mechanism for eliminating limit cycle oscillations on servocontrolled aerodynamic control surfaces |
| 02/08/2007 | US20070029443 Cover for an aircraft structure |
| 01/25/2007 | US20070018049 Integrated wingtip extensions for jet transport aircraft and other types of aircraft |
| 01/23/2007 | US7165742 Aircraft spiralling mechanism - B |
| 01/03/2007 | CN1890124A Airflow control devices based on active materials |
| 12/27/2006 | EP1735211A1 Fairing for an aircraft structure |
| 12/12/2006 | US7147271 Airflow control devices with planar surfaces |
| 12/12/2006 | US7147269 Airflow control devices using current |
| 11/30/2006 | US20060267376 Airflow control devices based on active materials |
| 11/30/2006 | DE102005028688A1 Wing unit`s aerodynamic characteristics adapting device for e.g. aircraft, has winglet rotatable in relation to wing unit, such that angle between rotary axis and main direction of extension of unit differs from specified degree |
| 11/29/2006 | EP1587734B1 Aircraft with forward opening inlay spoilers for yaw control |
| 11/23/2006 | WO2006100526A3 Aerofoil surface for controlling spin |
| 11/22/2006 | EP1631493B1 Aircraft with topside only spoilers |
| 10/26/2006 | US20060237595 Wing for an aircraft or spacecraft |
| 10/26/2006 | US20060237580 Canard position and dihedral for boom reduction and pitch/directional control |
| 10/26/2006 | DE102005017825A1 Aircraft`s wake reducing system, has component provided fixed unit and two aerofoil units, which are periodically swivelable between end positions for interference of rolling procedure of air in area of outer aerofoil in flight direction |
| 10/24/2006 | US7125058 Locking device with solenoid release pin |
| 10/11/2006 | CN1845848A Flow-mechanically effective surface for minimising induced resistance |
| 10/03/2006 | US7114685 Wing for an aircraft or spacecraft |
| 09/28/2006 | WO2006100526A2 Aerofoil surface for controlling spin |
| 09/28/2006 | US20060214469 Airflow control devices based on active materials |
| 09/26/2006 | US7111810 Forward pivoted full flying control tail boom |
| 09/19/2006 | US7108230 Aircraft with topside only spoilers |
| 09/14/2006 | US20060202508 Airflow control devices based on active materials |
| 08/29/2006 | US7098619 Actuator and movement linkage system |
| 08/24/2006 | US20060186269 Adaptive compliant wing and rotor system |
| 08/23/2006 | EP1692038A2 Wing gull integration for nacelle clearance, compact landing gear stowage, and sonic boom reduction |
| 08/22/2006 | US7093791 Aircraft spiralling mechanism—c |
| 08/10/2006 | WO2006057575A3 Lifting-type aeroplane fuselage |
| 08/01/2006 | US7083141 Self-propelled projectile |
| 07/27/2006 | WO2006078651A1 Control surface assemblies with torque tube base |
| 07/25/2006 | CA2272435C No-back brake |
| 07/12/2006 | EP0965048A4 On-the-fly accuracy enhancement for civil gps receivers |
| 07/04/2006 | US7070146 Aircraft thickness/camber control device for low sonic boom |
| 07/04/2006 | US7070144 Aircraft and missile afterbody flow control device and method of controlling flow |
| 06/13/2006 | US7059664 Airflow control devices based on active materials |
| 06/13/2006 | US7059561 Deployment device for a fin |
| 06/01/2006 | CA2596429A1 Lifting-type aeroplane fuselage |
| 05/30/2006 | US7051976 Process for improving the maneuverability of an aircraft during a resource |
| 05/18/2006 | US20060102802 Aircraft with forward opening inlay spoilers for yaw control |
| 05/09/2006 | US7040210 Apparatus and method for restraining and releasing a control surface |
| 05/04/2006 | US20060091683 Locking device with solenoid release pin |
| 04/20/2006 | DE10318230B4 Verfahren und Vorrichtung zur Kompensation von Seitenwinden beim Landeanflug von Flugzeugen Method and apparatus for compensation of crosswinds on the approach of aircraft |
| 04/19/2006 | EP0993588B1 Gps guided munition |
| 03/29/2006 | EP1640265A1 Horizontal stabilizer trim device |
| 03/23/2006 | US20060060699 Process for improving the maneuverability of an aircraft during a resource |
| 03/23/2006 | US20060060696 Link between the wing and canard for flutter reduction |
| 03/09/2006 | US20060049307 Flow-mechanically effective surface for minimizing induced resistance |
| 03/08/2006 | EP1631493A2 Aircraft with topside only spoilers |
| 02/28/2006 | US7004425 Flying body for firing from a tube with over-caliber stabilizers |
| 02/23/2006 | WO2006019332A1 Aircraft lifting surface (variants) |
| 02/14/2006 | US6997413 Flying amphibious SUV |
| 02/09/2006 | DE102004034367A1 Deflection device e.g. for aerodynamic body, has edge which exhibits surface and surface is set for local direction of flow and deflector attachable at end of body with deflector shaped as missile |
| 01/31/2006 | US6991280 Airflow control devices based on active materials |
| 01/26/2006 | US20060016927 Method and apparatus for rotatably supporting movable components, including canards |