| Patents for B64C 13 - Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers (4,795) |
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| 02/08/2006 | CN1732108A Augmenting flight control surface actuation system and method |
| 02/02/2006 | WO2006010842A1 Device for antagonistic artificial force gradient for an aircraft control surface remote control device |
| 02/02/2006 | WO2006010841A1 Device for remote control of an aircraft control surfaces |
| 02/02/2006 | US20060022086 Forward pivoted full flying control tail boom |
| 02/01/2006 | EP1185912B1 Device for controlling an apparatus |
| 01/26/2006 | US20060016927 Method and apparatus for rotatably supporting movable components, including canards |
| 01/26/2006 | DE102004029194A1 Stabilization system for aircraft subjected to gust loading has yaw sensor in cockpit connected to regulator and frequency measurement circuits with connections to ailerons and spoilers on wing |
| 01/25/2006 | EP1619414A2 Actuator |
| 01/25/2006 | EP1619413A2 Actuator |
| 01/19/2006 | WO2006006950A1 Redundant flow control for hydraulic actuator systems |
| 01/17/2006 | US6986486 Aircraft control system |
| 01/17/2006 | US6986483 Inertial reference system for an aircraft |
| 01/17/2006 | US6986249 Apparatus for coupling force-activated actuators |
| 01/12/2006 | WO2006004570A2 Forward pivoted full flying control tail boom |
| 01/12/2006 | DE102004029196A1 Load-reduction system for reducing load acting on fuselage of e.g. aircraft, includes at least one control unit which modifies amplitude characteristics and/or phase characteristics of loads acting on fuselage of aircraft |
| 01/11/2006 | EP1614626A1 Aerodynamic control device with displaced motor for a missile |
| 01/05/2006 | DE102004055740A1 Flugzeughochauftriebssystem mit Überlastsicherung Aircraft high lift system with overload protection |
| 01/03/2006 | US6981439 Redundant flow control for hydraulic actuator systems |
| 12/29/2005 | WO2005124192A2 Compact actuator |
| 12/29/2005 | WO2005044661A3 Supersonic aircraft with aerodynamic control |
| 12/29/2005 | WO2005024184A3 Variable cam exhaust nozzle |
| 12/28/2005 | EP1218240B1 Variable gradient control stick force feel adjustment system |
| 12/21/2005 | EP1607326A1 System and method for reducing the loads acting on the fuselage structure in means of transport |
| 12/21/2005 | EP1607325A1 Device and Method for attenuating at least one rigid body mode and/or at least one elastic mode of an aircraft |
| 12/16/2005 | CA2510117A1 System and method for reducing the loads acting on the fuselage structure in means of transport |
| 12/15/2005 | US20050278087 Remote image management system (RIMS) |
| 12/15/2005 | US20050277513 Compact actuator |
| 12/15/2005 | US20050276701 Hydraulic motors |
| 12/14/2005 | EP1604896A2 Airplane high lift system with overload prevention |
| 12/14/2005 | EP1509705B1 Actuator with two motors, a differential reducer and a torque limiter |
| 12/08/2005 | US20050269887 High-reliability electro-mechanical actuator |
| 12/07/2005 | EP1488111B1 Linear, hydraulic pivot drive |
| 12/01/2005 | WO2005106285A3 Methods and apparatus for minimizing backlash in a planetary gear mechanism |
| 12/01/2005 | WO2005044660A3 Wing gull integration for nacelle clearance, compact landing gear stowage, and sonic boom reduction |
| 12/01/2005 | US20050263644 Control system for airbrakes of an aircraft |
| 11/30/2005 | EP1600372A2 Hydraulic motors |
| 11/30/2005 | EP1600371A1 Control system for aircraft airbrakes |
| 11/28/2005 | CA2508805A1 Control system for airbrakes of an aircraft |
| 11/22/2005 | US6966614 Architecture for a hydraulic circuit |
| 11/17/2005 | US20050252318 Apparatus for releasing a jam in a lead screw actuator |
| 11/16/2005 | EP1141554B1 Electrostatic/pneumatic actuators for active surfaces |
| 11/15/2005 | US6965816 PFN/TRAC system FAA upgrades for accountable remote and robotics control to stop the unauthorized use of aircraft and to improve equipment management and public safety in transportation |
| 11/15/2005 | US6964521 Compliant linear bearing |
| 11/10/2005 | WO2005106285A2 Methods and apparatus for minimizing backlash in a planetary gear mechanism |
| 11/10/2005 | US20050250614 Methods and apparatus for minimizing backlash in a planetary gear mechanism |
| 11/09/2005 | EP1592781A2 Improved vertical take-off and landing vehicles |
| 11/03/2005 | WO2005103939A1 Control system for vehicles |
| 11/03/2005 | US20050242243 Process and device for the optimization of the deflection of the spoiler flaps of an aircraft in flight |
| 11/03/2005 | US20050242240 Aircraft with a detachable passenger escape cabin |
| 11/03/2005 | US20050242234 Lifters, methods of flight control and maneuver load alleviation |
| 11/03/2005 | CA2555836A1 Control system for vehicles |
| 11/02/2005 | EP1591705A1 Valve |
| 11/02/2005 | EP1590717A1 Device for controlling a vehicle |
| 10/27/2005 | WO2005100154A1 System for rotor head and rotor blade |
| 10/25/2005 | CA2257338C Method for controlling an aerodyne for the vertical avoidance of a zone |
| 10/20/2005 | US20050234607 Control system and method with multiple linked inputs |
| 10/20/2005 | US20050234606 Aircraft mode suppression |
| 10/20/2005 | US20050230566 Method and apparatus for loss of control inhibitor systems |
| 10/20/2005 | US20050230564 Automatic takeoff apparatus for aircraft, automatic landing apparatus for aircraft, automatic takeoff and landing apparatus for aircraft, automatic takeoff method for aircraft, automatic landing method for aircraft and automatic takeoff and landing method for aircraft |
| 10/20/2005 | US20050230563 Automatic formation flight control system |
| 10/20/2005 | US20050230534 Methods and apparatus for vibration and buffet suppression |
| 10/20/2005 | US20050229729 Actuator with two motors, a differential reducer and a torque limiter |
| 10/19/2005 | EP1586969A1 Automatic takeoff apparatus for aircraft, automatic landing apparatus for aircraft, automatic takeoff and landing apparatus for aircraft, automatic takeoff method for aircraft, automatic landing method for aircraft and automatic takeoff and landing method for aircraft |
| 10/19/2005 | CN1684870A Rotorcraft control system with stepped mixing linkage |
| 10/18/2005 | US6955324 Laser-tethered vehicle |
| 10/18/2005 | CA2270752C Reduced wing effort feature for aircraft |
| 10/18/2005 | CA2182758C Compound rudder control system on a vehicle structure |
| 10/13/2005 | US20050225456 Helicopter tactile exceedance warning system |
| 10/13/2005 | US20050224659 Intelligent multifunctional actuation system for vibration and buffet suppression |
| 10/06/2005 | US20050218262 Process for improving the landing of an aircraft |
| 10/06/2005 | DE102005011118A1 Brake mechanism for aircraft uplifting system, has hydraulic system, having own supply, connected to motor such that movement of motor/drive shaft is braked or motor/shaft is released from brake position |
| 09/27/2005 | CA2204065C Method and apparatus for turn coordination gain as a function or flap position |
| 09/22/2005 | DE19547316B4 Umschaltkupplung Shift clutch |
| 09/15/2005 | CA2500887A1 Braking device for a high-lift system of an aircraft and aircraft with such a device |
| 09/14/2005 | EP1574923A2 Aircraft mode suppression |
| 09/14/2005 | CN1218859C Manipulator of power-boosting ground effect aircraft for ground effect transition region |
| 09/08/2005 | US20050193887 Back-pressure valve and actuation system |
| 09/01/2005 | WO2005079460A2 Linkage and sensor assembly |
| 08/31/2005 | EP1568605A1 Method and device for the optimization of the deployment of the spoiler of an aircraft during flight |
| 08/25/2005 | WO2005077470A1 Device for exercising the musculature of an ankle and device for controlling the movement of an external element |
| 08/25/2005 | US20050187677 PFN/TRAC systemTM FAA upgrades for accountable remote and robotics control to stop the unauthorized use of aircraft and to improve equipment management and public safety in transportation |
| 08/24/2005 | EP1565673A2 Standardized rotary actuator |
| 08/24/2005 | EP1565373A1 Augmenting flight control surface actuation system and method |
| 08/18/2005 | US20050178927 Linear, hydraulic pivot drive |
| 08/18/2005 | US20050178926 Disengage device |
| 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 |
| 08/18/2005 | US20050178885 Method and apparatus for supporting aircraft components, including actuators |
| 08/18/2005 | US20050178215 Linkage and sensor assembly |
| 08/16/2005 | US6929222 Non-jamming, fail safe flight control system with non-symmetric load alleviation capability |
| 08/16/2005 | US6929216 Method and apparatus for installing and actuating movable airfoils, including canards |
| 08/16/2005 | CA2201078C Device for maintaining the speed of an aircraft within a range of determined speeds |
| 08/11/2005 | US20050173595 Helicopter force-feel and stability augmentation system with parallel servo-actuator |
| 08/11/2005 | US20050173593 Forward pivoted full flying control tail boom |
| 08/10/2005 | EP1562091A1 Method for improving the landing of an aircraft |
| 08/10/2005 | CN1653273A Integrated three function valve |
| 08/09/2005 | US6928340 Process and system for moving a control surface 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 | WO2005021970A3 Regulated pressure supply for a variable-displacement reversible hydraulic motor |