| Patents for B64C 13 - Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers (4,795) |
|---|
| 07/26/2007 | WO2007084529A2 System and method for an integrated backup control system |
| 07/25/2007 | CN101006403A Electric flight control system for aircraft elevators |
| 07/19/2007 | WO2007079855A1 Rotor blade for a rotary wing aircraft |
| 07/19/2007 | US20070164168 System and method for an integrated backup control system |
| 07/19/2007 | US20070164167 Autorotation flight control system |
| 07/18/2007 | EP1807304A1 Method and device for enhancing the braking efficiency of an aircraft during the ground run thereof |
| 07/18/2007 | CN101001781A Method and device for improving maneuverability of an aircraft during approach phases before landing followed by flare-out |
| 07/12/2007 | US20070162196 Autonomous control system apparatus and program for a small, unmanned helicopter |
| 07/12/2007 | US20070159126 Bilateral servo controller |
| 07/12/2007 | DE102005062919A1 Tragfläche für ein Flugzeug und Flugzeug Wing for an aircraft and aircraft |
| 07/11/2007 | EP1642181A4 System and method for controlling model aircraft |
| 07/10/2007 | CA2290118C Automatic guidance system for flight vehicle having parafoil and navigation guidance apparatus for the system |
| 07/05/2007 | WO2007074173A2 Airfoil for an aircraft and aircraft |
| 07/05/2007 | WO2007061641A3 Wing load alleviation apparatus and method |
| 07/05/2007 | DE102005061750A1 Flexible Steuerfläche für ein Luftfahrzeug Flexible control surface for an aircraft |
| 07/05/2007 | DE102005059369A1 Verfahren und Einrichtung zur automatischen Entlastung eines Hochauftriebsflächensystems, insbesondere eines Landeklappensystems, eines Flugzeugs Method and apparatus for automatic discharge of a high lift surface system, especially a landing flap system, of an aircraft |
| 07/04/2007 | EP1803644A2 Distributed flight control surface actuation system |
| 07/04/2007 | EP1802940A2 Mechanical flight control auxiliary power assist system |
| 07/04/2007 | EP1557588B1 Load transfer detection device through breakable shear pin |
| 07/03/2007 | US7237747 Device for assisting an airplane in intercepting a segment of a flight path utilizing positional and ground speed indicators |
| 06/28/2007 | US20070145184 Device and system for assistance within interception by an aircraft of a flight path segment |
| 06/28/2007 | US20070145183 A device for assisting an airplane in intercepting a segment of a flight path utilizing positional and ground speed indicators |
| 06/27/2007 | CN1989041A Aircraft with wings whose maximum lift can be altered by controllable wing components |
| 06/27/2007 | CN1323244C Integrated three function valve |
| 06/21/2007 | WO2007068413A2 Method and device for providing automatic load alleviation to a high lift surface system, in particular to a landing flap system, of an aircraft |
| 06/21/2007 | DE102005059423A1 Verfahren und Einrichtung zur redundanten Versorgung von mehreren elektrischen Stell-oder Antriebsmotoren durch eine gemeinsame Leistungselektronikeinheit Method and apparatus for redundant power supply for several electric servo-drive motors or by a common power electronics unit |
| 06/21/2007 | CA2628531A1 Method and device for providing automatic load alleviation to a high lift surface system, in particular to a landing flap system, of an aircraft |
| 06/20/2007 | EP1797487A2 Autonomous flight for flight platforms |
| 06/20/2007 | CN2913182Y Flexible shaft driving device for airplane trailing flap control system |
| 06/14/2007 | US20070131822 Aerial and ground robotic system |
| 06/14/2007 | DE102005059933A1 Fiber composite articles, especially tension or traction struts, comprise core with curved edges which surround inner peripheries of longitudinal bores whose outer edges are enclosed by peripheral flocked fiber composite strip |
| 06/13/2007 | EP1795987A2 Actuator |
| 06/12/2007 | US7229047 Aircraft roll disconnect mechanism |
| 06/12/2007 | US7229046 Servo mounting system for direct drive of an aircraft control surface |
| 06/12/2007 | CA2297567C System for aircraft yaw control |
| 06/06/2007 | EP1793477A1 Fault-tolerant electro-mechanical actuator having a torque sensing control system |
| 06/06/2007 | EP1791755A1 Aircraft with wings whose maximum lift can be altered by controllable wing components |
| 06/05/2007 | US7226020 Apparatus for driving and adjusting flaps hinged to an aircraft |
| 05/31/2007 | WO2007061641A2 Wing load alleviation apparatus and method |
| 05/31/2007 | US20070120011 Active multistable twisting device |
| 05/30/2007 | EP1790567A2 Electro-hydraulic actuator system |
| 05/30/2007 | EP1789315A2 System and method for remote control of interdiction aircraft |
| 05/30/2007 | CN2905657Y Aviation device |
| 05/29/2007 | US7225063 Aircraft control system |
| 05/29/2007 | US7225061 Method and device for detecting pilot induced oscillations in an aircraft |
| 05/24/2007 | WO2007057638A1 Aircraft cooling duct |
| 05/23/2007 | EP1786668A1 No-back device having malfunction detection |
| 05/23/2007 | EP1786667A1 Systems and methods for providing differential motion to wing high lift devices |
| 05/22/2007 | US7219861 Guidance system for radio-controlled aircraft |
| 05/18/2007 | WO2007056294A2 A method and means for piloting control of a forward-moving vehicle |
| 05/17/2007 | US20070109745 High Integrity and Availability Multi-Channel Systems |
| 05/17/2007 | US20070108343 Flight control surface actuator assembly including a free trail mechanism |
| 05/17/2007 | US20070108342 Reconfigurable flight control surface actuation system and method |
| 05/16/2007 | EP1785347A2 Reconfigurable flight control surface actuation system and method |
| 05/16/2007 | EP1785346A2 Flight control surface actuator assembly |
| 05/16/2007 | CN1965182A Compact actuator |
| 05/15/2007 | US7216831 Shape changing structure |
| 05/15/2007 | CA2255996C Aircraft flight control actuator |
| 05/10/2007 | US20070102590 Method and means for piloting control of a forward-moving vehicle |
| 05/10/2007 | US20070102574 Securing a vehicle |
| 05/10/2007 | US20070102573 Ice protection system for aircraft |
| 05/10/2007 | DE102005038017B3 Verfahren zur Flugführung mehrerer im Verband fliegender Flugzeuge Procedures for flight guidance of several aircraft flying in the association |
| 05/09/2007 | EP1781538A1 Aircraft flight control surface actuation system communication architecture |
| 05/03/2007 | WO2007048936A1 Engine speed control device, a method for controlling engine speed and an aircraft provided therewith |
| 05/03/2007 | US20070096675 Mobile robot charge station return system |
| 05/03/2007 | CA2627691A1 Engine-speed control device, method for controlling engine speed and aircraft equipped with such a device |
| 05/01/2007 | US7211980 Robotic follow system and method |
| 04/26/2007 | DE10151663B4 Steuervorrichtung für einen funkferngesteuerten Modellhelikopter Control apparatus for a radio-controlled model helicopter |
| 04/25/2007 | EP1776625A1 Electric flight control system for aircraft elevators |
| 04/24/2007 | US7209809 Method and apparatus for obtaining high integrity and availability in multi-channel systems |
| 04/19/2007 | WO2007042652A1 Method and device for attenuating on an aircraft the effects of a vertical turbulence |
| 04/19/2007 | US20070084971 Wireless-controlled airplane |
| 04/19/2007 | CA2622110A1 Method and device for attenuating on an aircraft the effects of a vertical turbulence |
| 04/18/2007 | EP1773655A1 Device for antagonistic artificial force gradient for an aircraft control surface remote control device |
| 04/10/2007 | US7201700 Geared rotary actuators |
| 04/10/2007 | US7201347 Process for improving the landing of an aircraft |
| 04/05/2007 | DE102005042511A1 Trim actuator actuating system for airplane, has autonomous hydraulic power supply system to supply hydraulic power to hydraulic linear actuator during malfunction operation in which another power supply system is in breakdown state |
| 04/04/2007 | EP1770010A2 Control device with a joystick for an aircraft |
| 04/04/2007 | EP1768900A1 Device for remote control of an aircraft control surfaces |
| 04/04/2007 | EP1768899A1 Method and device for improving maneuverability of an aircraft during approach phases before landing followed by flare-out |
| 04/03/2007 | CA2270753C Mixed operating system for aircraft aerodynamic surface |
| 03/29/2007 | WO2007034079A1 Method and device for carrying out at least one flight testing on an aircraft and the use thereof |
| 03/29/2007 | US20070069071 Systems and methods for providing back-up hydraulic power for aircraft, including tanker aircraft |
| 03/29/2007 | US20070069070 Energy recovery apparatus and method |
| 03/29/2007 | CA2620187A1 Method and device for carrying out at least one flight testing on an aircraft and the use thereof |
| 03/27/2007 | US7195209 Aircraft high-lift system with overload protection |
| 03/27/2007 | US7195208 Multi-device controller for model aircraft |
| 03/27/2007 | US7195200 Unmanned helicopter, takeoff method of unmanned helicopter, and landing method of unmanned helicopter |
| 03/22/2007 | WO2006035429A3 Autonomous flight for flight platforms |
| 03/22/2007 | DE102005033697A1 Control surface e.g. rudder, operating mechanism for airplane, has gearing placed downstream of hydraulic motor so that drive shaft of motor drives input shaft of gearing, and output shaft coincides with rotational axis of rudder |
| 03/21/2007 | CN1934562A Control system for vehicles |
| 03/20/2007 | US7191985 Aircraft multi-axis modal suppression system |
| 03/15/2007 | WO2007030028A1 Method and a set of means for piloting an aircraft |
| 03/15/2007 | WO2007028597A1 Trim actuator actuating system for a hydraulically actuatable trimmable horizontal stabilizer actuator |
| 03/15/2007 | US20070057114 Procedure and device for improving the maneuverability of an aircraft during the approach to landing and flare-out phases |
| 03/15/2007 | DE102005042510A1 Locking mechanism for fixing linear actuator of airplane, has positive locking units, which are arranged at distance from one another in longitudinal direction of cylinder, where piston rod of linear actuator is fixed opposite to cylinder |
| 03/15/2007 | CA2618671A1 Trim actuator actuating system for a hydraulically actuatable trimmable horizontal stabilizer actuator |
| 03/13/2007 | US7190096 Fault-tolerant electro-mechanical actuator having motor armatures to drive a ram and having an armature release mechanism |
| 03/08/2007 | WO2006016070A8 Method and device for improving maneuverability of an aircraft during approach phases before landing followed by flare-out |
| 03/08/2007 | US20070055434 Automatic control system for controllin a vehicle on demand |