| 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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| 05/04/2011 | EP2316727A1 High-lift device track |
| 05/04/2011 | CN102046467A Error tolerant adjustment system for adjusting servo tabs of an aircraft, comprising a control mechanism with a fixed rotational axis |
| 04/28/2011 | WO2011048399A1 Tactile cueing apparatus |
| 04/28/2011 | US20110094848 Method and apparatus for determining the apparent operational integrity of a no-back device |
| 04/28/2011 | CA2778058A1 Tactile cueing apparatus |
| 04/27/2011 | CN102036877A Method for monitoring the output of an electromechanical actuator of the rotary-linear type |
| 04/26/2011 | US7931239 Homeostatic flying hovercraft |
| 04/21/2011 | US20110089877 Fault-tolerant electromechanical actuator having a torque sensing control system |
| 04/21/2011 | DE102005059933B4 Flechttechnisch hergestelltes Faserverbundbauteil Flechttechnisch manufactured fiber composite component |
| 04/20/2011 | EP2311729A1 Tactile cueing apparatus |
| 04/20/2011 | CN201800912U Combined double-body unmanned airship |
| 04/20/2011 | CN102026867A Control system for a hydraulically actuatable horizontal stabilizer and test method for testing the integrity of a control system |
| 04/19/2011 | CA2444404C Force-limiting rotary lock |
| 04/14/2011 | WO2011042746A1 Vehicle armrest |
| 04/14/2011 | US20110084173 Method and device for providing automatic load alleviation to a high lift surface system, in particular to a landing flap system, of an aircraft |
| 04/13/2011 | EP2308752A1 Cockpit handgrip and armrest with at least one control operable by the ocupant whilst resting his forearm on the armrest. |
| 04/13/2011 | CN102009743A Blowing based fuselage high incidence pitching moment control method |
| 04/13/2011 | CN101628623B Method for solving electromagnetic compatibility of horizontal tail rudder surface control system of airplane |
| 04/13/2011 | CN101585411B Hydraulic servo steering engine system |
| 04/06/2011 | EP2303686A2 Position sensing assembly |
| 04/06/2011 | CN102001444A Neutral position adjustment device of flight control system and neutral position setting method thereof |
| 04/06/2011 | CN102001443A Composite spring |
| 04/05/2011 | US7920794 Free space optical communication |
| 03/31/2011 | WO2010118886A3 High lift system for an airplane, airplane system and propeller airplane having a high lift system |
| 03/30/2011 | EP2300318A2 Wing-body load alleviation for aircraft |
| 03/30/2011 | CN201779215U Rotary electric steering engine and harmonic reducer thereof |
| 03/29/2011 | US7913955 Aircraft control surface drive system and associated methods |
| 03/24/2011 | WO2011034236A1 Flight control system for an unmanned aerial vehicle using the postural change of a controller, and method for operating flight control system |
| 03/24/2011 | WO2011032937A2 Method for simulating specific movements by haptic feedback, and device implementing the method |
| 03/24/2011 | US20110068221 Control System for a Hydraulically Actuatable Horizontal Stabilizer and Test Method for Testing the Integrity of a Control System |
| 03/23/2011 | EP2296965A1 System and method for determining characteristic parameters in an aircraft |
| 03/23/2011 | CN101988570A Design method of gears and racks for airplane slat actuators |
| 03/17/2011 | WO2011030901A1 Aircraft flight control system |
| 03/17/2011 | US20110062282 Fault-tolerant actuating system for adjusting flaps of an aircraft, comprising adjustment kinematics with a fixed pivot, and a method for monitoring an actuating system |
| 03/16/2011 | EP1960263B1 Method and device for providing automatic load alleviation to a high lift surface system, in particular to a landing flap system, of an aircraft |
| 03/15/2011 | US7906749 System and method for deployment and actuation |
| 03/10/2011 | US20110057074 Modular miniature unmanned aircraft with vectored thrust control |
| 03/09/2011 | EP2293429A2 Secured surveillance and control device for an aircraft handling actuator |
| 03/09/2011 | EP2292513A1 Actuator with integrated status monitoring system and method for manufacturing same |
| 03/08/2011 | CA2714354A1 Secure monitoring and control device for aircraft piloting actuator |
| 03/03/2011 | WO2010125080A4 Device and method for the residual analysis of a residuum to detect system errors in the system behavior of an aircraft |
| 03/03/2011 | US20110048147 Aircraft stabilizer actuator |
| 03/03/2011 | DE202010013203U1 Zug-Druck-Stange mit Bolzenelement und Halteband Train-push rod with bolt member and tether |
| 03/03/2011 | DE102009037707A1 Verstellmechanismus einer Verstellvorrichtung zur Ankopplung einer Verstellklappe an einen Hauptflügel und eine solche Verstellvorrichtung Adjusting an adjustment device for coupling a shift valve to a main wing and such adjustment |
| 02/24/2011 | US20110042524 Passive adaptive structures |
| 02/23/2011 | EP2285673A1 No-back device and method for determining the apparent operational integrity of a no-back device |
| 02/23/2011 | EP2004482B1 Method and device for flying an aircraft about an aircraft axis |
| 02/17/2011 | US20110036944 Slat deployment mechanism |
| 02/16/2011 | EP2284078A2 Improved load detection on a flight control actuator |
| 02/15/2011 | CA2437216C Procedure and system to move the elevator of an aircraft |
| 02/09/2011 | CN101970292A Modularized airplane structures and methods |
| 02/08/2011 | US7883059 Actuator systems and associated methods for unmanned air vehicles and other applications |
| 02/03/2011 | US20110024566 Electrical power transfer assmebly |
| 02/03/2011 | US20110024551 Variable damping of haptic feedback for a flight-attitude changing linkage of an aircraft |
| 02/03/2011 | DE102009027979A1 Verfahren und Vorrichtung zum Bereitstellen eines Pilotwarn-Signals für einen Piloten eines Flugzeuges Method and apparatus for providing a pilot-warning signal for a pilot of an aircraft |
| 02/03/2011 | DE102009003938B4 Flüssigkeitsleitung, Verwendung einer Flüssigkeitsleitung und Flugzeug mit mindestens einer Flüssigkeitsleitung Liquid line, using a liquid line and plane with at least one liquid line |
| 02/02/2011 | EP2280194A1 Rotary actuator |
| 02/02/2011 | EP2279941A1 Variable damping of haptic feedback for kinematic linkage to change the flight attitude of an aircraft |
| 02/02/2011 | CN201729037U Airphibious aircraft |
| 02/02/2011 | CN101962074A Control rod |
| 02/01/2011 | US7878461 System and method for an integrated backup control system |
| 01/27/2011 | WO2011009492A1 Selective aileron system |
| 01/26/2011 | EP2276664A1 Control system for a hydraulically actuatable horizontal stabilizer and test method for testing the integrity of a control system |
| 01/19/2011 | EP2274200A1 Landing flap mechanism driven by pinion gears |
| 01/19/2011 | CN201712787U Electric tilt rotor unmanned aircraft |
| 01/19/2011 | CN101948007A Automatic center returning and resetting device of handle |
| 01/13/2011 | US20110006166 Rotary wing vehicle |
| 01/13/2011 | US20110006156 Hydraulic actuator with end position damping |
| 01/13/2011 | US20110006155 Actuator Arrangement |
| 01/13/2011 | US20110006154 Enhanced Lubrication Skewed Roller Clutch Assembly And Actuator Including Same |
| 01/12/2011 | EP2137067B1 Method and device for moveable tail trimming in an aircraft |
| 01/11/2011 | US7866602 Sensing load relief by a secondary path of a flight control actuator |
| 01/11/2011 | CA2462217C Adaptive flap and slat drive system for aircraft |
| 01/05/2011 | CN201694387U Automatic aircraft pilot actuator steel rope connecting device |
| 01/05/2011 | CN101939220A Distributed flight control system |
| 01/05/2011 | CN101934858A Miniature electric ducted propeller type intelligent unmanned aerial vehicle |
| 12/30/2010 | US20100327124 Method and device for laterally trimming an airplane during a flight |
| 12/30/2010 | US20100327122 Air-vehicle augmented kinesthetic control system |
| 12/30/2010 | US20100327111 Electrical power transmitting telescopic strut |
| 12/30/2010 | DE102005016638B4 Flügelklappen-Mechanismus zur Verstellung einer einem Tragflügel zugeordneten aerodynamischen Flügelklappe Wing flap mechanism for adjusting a associated with a wing aerodynamic flap |
| 12/29/2010 | EP2267569A1 Aircraft multi-axis modal suppression system for reducing torsional vibration in the aircraft structure |
| 12/29/2010 | EP2041453B1 Flap actuator |
| 12/23/2010 | WO2010125080A3 Device and method for the residual analysis of a residuum to detect system errors in the system behavior of an aircraft |
| 12/23/2010 | US20100320314 Lenticular airship and associated controls |
| 12/22/2010 | EP2162641B1 Method and device for fault detection in the load path of a spindle actuator |
| 12/21/2010 | CA2580272C Control system for automatic flight in windshear conditions |
| 12/21/2010 | CA2472291C System for automatically controlling an aircraft's high-lift devices, in particular the leading-edge slats on the wings |
| 12/21/2010 | CA2389096C Aircraft spiralling mechanism - 2 |
| 12/16/2010 | WO2010142771A1 Device for actuating a control surface of an aircraft |
| 12/16/2010 | WO2010105818A3 An aircraft comprising a device for influencing the directional stability of the aircraft, and a method for influencing the directional stability of the aircraft |
| 12/15/2010 | EP2261120A1 Landing method for an unmanned helicopter |
| 12/15/2010 | EP2261116A2 Automatic trim system for fly-by-wire aircraft with unique trim controllers |
| 12/15/2010 | CN201670358U Double-duct vertical take-off and landing unmanned aerial vehicle |
| 12/09/2010 | US20100308179 Electric power actuator and control method for such an actuator |
| 12/09/2010 | US20100308178 Variable ratio crank for a manual flight control linkage of a rotary wing aircraft |
| 12/09/2010 | US20100308162 Landing flap kinematics driven by way of a pinion drive |
| 12/08/2010 | EP2257469A1 Method and device for detecting absences of manual and automatic piloting of an aircraft |
| 12/08/2010 | EP1989466B1 Jam-tolerant actuator |
| 12/08/2010 | CN101909992A System for actuating at least one regulating flap of an aircraft and a method for checking the system. |
| 12/08/2010 | CN101905742A A piloting assistance device, a hybrid helicopter provided, and a method implemented by said device |