| 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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| 08/03/2011 | CN102143886A Slat support assembly |
| 08/02/2011 | US7988099 Winglet |
| 07/27/2011 | EP2346734A1 Active winglet |
| 07/27/2011 | CN101750978B Open platform for supporting design, verification and validation of telex flight control system |
| 07/27/2011 | CN101506038B Jam-tolerant actuator |
| 07/26/2011 | US7987025 Stores dependent angle of attack feedback |
| 07/26/2011 | US7984880 Mechanisms and methods for providing rudder control assist during symmetrical and asymmetrical thrust conditions |
| 07/26/2011 | US7984670 Hydraulic distributor provided with a device for detecting seizing |
| 07/26/2011 | CA2490843C Apparatus for driving and adjusting of flaps hinged to an aircraft |
| 07/21/2011 | WO2011066030A3 Systems and devices for remotely operated unmanned aerial vehicle report-suppressing launcher with portable rf transparent launch tube |
| 07/21/2011 | US20110174921 Flight control system for an aircraft |
| 07/21/2011 | US20110174920 Flight control system especially suited for vtol vehicles |
| 07/21/2011 | DE10313728B4 Klappensystem am Tragflügel eines Starrflügel-Flugzeuges Flap system on the wing of a fixed-wing aircraft |
| 07/20/2011 | EP2345579A2 Compact electromechanical actuator |
| 07/20/2011 | EP2345181A1 Methods and systems for providing full avionics data services over a single fiber |
| 07/20/2011 | EP2076433B1 Active human-machine interface system without a force sensor |
| 07/20/2011 | CN102126552A Flight control system |
| 07/18/2011 | CA2727592A1 Flight control system for an aircraft |
| 07/14/2011 | WO2011020593A3 Adjustment mechanism of an adjustment device for coupling an adjustment flap to a main wing, and such an adjustment device |
| 07/14/2011 | US20110168851 Automatic trim system for fly-by-wire aircraft with unique trim controllers |
| 07/14/2011 | CA2728235A1 Compact electromechanical actuator |
| 07/13/2011 | EP2342113A1 System provided with an assistance-controller for assisting an operator of the system, control-operation assisting device, control-operation assisting method, driving-operation assisting device, and driving-operation assisting method |
| 07/13/2011 | CN102123911A Light multipurpose aircraft provided with a control integrated system |
| 07/13/2011 | CN102120489A Tilt ducted unmanned aerial vehicle |
| 07/12/2011 | US7975671 Engine speed control device, a method for controlling engine speed and an aircraft provided therewith |
| 07/12/2011 | CA2727467A1 Minimum temperature control for electromechanical actuator |
| 07/07/2011 | US20110163206 Helicopter control stick support assembly |
| 07/07/2011 | US20110163204 High lift system for an aircraft with a high lift flap and method for adjusting the high lift flap |
| 07/06/2011 | EP2340994A1 Helicopter control stick support assembly |
| 07/06/2011 | EP2212193B1 Method and device for reducing the induced speeds in vortices in the wake of an aircraft |
| 07/06/2011 | CN102114912A Aircraft |
| 06/30/2011 | US20110155861 Device for piloting a craft having an electromagnetic actuator |
| 06/30/2011 | US20110155840 Morphing aircraft |
| 06/30/2011 | DE102009060327A1 Flugzeug mit einer Steuerungsvorrichtung Aircraft with a control device |
| 06/30/2011 | CA2784945A1 Aircraft with a control device |
| 06/29/2011 | EP2338789A2 Actuator control system |
| 06/29/2011 | CN102112371A System and method for determining characteristic parameters in aircraft |
| 06/29/2011 | CN102107731A Actuator control system |
| 06/29/2011 | CN102107730A Dynamic controller of hinge-free aircraft |
| 06/23/2011 | WO2011072362A1 Response mode for control system of piloted craft |
| 06/23/2011 | CA2784615A1 Response mode for control system of piloted craft |
| 06/22/2011 | EP2336023A2 Feedback torque limiter |
| 06/22/2011 | DE102007027698B4 Dualer Linear-Aktuator Dual linear actuator |
| 06/22/2011 | CN102106100A Methods and systems for providing full avionics data services over a single fiber |
| 06/22/2011 | CN102105356A Assembly of actuators and of a system for supplying electrical power from a network |
| 06/16/2011 | WO2011070536A2 Method and system for automatic logging of flight-hour data of components in aircrafts |
| 06/16/2011 | WO2011070347A1 Control surface assembly |
| 06/16/2011 | US20110139938 Aircraft reaction link |
| 06/16/2011 | US20110139937 Method and apparatus for deploying an auxiliary lift foil |
| 06/16/2011 | DE102006020554B4 Verbindungsstrebe zur Anordnung zwischen benachbarten Landeklappen eines Flugzeuges Connecting strut for arrangement between adjacent flaps of an aircraft |
| 06/15/2011 | EP2332838A1 Device for testing load bearing detection of a secondary channel of a flight control actuator, and associated testing method |
| 06/15/2011 | EP2332830A2 Aircraft reaction link |
| 06/15/2011 | CN101421157B Rotary wing vehicle |
| 06/09/2011 | WO2011068659A2 Active winglet |
| 06/09/2011 | US20110133037 Personal flight vehicle including control system |
| 06/09/2011 | DE102009057405A1 Flugzeug mit einer Anordnung von Strömungsbeeinflussungs-Vorrichtungen Aircraft with an array of flow influencing devices |
| 06/08/2011 | EP2328806A1 Error tolerant adjustment system for adjusting servo tabs of an aircraft, comprising a control mechanism with a fixed rotational axis |
| 06/08/2011 | EP2328805A2 High lift system for an aircraft with a high lift flap and method for adjusting the high lift flap |
| 06/08/2011 | CN201856894U Left and right separable soft/hard hybrid operation linear system for airplane |
| 06/08/2011 | CN101467114B Method for piloting an aircraft in approach phase |
| 06/08/2011 | CN101454200B Flying process and device of an aircraft optimizing the control of ailerons in a high-lift configuration |
| 06/08/2011 | CA2724857A1 Testing device to detect load bearing by a secondary channel of a flight control actuator and associated testing process |
| 06/07/2011 | US7956606 Position sensing assembly |
| 06/07/2011 | US7954756 Flap actuator |
| 06/03/2011 | WO2011066031A2 Elevon control system |
| 06/03/2011 | WO2011066030A2 Systems and devices for remotely operated unmanned aerial vehicle report-suppressing launcher with portable rf transparent launch tube |
| 06/03/2011 | CA2789726A1 Elevon control system |
| 06/03/2011 | CA2789722A1 Systems and devices for remotely operated unmanned aerial vehicle report-suppressing launcher with portable rf transparent launch tube |
| 06/02/2011 | US20110130913 Unmanned aerial vehicle control systems |
| 06/02/2011 | US20110127384 Flying vehicle |
| 06/02/2011 | US20110127380 Advanced aircraft cockpit |
| 06/02/2011 | US20110127375 Method for monitoring a no-back device of an adjustable horizontal trim actuator, corresponding system and aircraft |
| 06/01/2011 | CN101389532B Electrical control system for an aircraft steering vane |
| 06/01/2011 | CN101378956B Rotor blade for a rotary wing aircraft |
| 05/26/2011 | US20110121140 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 |
| 05/25/2011 | CN102076559A Position sensing assembly |
| 05/24/2011 | US7946536 Device for interconnecting first and second control sticks of an aircraft in roll and in pitch |
| 05/24/2011 | US7946528 Flight control system especially suited for VTOL vehicles |
| 05/19/2011 | WO2011057819A1 Transmission assembly for a drive system of storage spaces of an aircraft |
| 05/18/2011 | EP2322808A2 Electro-hydrostatic actuator with damping mechanism, drive device and control method using such an actuator |
| 05/18/2011 | EP2321709A1 Force gradient using a non-contact proximity sensor |
| 05/18/2011 | CN201836290U Friction damping device |
| 05/18/2011 | CN102066195A No-back device and method for determining the apparent operational integrity of a no-back device |
| 05/18/2011 | CN102060104A Micro-switch assembly |
| 05/17/2011 | US7945353 Adaptive control in the presence of input constraints |
| 05/12/2011 | US20110112705 Electronic control device for a piloting member with multifunctional microcontrollers, piloting device and aircraft |
| 05/12/2011 | US20110108674 Cockpit Rudder Control Mechanism For An Aircraft |
| 05/12/2011 | US20110108673 Electronic operational control device for a piloting member with cross-monitoring, piloting device and aircraft |
| 05/12/2011 | US20110108664 Flap actuator |
| 05/11/2011 | EP2318278A2 Advanced primary navigation displays for precision and non-precision approaches |
| 05/11/2011 | EP2318270A2 Assembly of actuators and of a system for supplying electrical power from a network |
| 05/11/2011 | EP2318269A2 Slat support assembly |
| 05/11/2011 | CN201829334U Rotating electric steering engine and contactless rotating transformer thereof |
| 05/11/2011 | CN101486379B Coaxial unmanned helicopter course operating circuit and method for determining parameter K |
| 05/11/2011 | CN101331056B Method and device for providing automatic load alleviation to a high lift surface system, in particular to a landing flap system, of an aircraft |
| 05/05/2011 | WO2011052822A1 Portable unmanned airship for magnetic-force surveying and a magnetic-force surveying system employing the same |
| 05/05/2011 | WO2010151230A3 Actuator system for flap on rotor blade of a wind turbine |
| 05/05/2011 | US20110101176 Control station |
| 05/05/2011 | US20110101171 Apparatus for Twisting a Wing to Increase Lift on Aircraft and Other Vehicles |
| 05/05/2011 | DE102009050748A1 Flugzeug mit an einem zentralen Rumpfkörper angebundenen Seitenleitwerken und Verfahren sowie Regeleinheit zum Kompensieren eines negativen Nickmoments Aircraft with tethered to a central fuselage body vertical stabilizers and procedures, and control unit for compensating a negative pitching moment |