Patents
Patents for B64C 13 - Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers (4,795)
03/2013
03/27/2013EP2572980A2 Active feedback user interface system and gimbal assembly therefor
03/23/2013CA2782041A1 Aircraft flap mechanism having compact large fowler motion providing multiple cruise positions
03/21/2013US20130068892 Flying apparatus for aerial agricultural application
03/21/2013US20130068882 Flying saucer
03/21/2013DE112010005656T5 Elektromechanische Antriebseinrichtung der aerodynamischen Fläche des Flugzeuges Electromechanical drive means of the aerodynamic surface of the aircraft
03/21/2013DE102011113952A1 Actuator system for aircraft for adjusting load of aircraft, has electric motor-driven actuating device and eddy current brake for converting mechanical energy partially or completely into heat by introducing load into actuating device
03/20/2013EP2570880A2 A method for real-time model based structural anomaly detection
03/20/2013CN202815448U Multipath PWM signal generating device suitable for unmanned plane steering engine control
03/19/2013US8401716 Flight control systems
03/19/2013US8398019 Adjusting device for adjusting a high-lift flap and airfoil wing comprising such an adjusting device
03/13/2013CN202794931U Steering engine controller
03/12/2013US8393570 Landing flap kinematics driven by way of a pinion drive
03/12/2013US8393569 Breakable coupling device, and an associated trim actuator
03/12/2013US8393568 Enhanced lubrication skewed roller clutch assembly and actuator including same
03/07/2013WO2012052438A3 System for motorized displacement of a mobile element, method of driving such a system and method of testing such a system
03/06/2013EP2563655A1 Device for detecting the breakage of a primary path in a flight control actuator
03/06/2013CN202765287U Unmanned aerial vehicle onboard flight control system
03/06/2013CN102060104B Micro-switch assembly
02/2013
02/28/2013WO2013026582A1 Hub of a wind turbine
02/27/2013CN102947177A Power supply and control device for actuators, corresponding actuation assembly, and aircraft comprising such a device
02/26/2013US8386092 Hold line awareness using tactile devices
02/26/2013CA2536802C Variable cam exhaust nozzle
02/21/2013US20130043353 Lenticular airship and associated controls
02/20/2013EP2558817A1 Automatic flight control for uav based solid modeling
02/20/2013CN102935891A Airplane design method and scheme
02/19/2013US8380364 Manual and computerized flight control system with natural feedback
02/19/2013US8376271 Aircraft actuator
02/14/2013WO2013023123A2 Control quadrant
02/14/2013US20130041528 Intelligent modular aerospace system
02/14/2013US20130041527 Variable bandwidth control actuation methods and apparatus
02/14/2013US20130037658 Aircraft with a control device
02/13/2013EP2557467A2 Device and method for the evaluation of a residual for detecting systematic errors in the system behaviour of a system of an aircraft
02/13/2013EP2557034A2 Hybrid power system architecture for an aircraft
02/13/2013CN202728576U Transformable composite aircraft formed by fixed wing and electric multi-propeller
02/12/2013US8374804 Aircraft dynamic pressure estimation system and method
02/12/2013US8373376 Drive system and method for activating the same
02/12/2013US8371535 Method for releasing an unmanned missile from a carrier aircraft
02/12/2013CA2502617C Process and device for securing a low-altitude flight by an aircraft
02/07/2013US20130035808 Aircraft with a control device
02/07/2013US20130031997 Four-bar vehicle controller providing up to three independent or combined axes of control and improved cockpit and control input ergonomics
02/06/2013CN102917947A Device for detecting the breakage of a primary path in a flight control actuator
02/05/2013US8366054 Hand launchable unmanned aerial vehicle
02/05/2013CA2508805C Control system for airbrakes of an aircraft
02/05/2013CA2503048C Process and device for determining a safe altitude for an aircraft
01/2013
01/31/2013WO2013015791A1 Electric motor clamping system
01/31/2013WO2013015783A1 Rudder bias gain changer
01/31/2013US20130026299 Method And Device For An Optimal Management Of The Slats, The Flaps And The Landing Gear Of An Aircraft
01/31/2013US20130026298 Actuator force equalization controller
01/31/2013US20130026287 Method And Device For Detecting An Uncontrolled Movement Of An Aircraft Control Surface
01/31/2013CA2842825A1 Electric motor clamping system
01/31/2013CA2841447A1 Rudder bias gain changer
01/30/2013EP2551191A1 Method and device for detecting the deployment of an aircraft control surface.
01/30/2013CN101808896B Automatic control of a high lift system of an aircraft
01/29/2013CA2580776C Autonomous flight for flight platforms
01/24/2013WO2013013084A1 Personal aircraft
01/24/2013US20130022945 Display System
01/24/2013US20130020444 Trailing Edge Split Flap with Pneumatic Actuation
01/24/2013CA2841315A1 Personal aircraft
01/23/2013EP2548799A1 Aerodynamic coefficient estimation device and control surface failure/damage detection device
01/23/2013CN202686757U Deceleration system with self-locking function for steering engine
01/23/2013CN202686756U Control surface deflection angle limiting device
01/23/2013CN101678894B Method for adding resistance during landing and the aircraft
01/22/2013US8359130 Method and device for attenuating on an aircraft the effects of a vertical turbulence
01/17/2013WO2012136804A3 High lift system for an aircraft
01/16/2013CN202670092U Light aircraft flap control device
01/15/2013CA2643029C Actuation system for a lift assisting device and roller bearings used therein
01/10/2013WO2013006340A1 Electronically synchronized flap system
01/10/2013US20130009016 Retractable vortex generator for reducing stall speed
01/10/2013US20130009014 Instantaneous wireless network established by simultaneously descending parafoils
01/10/2013CA2840391A1 Electronically synchronized flap system
01/09/2013EP2543589A1 Primary flight controls
01/09/2013CN202657242U Rocker mechanism
01/09/2013CN102862675A A simplified user interface for an aircraft
01/09/2013CN102219051B Method for controlling four-rotor aircraft system based on human-computer interaction technology
01/09/2013CN101604353B Method of designing an airfoil assembly
01/08/2013CA2782447A1 A simplified user interface for an aircraft
01/08/2013CA2731552C Assembly of actuators and of a system for supplying electrical power from a network
01/03/2013US20130001366 Landing system
01/03/2013US20130001357 Horizontal stabilizer trim actuator failure detection system and method using position sensors
01/03/2013US20130000432 Device for adjusting and locking a movable control surface
01/02/2013EP2540621A1 Control system of aircraft, method for controlling aircraft, and aircraft
01/01/2013US8346409 Variable speed flap retraction and notification
12/2012
12/27/2012WO2012178181A1 Apparatus to eliminate back drive in push pull system of rotor aircraft and related methods
12/27/2012US20120325977 Aircraft with a device for directionally stabilizing the aircraft, computer program product and method for directionally stabilizing the aircraft
12/27/2012US20120325976 Slat monitoring system
12/27/2012US20120325959 Adjustable servomechanism assemblies and associated systems and methods
12/27/2012CA2840379A1 Apparatus to eliminate back drive in push pull system of rotor aircraft and related methods
12/26/2012CN102837821A Controller of steering engine
12/25/2012US8340840 Method and device for reducing on an aircraft lateral effects of a turbulence
12/25/2012US8336827 Method and device for reducing the induced speeds in vortices in the wake of an aircraft
12/25/2012US8336818 Jam tolerant electromechanical actuation systems and methods of operation
12/25/2012US8336817 Jam tolerant electromechanical actuation systems and methods of operation
12/20/2012WO2012173632A1 Self-sustaining drone aircraft freight and observation system
12/20/2012US20120318929 Aircraft with a refueling device and method for controlling the flight path of an aircraft during its refueling
12/20/2012CA2839581A1 Self-sustaining drone aircraft freight and observation system
12/18/2012CA2602667C Landing flap drive system
12/13/2012US20120312931 Flap adjusting system of an aircraft with a regulating flap
12/13/2012DE102011106127A1 Vorrichtung zur Reduzierung von Strukturschwingungen von Tragflügeln An apparatus for reducing structural vibrations of airfoils
12/12/2012EP2532585A2 Method and assembly for attaching components
12/12/2012EP2532584A2 Method and apparatus for attaching components having dissimilar rates of thermal expansion
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