Patents
Patents for B64C 13 - Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers (4,795)
09/2013
09/04/2013CN103274044A 飞行器舵板传动机构 Aircraft rudder actuator
09/03/2013US8527180 Systems and methods for controlling aircraft electrical power
09/03/2013US8527173 Method and system for managing the energy variation of an aircraft
09/03/2013US8527118 Automated safe flight vehicle
09/03/2013US8523116 Panel-mounted aircraft control stick
09/03/2013US8523102 Method and apparatus for aircraft sensor and actuator failure protection using reconfigurable flight control laws
09/03/2013CA2657474C Flap actuator
08/2013
08/29/2013WO2013126357A1 Retention mechanism and method for removeably supporting a portable flight controller
08/28/2013EP2631171A2 Aircraft actuator hydraulic system
08/28/2013EP2631170A1 Device for generating force feedback for control sticks such as aircraft joysticks
08/28/2013EP2630034A2 System for motorized displacement of a mobile element, method of driving such a system and method of testing such a system
08/28/2013CN102390524B Method for determining using priority of each control surface of multi-control-surface aircraft during over-the-horizon stage
08/27/2013US8517314 Actuator arrangement
08/24/2013CA2807019A1 System and method for automation of rotorcraft entry into autorotation and maintenance of stabilized autorotation
08/22/2013WO2013121323A1 Shock touch protection of a mobile device
08/22/2013US20130214092 Aerodynamic body with an ancillary flap
08/21/2013EP2629168A2 Method and system for providing sideslip envelope protection
08/21/2013CN103253368A Pneumatic bionic muscle
08/21/2013CN102046467B Error tolerant actuation system for adjusting servo tabs of an aircraft, comprising a control mechanism with a fixed rotational axis, method for monitoring actuation system
08/21/2013CN101905742B A piloting assistance device, a hybrid helicopter provided, and a method implemented by said device
08/21/2013CN101484355B Adjusting device for adjusting a high-lift flap and airfoil wing comprising such an adjusting device
08/20/2013US8515609 Flight technical control management for an unmanned aerial vehicle
08/20/2013US8513582 Method for stepping a first member relative to a second member associated with a projectile
08/20/2013US8511621 Device for piloting a craft having an electromagnetic actuator
08/20/2013US8511619 Slat deployment mechanism
08/15/2013WO2013120031A1 Autopilot control arrangement and methods
08/15/2013WO2013119242A1 Actuator system and method
08/15/2013US20130211631 Integrated Aircraft Flight Control Units
08/15/2013US20130211629 Display system
08/15/2013US20130206922 Method of Guidance for Aircraft Trajectory Correction
08/15/2013US20130206917 High-positioned 3-position variable camber krueger
08/15/2013US20130206916 System and method for minimising buffeting
08/15/2013US20130206898 Pilot Control System with Pendent Grip
08/14/2013EP2626593A1 Electro mechanical actuator
08/14/2013EP2626301A2 Pilot control system with pendent grip
08/14/2013EP2626300A1 Pilot control system with hand rest
08/14/2013EP2626299A1 Pilot control system with adjustable pedals
08/14/2013EP2626297A1 Integrated aircraft flight control units
08/14/2013EP2626296A1 Pilot control system with compact gimbal mechanism
08/14/2013EP2625104A1 High lift system for an aircraft with a separate drive unit for each wing half
08/14/2013EP2625097A1 High-lift system for a wing of an aircraft
08/14/2013DE102012002921A1 Servoventil Servo valve
08/14/2013CN203127140U Large-torque ball screw electric steering machine
08/14/2013CN103241368A Linear actuator and aircraft component comprising same
08/14/2013CN101962074B Control rod
08/13/2013US8508173 Adjustable ergonomic control console with user login
08/13/2013US8505854 Flight assistance apparatus
08/10/2013CA2804821A1 An improved electro mechanical actuator
08/10/2013CA2804801A1 Pilot control system with adjustable pedals
08/10/2013CA2804411A1 Pilot control system with compact gimbal mechanism
08/10/2013CA2804332A1 Pilot control system with pendent grip
08/10/2013CA2804196A1 Integrated aircraft flight control units
08/10/2013CA2803524A1 Pilot control system with hand rest
08/10/2013CA2795637A1 High-positioned 3-position variable camber krueger
08/08/2013DE102012002067A1 Luft-Boden-Überwachungs- und/oder Wirksystem und Verfahren zur luftgestützten Inspektion und/oder Bekämpfung von auf dem Land oder auf See befindlichen Objekten Air-to-ground surveillance and / or active system and method for airborne inspection and / or combating located on land or at sea objects
08/08/2013DE102012002033A1 Flugsystem Flight Systems
08/07/2013CN103231798A Control device of digital electric steering engine and control method
08/07/2013CN103231797A Four-axle-linkage electric steering engine
08/06/2013US8504221 Apparatus and method for controlling a control surface of a vehicle based on a load identified on the control surface
08/06/2013US8500065 Device for supplying loads in the overhead area of a passenger cabin, in particular in commercial aircraft
08/06/2013US8500064 Hybrid power system architecture for an aircraft
08/06/2013US8499653 Fault tolerant electro-mechanical actuator
07/2013
07/31/2013EP2620362A2 Flight control system mode and method providing aircraft speed control through the usage of momentary on-off control
07/31/2013CN103224022A Gray sliding-mode control used for double-Y type brushless direct-current electric steering engine and device thereof
07/30/2013US8496204 Method and system for minimizing axial backlash in a dual load path fail-safe aircraft actuator system
07/30/2013CA2469165C Display system
07/25/2013WO2013107656A1 Rotation lock
07/25/2013US20130187009 Aircraft with wings and a system for minimizing the influence of unsteady flow states
07/25/2013DE102012000987A1 Rotationssperre Rotation lock
07/24/2013EP2617646A2 Aircraft actuator hydraulic system
07/24/2013EP2616334A1 Method and apparatus for actively manipulating aerodynamic surfaces
07/24/2013EP2616332A1 Method and apparatus for actively manipulating aerodynamic surfaces
07/24/2013CN103213683A Small multipurpose unmanned plane with oil tank embedded into blended wing body
07/24/2013CN103213673A Control method for double-Y-type brushless direct current electric steering engine and driving device
07/18/2013US20130181089 Adjustment system of an aeroplane with an adjustable flap
07/17/2013EP2615514A2 Quiet landing attitude modifier for airplane
07/17/2013EP2615026A1 Method and apparatus for minimizing dynamic structural loads of an aircraft
07/17/2013CN101868407B Landing flap mechanism driven by pinion gears
07/17/2013CN101443560B Ballistically tolerant linear hydraulic actuator
07/16/2013US8485477 Rotational aircraft throttle interface
07/16/2013US8484962 System and method for the temperature regulation of a hydraulic fluid
07/11/2013CA2793199A1 Quiet landing attitude modifier for airplane
07/10/2013CN203047529U Adjusting device
07/10/2013CN103201171A System for motorized displacement of a mobile element, method of driving such a system and method of testing such a system
07/10/2013CN103192985A Novel integrated structure pull bar for airplane
07/09/2013US8480037 Device for determining the position of a throttle lever in an aircraft
07/03/2013EP2610168A1 Adjustable pitch link
07/03/2013CN101802454B Method and device for fault detection in the load path of a spindle actuator
07/02/2013US8478457 Fatigue management system
07/02/2013US8474761 Method of piloting a rotary wing drone having multiple rotors
07/02/2013US8474752 Actuator force equalization controller
07/02/2013US8474486 Actuator system
06/2013
06/27/2013WO2013095391A1 Controller for an external device
06/27/2013US20130166103 Aircraft exploration system
06/27/2013US20130162418 Motor generated detent feel
06/26/2013EP2607229A2 Composite rod, manufacturing method and tool
06/26/2013EP2605962A2 A wing control system
06/26/2013CN102105356B Assembly of actuators and of a system for supplying electrical power from a network
06/25/2013US8469317 Line replaceable, fly-by-wire control columns with push-pull interconnect rods
06/25/2013CA2568848C Method and device for improving maneuverability of an aircraft during approach phases before landing followed by flare-out
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