Patents
Patents for B64C 13 - Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers (4,795)
06/2013
06/20/2013US20130153713 Translating cable device sealing
06/19/2013EP2604515A1 Method and system for controlling a high-lift device or a flight control surface, and air- or spacecraft comprising such system
06/19/2013EP2604514A2 Automatically locking linear actuator
06/19/2013CN101970292B Modularized airplane structures and methods
06/19/2013CN101535125B Aerodynamic body and carrier wing comprising an aerodynamic body, actuating drive control module, computer, computer program, and method for influencing post-turbulences
06/14/2013CA2797715A1 Translating cable device sealing
06/13/2013WO2013023123A3 Control quadrant
06/13/2013US20130146705 Wing control system
06/12/2013CN202987499U Racemic shifting fork
06/12/2013CN103153791A High lift system for an aircraft with a separate drive unit for each wing half
06/12/2013CN103153784A High-lift system for a wing of an aircraft
06/12/2013CN101263050B Trim actuator actuating system for a hydraulically actuatable trimmable horizontal stabilizer actuator
06/12/2013CA2793044A1 Wing variable camber trailing edge tip
06/11/2013CA2502615C Process and device for automatically determining a capture trajectory of an aircraft's flight path and automatic aircraft guidance method and system
06/06/2013WO2013081697A2 Jam protection and alleviation for control surface linkage mechanisms
06/06/2013DE102011120389A1 Method for determining operability of load path of positioning device, involves removing component of load path, and establishing connection between two load paths, where test tool is coupled with undeveloped component of former load path
06/06/2013DE102011119946A1 Positioning device for positioning e.g. landing flap at fuselage of aircraft, has upper and lower gaps provided in load path, and detent unit of detent device penetrating into gaps when component of another load path is damaged
06/05/2013CN202966662U Unmanned helicopter for spraying pesticides
06/05/2013CN202966656U Small integrated electric steering engine assembly
06/05/2013CN202966655U Four-axis aircraft balance stabilization control device based on cross-flow fan drive
06/05/2013CN102009743B Blowing based fuselage high incidence pitching moment control method
06/04/2013US8457872 Method for managing the flight of an aircraft
06/04/2013US8457809 Electronic device and method for controlling unmanned aerial vehicle using the same
06/04/2013US8456125 Debris sensor for cleaning apparatus
05/2013
05/30/2013WO2013076158A1 An electromechanical actuator for an aircraft control surface, and an aircraft provided with such an actuator
05/30/2013US20130134262 Jam Protection and Alleviation for Control Surface Linkage Mechanisms
05/30/2013US20130134258 Aerodynamic wing load distribution control
05/30/2013CA2854239A1 An electromechanical actuator for an aircraft control surface, and an aircraft provided with such an actuator
05/29/2013EP2597034A1 Counterbalanced control stick system
05/29/2013DE102008031266B4 Verwendung eines Thermogenerators an einem Luftfahrzeug Using a thermal generator on an aircraft
05/29/2013CN202953172U Motor-driven steering engine
05/29/2013CN102001443B Composite spring
05/28/2013US8450894 Fault-tolerant electromechanical actuator having a torque sensing control system
05/28/2013CA2791970A1 Counterbalanced control stick system
05/28/2013CA2555836C Control system for vehicles
05/23/2013US20130126680 Unmanned air vehicle fault tolerant flight control system and method
05/23/2013US20130126670 Deployment system
05/22/2013EP2595023A2 Aircraft control apparatus and aircraft control system
05/21/2013US8447445 Dynamic adjustment of wing surfaces for variable camber
05/18/2013CA2795775A1 Method of guidance for aircraft trajectory correction
05/16/2013US20130119194 Trailing-edge flap system
05/16/2013DE102011118321A1 Hydraulic rotary drive for e.g. tail structure of aircraft, has several hydraulic linear actuators that are arranged side by side and are connected with common crankshaft such that crankshaft is rotatable upon actuation of actuators
05/16/2013DE102011118240A1 Mechanischer Lösemechanismus Mechanical release mechanism
05/15/2013CN202935576U Coaxial aircraft
05/15/2013CN202935571U Aircraft flap device
05/15/2013CN202935570U Portable mapping unmanned aerial plane
05/14/2013US8442736 System for enhancing cornering performance of a vehicle controlled by a safety system
05/08/2013DE102011117706A1 Propulsion system for flaps e.g. landing flaps of aircraft, has drive unit arranged at distance in half wing from wing root such that maximum rotational loads arising at elements of drive train are reduced
05/08/2013DE102011117620A1 Vorrichtung zur Reduzierung einer Druckschwankung in einer fluidgefüllten Leitung Apparatus for reducing a pressure fluctuation in a fluid-filled pipe
05/08/2013CN103097241A A device for an adjustable flap of a wing
05/08/2013CN103085968A Compact two axis gimbal for control stick
05/07/2013US8437891 Method and apparatus for parafoil guidance that accounts for ground winds
05/02/2013US20130105634 Compact two axis gimbal for control stick
05/02/2013US20130105623 Device for detecting breakage of a primary path in a flight control actuator
05/02/2013DE102011114222A1 Electronic load limitation function for electromechanical actuator of flight controller, performs manipulation of control signals of actuator to reduce load and to retrieve nominal control, when position load exits permissible load range
05/01/2013EP2587350A2 Method for determining valid touch screen inputs
05/01/2013EP2586702A2 Compact two axis gimbal for control stick
04/2013
04/30/2013CA2620187C Method and device for carrying out at least one flight testing on an aircraft and the use thereof
04/25/2013WO2013058173A1 Aircraft and aircraft control method
04/25/2013WO2013058171A1 Aircraft and aircraft control method
04/25/2013US20130099064 Methods And Systems For Providing Constant-Feel, Multi-Axis Tactile Cues
04/24/2013EP2584173A1 Gas Turbine Engine
04/24/2013EP2583896A1 Methods and Systems for Providing Constant-Feel, Multi-Axis Tactile Cues
04/24/2013EP2582577A2 Sequential power supply system for actuators and aircraft comprising such a system
04/24/2013CN202896880U Spherical micro unmanned aerial vehicle
04/24/2013CN103057698A Device for adjusting camber angle of V-shaped empennage
04/24/2013CN103057697A Rudder pedal control apparatus for airplane, and control method thereof
04/24/2013CN103057696A Novel fixed-wing aircraft starting device
04/24/2013CN101844618B Method and device for optimizing the operation of propulsive propellers disposed on either side of rotorcraft fuselage
04/23/2013US8428793 Automatic downlink messaging during emergency flight situations
04/23/2013US8424801 Slat support assembly
04/17/2013CN202879792U Suspension type aviation camera shooting and tracing autonomous aircraft system
04/17/2013CN103051373A Self-rotor unmanned aerial vehicle-based air emergency communication system
04/17/2013CN102198857B Assessment method for wing level of airplane based on robot and height detection unit
04/17/2013CN101909992B System for actuating at least one regulating flap of an aircraft and a method for checking the system.
04/16/2013US8418967 Passive adaptive structures
04/16/2013CA2520064C Device for detecting synchronous errors of high-lift surfaces on aircraft
04/11/2013WO2013051300A1 Disaster circumstance ascertainment system
04/11/2013US20130087662 Flap support
04/11/2013DE102012009657B3 Method for detecting and identifying oscillatory error in flight control system of aircraft, involves determining residual on basis of control signal, position, provided vector indicating aircraft flight condition and model
04/11/2013DE102011115362A1 Modular electronic flight control system for controlling actuators in e.g. primary flight controls of e.g. civilian aircraft, has control units comprising electronic control of actuators and arranged and distributed in airplane
04/11/2013DE102011115360A1 Electronic flight control system for controlling and monitoring of actuators of flight control of e.g. military aircraft, has electronic units connected with one another over bus system to control actuators in multiplex mode
04/11/2013DE102011115359A1 Electronic device, particularly smart actuator electronics, such as remote electronic unit for actuator control system for positioning actuator, is attached directly or indirectly to actuator or is partially integrated in actuator
04/11/2013DE102011115356A1 Flight control system for electronic control of actuators of e.g. military aircraft, has flight control devices for performing signal transmissions via digital data bus i.e. triple-redundant bidirectional bus
04/11/2013DE102011115318A1 Flight control system for aircraft, has actuator control electronics and actuators connected with each other through data network, where control electronics are connected in addition to another data network of redundant implemented system
04/10/2013EP2576340A2 A device for an adjustable flap of a wing
04/10/2013CN202863758U Steering engine with angle information feedback function
04/10/2013CN103029829A Hydraulic return locking device for dual-redundancy steering engine
04/10/2013CN103029827A Flap support
04/09/2013US8417395 Hierarchical closed-loop flow control system for aircraft, missiles and munitions
04/09/2013US8414260 Control system for controlling propeller aircraft engine during takeoff
04/04/2013WO2013002874A3 Shape memory alloy actuator system and method
04/04/2013US20130082149 Power supply and control device for actuators, corresponding actuation assembly, and aircraft comprising such a device
04/04/2013US20130082136 Method and apparatus for actively manipulating aerodynamic surfaces
04/03/2013CN103010457A Electrical rudder control system for an aircraft
04/03/2013CN102123911B Light multipurpose aircraft provided with a control integrated system
04/03/2013CN101792022B Small multipurpose unmanned aerial vehicle with oil tank embedded into blended wing body
04/02/2013US8408500 Cable carrier chain for leading edge mobile slat for an aircraft wing
03/2013
03/28/2013US20130075537 Aircraft flap mechanism having compact large fowler motion providing multiple cruise positions
03/28/2013US20130075535 Electrical rudder control system for an aircraft
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