Patents
Patents for B64C 13 - Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers (4,795)
12/2012
12/12/2012EP2532583A2 Telescopic actuator
12/12/2012CN202593853U Novel control surface control device
12/12/2012CN202593851U All-moving wing aircraft without control plane
12/12/2012CN101301930B Improved load detection on a flight control actuator
12/06/2012US20120305701 Aircraft control surface drive mechanism
12/06/2012US20120305698 Method and Apparatus for Actively Manipulating Aerodynamic Surfaces
12/06/2012DE102007028919B4 Vorrichtung und Verfahren zur Temperaturregelung eines Hydraulikfluids Device and method for temperature control of a hydraulic fluid
12/05/2012EP2530012A2 Aircraft control surface drive mechanism
12/05/2012CN102806992A Resolver type skew sensor with gimbal attachment
12/05/2012CN102806991A Deployable aerodynamic devices with reduced actuator loads
12/05/2012CN102806990A Portable mapping unmanned aerial plane
12/04/2012US8322136 Method for operating a turbo charger and controller
11/2012
11/29/2012US20120303210 Suppressing electrical failure effects in servo control systems
11/29/2012US20120298806 Control system of aircraft, method for controlling aircraft, and aircraft
11/28/2012EP2527248A2 Suppressing electrical failure effects in servo control systems
11/28/2012CN102795336A High integrity linear actuator and method of operation
11/28/2012CN102795334A Method of determining the static force developed by a servo-control
11/22/2012WO2012156772A1 Apparatus and method for maintaining a tension in a cable control system
11/22/2012WO2012155418A1 Side rod control device
11/22/2012US20120296500 Aerodynamic coefficient estimation device and control surface failure/damage detection device
11/22/2012CA2836641A1 Apparatus and method for maintaining a tension in a cable control system
11/21/2012EP2524865A1 Aircraft wing assembly
11/21/2012CN101879942B Helicopter rotor wing automatic clutch control system with safety protection function
11/20/2012CA2611558C Method and device for driving an aircraft during the ground run thereof
11/15/2012US20120286102 Remotely controlled vtol aircraft, control system for control of tailless aircraft, and system using same
11/15/2012DE102012009149A1 Bidirectional operable rotational lock for tie rod of braking system to actuate horizontal tail units of airplane, has mechanical device connected with mass so that device is movable along axial direction when applying torque
11/15/2012DE102011101348A1 Control device, particularly for aircraft, has rotational drive and linear control movement, which has load transmitting components for transferring force or torque, where part of load transmitting components is redundant
11/14/2012CN202529144U Gear transmission device with balance and redundancy protection functions
11/14/2012CN102781774A Aircraft with a control device
11/14/2012CN102777545A Aircraft and long-service-life electric steering engine thereof
11/14/2012CN102774496A Slit control device of circulation control tail beam of helicopter
11/08/2012DE102011100481A1 Flugzeug mit einer Vorrichtung zur Richtungsstabilisierung des Flugzeugs, Computerprogrammprodukt sowie Verfahren zur Richtungsstabilisierung des Flugzeugs Aircraft with a device for stabilization of the direction of the aircraft, computer program product and method for stabilization of direction of the aircraft
11/07/2012EP2520995A2 Aircraft with a device for directionally stabilizing the aircraft, computer program product and method for directionally stabilizing the aircraft
11/07/2012CN102765475A Air vehicle and electric steering engine capable of resisting large bending torque thereof
11/07/2012CN102765474A Lenticular airship and associated controls
11/01/2012US20120277933 Flight Controller Management System with a Backdrive Monitor
11/01/2012US20120273623 Rotational Aircraft Throttle Interface
10/2012
10/31/2012EP2516892A1 Device for adjusting and locking a movable control surface
10/31/2012EP2516261A2 Aircraft with a control device
10/31/2012CN102762450A Adjustment mechanism of an adjustment device for coupling an adjustment flap to a main wing, and such an adjustment device
10/26/2012WO2012101645A4 Dynamic limitation of monoblock flight control surfaces inclinations during stall susceptibility conditions
10/25/2012DE102011018446A1 Adjusting device for aircraft or airplane, has rotary drive and linear actuating movement, which has load-transmitting components, where force or torque is transferred by load-transmitting components
10/24/2012EP2512916A1 Response mode for control system of piloted craft
10/24/2012CN102753435A Aerodynamic coefficient estimation device and control surface failure/damage detection device
10/18/2012US20120261517 Multi-Element Airfoil System
10/18/2012US20120261508 Active gurney flap
10/17/2012EP2511173A1 Lenticular Airship and Associated Controls
10/17/2012EP2509857A1 Control surface assembly
10/17/2012CN102730186A Rotary actuator and method of operation with failsafe mechanism
10/11/2012WO2012136804A2 High lift system for an aircraft
10/11/2012US20120256055 Aircraft rotary wing motion control and instrumented motion control fluid device
10/11/2012DE102011016336A1 Hochauftriebssystem für ein Luftfahrzeug High-lift system for an aircraft
10/10/2012CN102717889A Flap control method and device of light airplane
10/10/2012CN102717888A Flap assembly of aircraft
10/04/2012WO2012131330A1 Actuator control system
10/04/2012US20120253556 Redundant two stage electro-hydraulic servo actuator control
10/04/2012US20120248260 Flight Trajectory Compensation System for Airspeed Variations
10/04/2012US20120248258 Flight Path Control System For Aircraft
10/04/2012US20120248257 Adjusting mechanism for kinematic guidance of an adjustable body during its adjustment on a supporting structural component, adjusting mechanism for kinematic adjustment of a high lift body, and high lift system comprising a like adjusting mechanism
10/04/2012US20120248254 Method of communication on an aircraft or a spacecraft, via the outside environment
10/04/2012DE102012102729A1 Hochzuverlässige Drehaktuatoren und Betriebsverfahren Highly reliable rotary actuators and operating procedures
10/04/2012CA2831492A1 Actuator control system
10/04/2012CA2773175A1 Self pumping and priming adhesive joint system
10/03/2012EP2505497A1 Actuator control system
10/03/2012EP2505496A2 Redundant two stage electro-hydraulic servo actuator control
10/03/2012EP2505495A1 Electromechanical actuator
10/03/2012CN102712359A Response mode for control system of piloted craft
10/03/2012CN102700708A Speed-increasing tail device of helicopter
10/03/2012CN102700706A Dual-redundancy actuator system and control method
09/2012
09/30/2012CA2772480A1 High integrity rotary actuator and method of operation
09/27/2012DE102011014835A1 Vorrichtung zum Verstellen einer Fläche eines Fluggerätemodells, Flächeneinheit, Fluggerätemodell und Verwendung eines Fluggerätemodells Device for adjusting a surface of a flying device model unit area, aircraft model and the use of a aircraft model
09/27/2012DE102011014687A1 Lasteinleitungselement für eine bewegbare Fläche eines Flugzeugs, Flugzeug mit mindestens einer bewegbaren Fläche und mindestens einem Lasteinleitungselement und Verfahren zum Lösen einer mit einem Lasteinleitungselement verbundenen bewegbaren Fläche Load transfer element for a movable surface of an aircraft, aircraft with at least one movable surface and at least one load transfer element and method for solving a movable surface connected to a load transfer element
09/26/2012EP2502826A1 A flying saucer
09/26/2012EP2502825A1 Backup control by linear actuator for manual flight command chain of an aircraft and Method
09/26/2012EP2501947A1 Transmission assembly for a drive system of storage spaces of an aircraft
09/26/2012CN102695649A Control system of aircraft, method for controlling aircraft, and aircraft
09/25/2012US8275496 Longitudinal and vertical gust feed forward compensation using lateral control surfaces
09/25/2012US8272599 Control lever assembly for a tilt-rotor aircraft
09/20/2012WO2012124594A1 Control system of aircraft, aircraft, control program for aircraft, and control method for aircraft
09/20/2012US20120234985 Cyclic stick for mechanically transmitting commands for controlling a rotorcraft, the stick having a lever arm that is amplified selectively in the event of an emergency
09/20/2012US20120234983 Control surface assembly
09/20/2012DE102009002682B4 Einrichtung und Verfahren zur Residuenauswertung eines Residuums zur Erkennung von Systemfehlern im Systemverhalten eines Systems eines Flugzeugs Apparatus and method for Residuenauswertung a residuum to detect system errors in the system behavior of a system of an aircraft
09/20/2012CA2828444A1 Aircraft control system, aircraft, aircraft control program, and method for controlling aircraft
09/19/2012EP2500267A1 Monitoring of a flight control actuator of an aircraft
09/19/2012EP2500266A1 Electrically powered actuator and control method.
09/19/2012EP2500265A1 Cyclic joystick with mechanical transmission for controlling a rotorcraft, including a lever arm selectively amplified in the event of an emergency
09/19/2012EP2500262A1 Lenticular Airship and Associated Controls
09/19/2012EP2500261A1 Lenticular Airship and Associated Controls
09/19/2012CN102673780A Double-configuration aircraft
09/19/2012CN102673777A Installation sliding bush device being suitable for control steel cable of power device
09/11/2012US8265807 Automatic takeoff and landing apparatus for aircraft, and methods for performing an automatic takeoff and an automatic landing of an aircraft
09/11/2012US8264218 Wing flap sensor unit
09/07/2012WO2012117280A1 Control computer for an unmanned vehicle
09/07/2012WO2012117009A1 A method of operating actuators simultaneously for moving aircraft flaps, an aircraft flap drive device, and an aircraft provided with such a device
09/07/2012CA2831216A1 Control computer for an unmanned vehicle
09/07/2012CA2826455A1 A method of operating actuators simultaneously for moving aircraft flaps, an aircraft flap drive device, and an aircraft provided with such a device
09/05/2012CN202414157U Flap equal-ratio homothetic motion guaranteeing mechanism
09/05/2012CN202414156U General airplane audio controller
09/04/2012US8256718 Method and device for providing automatic load alleviation to a high lift surface system, in particular to a landing flap system, of an aircraft
09/04/2012US8256714 Modularized airplane structures and methods
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