Patents
Patents for B64C 13 - Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers (4,795)
12/2010
12/08/2010CN101508339B Directly connected-type direct current electric steering engine of rocker structure
12/02/2010WO2010137596A1 Mobile body control device and mobile body in which mobile body control device is mounted
12/02/2010WO2010136188A1 Aircraft having a vertical lift system
12/02/2010US20100305780 Flight control system and method of separating control lever linkage
12/02/2010DE102009022602A1 Flugzeug mit einem Hochauftriebssystem Aircraft with a high-lift system
12/02/2010DE102005016639B4 Tragflügel mit ausfahrbaren aerodynamischen Flügelklappen, insbesondere Auftriebsklappen Wing with extendable aerodynamic wing flaps, in particular lift flaps
12/01/2010EP2256372A1 Spindle drive
12/01/2010EP2256033A1 Spindle drive
11/2010
11/30/2010CA2496776C Rotorcraft control system with stepped mixing linkage
11/25/2010US20100295303 Tethered system for power generation
11/25/2010DE102009020840A1 Flugzeughochauftriebssystem sowie Verfahren zur Ermittlung eines Betriebszustandes eines Flugzeughochauftriebssystems Aircraft lift augmentation system and method for determining an operating state of an aircraft high-lift system
11/24/2010EP2252506A1 Rotational aircraft throttle interface
11/24/2010CN201647123U Inflatable type flexible wing flap
11/23/2010US7837144 Fluid-driven artificial muscles as mechanisms for controlled actuation
11/23/2010US7837143 Method and apparatus for disabling pilot control of a hijacked aircraft
11/23/2010CA2650292C Ballistically tolerant linear hydraulic actuator
11/23/2010CA2476903C Linear hydraulic pivot drive
11/16/2010US7834494 Fault-tolerant electromechanical actuator having a torque sensing control system
11/11/2010US20100282899 System for Actuating at least One Positioning Flap of an Aircraft and a Method for Monitoring the System.
11/10/2010CN101879945A Electric tilting rotor wing unmanned aerial vehicle
11/10/2010CN101879942A Helicopter rotor wing automatic clutch control system with safety protection function
11/04/2010WO2010103157A4 System for increasing controllability for an aircraft
11/04/2010DE102009002682A1 Residuum analyzing device for detecting e.g. oscillations in behaviors of electrohydraulic rudder positioning system of aircraft, has threshold value providing unit for providing threshold value by associating constant and adaptive portions
11/03/2010CN201619690U Dual-spring double-gradient load mechanism
11/03/2010CN101370701B Long-range control system
10/2010
10/28/2010WO2010121384A1 Splitter plate for hybrid airship control
10/28/2010US20100270426 Aircraft actuator
10/27/2010EP1700041B1 Redundant flow control for hydraulic actuator systems
10/21/2010WO2010119280A1 High lift devices for aircraft
10/21/2010WO2010119209A1 Control system for a turboreactor nacelle
10/21/2010WO2010119204A1 Thrust reversal device
10/21/2010US20100264263 Integrated load sensing system
10/21/2010DE102009017653A1 Hochauftriebssystem eines Flugzeugs, Flugzeugsystem und Propeller-Flugzeug mit einem Hochauftriebssystem High-lift system of an aircraft, aircraft system and propeller aircraft with a high-lift system
10/21/2010DE102009002215A1 Controllable valve for hydraulic control of flame-resistant fluid within aircraft, has magnetic coil which moves component, provided in magnetic coil, from position to another position by short-term electric excitation
10/21/2010CA2758461A1 A high-lift system for an aeroplane, an aeroplane system and a propeller-driven aeroplane with a high-lift system
10/21/2010CA2758132A1 Control system for a turboreactor nacelle
10/21/2010CA2758091A1 Thrust reversal device
10/20/2010EP2240365A2 System for actuating at least one regulating flap of an aircraft and a method for checking the system
10/20/2010CN101868407A Landing flap mechanism driven by pinion gears
10/19/2010US7818100 System and method for optimized runway exiting
10/14/2010WO2010116509A1 Maneuver assisting device
10/14/2010WO2010116232A1 Enhanced lubrication skewed roller clutch assembly and actuator including it
10/14/2010US20100258678 Aircraft stall protection system
10/14/2010CA2758138A1 Enhanced lubrication skewed roller clutch assembly and actuator including it
10/13/2010EP2238026A1 Distributed flight control system
10/13/2010EP2238025A2 Vertical gust suppression for transport aircraft
10/13/2010CN201604794U 波音747飞机前缘襟翼动力组件控制盒 747 leading edge flap control box power components
10/13/2010CN101857086A Dual-culvert vertical take-off and landing unmanned aerial vehicle
10/12/2010CA2591645C Variable gradient control stick force feel adjustment system
10/07/2010WO2010114656A1 Transport system incorporating linear motor charged electric vehicle
10/07/2010WO2010112513A1 Aircraft flight control system comprising a connecting rod provided with a sensor
10/07/2010US20100256839 Performing Corrective Action on Unmanned Aerial Vehicle Using One Axis of Three-Axis Magnetometer
10/07/2010US20100252691 Aircraft electrical actuator arrangement
10/06/2010EP2236413A2 An aircraft electrical actuator arrangement
10/06/2010CN1934562B Control system for vehicles
10/06/2010CN101267987B Method and device for carrying out at least one flight testing on an aircraft and the use thereof
10/06/2010CN101218551B Method and device for lightening loads on the wing system of an aircraft in roll motion
10/05/2010US7809480 Autonomous flight for flight platforms
10/05/2010US7806372 Full authority fly-by-wire pedal system
10/05/2010US7806371 Remote control model aircraft with laser tag shooting action
09/2010
09/30/2010WO2010110795A1 Method and apparatus for optimizing a load in a flight control system while an aircraft is on the ground
09/30/2010WO2010084338A3 Bearing assembly
09/30/2010US20100250022 Useful unmanned aerial vehicle
09/29/2010CN201592775U Large bending moment resistant steering engine
09/29/2010CN201592774U Device for eliminating the flying side force of aircraft
09/23/2010US20100237199 Adjustable servomechanism assemblies and associated systems and methods
09/23/2010DE102009013758A1 Flugzeug mit einer Vorrichtung zur Beeinflussung der Richtungsstabilität des Flugzeugs sowie Verfahren zur Beeinflussung der Richtungsstabilität des Flugzeugs Aircraft with a device for influencing the directional stability of the aircraft as well as methods for influencing the directional stability of the aircraft
09/21/2010US7798443 Composite material for geometric morphing wing
09/16/2010WO2010103234A1 Aircraft control system with integrated modular architecture
09/16/2010WO2010103233A1 Distributed flight control system implemented according to an integrated modular avionics architecture
09/16/2010WO2010103157A1 System for increasing controllability for an aircraft
09/16/2010CA2754091A1 Aircraft control system with integrated modular architecture
09/16/2010CA2754031A1 Distributed flight control system implemented according to an integrated modular avionics architecture
09/15/2010EP1996459B1 Multi-mode unmanned and manned vehicle systems and methods
09/15/2010CN101346276B Airfoil for an aircraft and aircraft
09/14/2010US7793890 Control system for an aircraft
09/14/2010CA2607358C System for controlling flight direction
09/10/2010WO2010100436A2 Unmanned air vehicle (uav), control system and method
09/09/2010US20100228406 UAV Flight Control Method And System
09/07/2010US7788990 Lever device for operating a hydraulic actuator
09/07/2010US7788988 Drive assemblies
09/07/2010CA2475208C Control system for vertical take off and land (vtol) aircraft
09/02/2010US20100219298 Method and device for generating an optimum aerodynamic configuration of an aircraft during a flight
09/01/2010EP2222551A1 System and method for deployment and actuation
09/01/2010CN201566835U Aircraft steering wheel-like control device
08/2010
08/26/2010WO2010094952A1 Aircraft wing load alleviation system
08/26/2010US20100213311 Electromechanical actuating assembly
08/26/2010US20100213310 Shuttle Stop Force Limiter
08/26/2010DE112008002046T5 Steuervorrichtung Control device
08/25/2010EP1966045B1 Rotor blade for a rotary wing aircraft
08/24/2010CA2510115C Device and method for damping at least one of a rigid body mode and elastic mode of an aircraft
08/19/2010WO2010092222A1 Aircraft command and control unit
08/19/2010US20100206993 Steering structure of toy plane and infrared four-channel remote-control electric toy plane
08/18/2010EP1282555B1 Multi-mode tiltrotor nacelle control system
08/18/2010CN1914426B Redundant flow control for hydraulic actuator systems
08/18/2010CN101808896A Automatic control of a high lift system of an aircraft
08/18/2010CN101804862A Thrust steering device of unmanned aerial vehicle and control method thereof
08/17/2010US7777165 Methods and apparatus for adjustable surfaces
08/17/2010CA2418228C This is the english title
08/12/2010WO2010052590A8 Safety retention device for an actuator
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