Patents
Patents for B64C 13 - Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers (4,795)
04/2009
04/02/2009WO2009040102A1 Automatic control of a high lift system of an aircraft
04/02/2009WO2009013323A3 Aerodynamic profile, actuator for use therein and test model provided therewith
04/02/2009US20090084908 Minimizing dynamic structural loads of an aircraft
04/02/2009DE102007044642A1 Flugzeughochauftriebssystem Aircraft high lift system
04/02/2009CA2700435A1 Automatic control device of a high-lift system of an aircraft
04/01/2009EP2041453A2 Flap actuator
03/2009
03/31/2009US7510141 Autonomous control method for small unmanned helicopter
03/26/2009WO2008127854A4 Dynamic adjustment of wing surfaces for variable camber
03/25/2009EP2038613A1 Converter for converting a load factor command into a longitudinal attitude deviation instruction
03/24/2009US7509212 Enabling services on a UAV
03/24/2009US7506842 Aircraft control surface drive system and associated methods
03/18/2009EP2035275A1 Adjusting device for adjusting a high-lift flap and airfoil wing comprising such an adjusting device
03/18/2009EP2035271A1 Motor vehicle steering control
03/18/2009CN101389532A Electrical control system for an aircraft steering vane
03/12/2009WO2008137217A3 Vertical speed and flight path command algorithm for displacement collective utilizing tactile cueing and tactile feedback
03/12/2009US20090065648 Compensation actuator for a rotorcraft flight control
03/11/2009EP2033892A1 Flight control compensating actuator for an helicopter
03/11/2009EP2033059A2 Surface contact override landing scheme for a fbw rotary-wing aircraft
03/11/2009EP2032436A2 Wirelessly controlling unmanned aircraft and accessing associated surveillance data
03/10/2009US7501780 Docking system
03/10/2009CA2546390C Two-stage pressure relief valve
03/04/2009CN101378956A Rotor blade for a rotary wing aircraft
02/2009
02/26/2009WO2009023941A2 Aircraft flight control systems and methods
02/26/2009US20090050750 Airborne Manipulator System
02/26/2009US20090050748 Aircraft flight control systems and methods
02/26/2009US20090050747 Remote control model aircraft with laser tag shooting action
02/26/2009US20090050734 Flow control actuators
02/26/2009US20090049948 Device for artificially restoring an opposing force for a device for remotely controlling aircraft control surfaces
02/25/2009EP2027518A1 Method for piloting an aircraft in approach phase
02/19/2009US20090048723 Proactive optical wind shear protection and ride quality improvement system
02/19/2009US20090045296 Multi-mode unmanned and manned vehiclel systems and methods
02/18/2009EP2026158A2 Actuation response oscillation detection monitor
02/18/2009CN101370701A Long-range control system
02/12/2009WO2009020453A2 Control stick adapted for use in a fly-by-wire flight control system, and linkage for use therein
02/12/2009WO2009020452A1 Fault-tolerant actuator assembly, and method of moving a member relative to a support
02/12/2009WO2009000227A2 Rotor blade for a rotary wing aircraft
02/12/2009WO2008141792A4 Method and device for fault detection in the load path of a spindle actuator
02/12/2009WO2008127854A3 Dynamic adjustment of wing surfaces for variable camber
02/12/2009US20090039207 Flying object
02/12/2009US20090039205 Aircraft flight control user interface linkage system
02/12/2009CA2843614A1 Control stick adapted for use in a fly-by-wire flight control system, and linkage for use therein
02/12/2009CA2843578A1 Control stick adapted for use in a fly-by-wire flight control system, and linkage for use therein
02/12/2009CA2669919A1 Control stick adapted for use in a fly-by-wire flight control system, and linkage for use therein
02/11/2009EP2021239A1 Flying process and device of an aircraft optimizing the control of ailerons in a high-lift configuration
02/11/2009EP1781538B1 Aircraft flight control surface actuation system communication architecture
02/05/2009WO2009016361A2 Control device
02/05/2009WO2009016300A2 Advanced aircraft cockpit
02/05/2009DE102007030059A1 Verfahren zur Ansteuerung eines Antriebssystems und Antriebssystem Process for controlling a drive system and drive system
02/05/2009CA2692832A1 Advanced aircraft cockpit
01/2009
01/29/2009WO2009013322A1 Combined feed back control and feedforward control in order to actively reduce oscillations in aircraft
01/22/2009US20090021490 Display system
01/22/2009US20090020651 Method and device for piloting an aircraft about a piloting axis
01/22/2009DE202008015384U1 Vorrichtung für schaltbare Pilotensteuerkräfte Device for switchable pilot control forces
01/21/2009EP2016291A2 Ballistically tolerant linear hydraulic actuator
01/20/2009CA2392734C Multi-mode tiltrotor nacelle control system with integrated envelope protection
01/15/2009WO2009008761A1 Light multipurpose aircraft
01/15/2009WO2009008760A1 Aircraft with an integrated radioelectronic system
01/15/2009US20090014595 Electrical control system for an aircraft steering vane
01/14/2009CN101346276A Airfoil for an aircraft and aircraft
01/13/2009US7475848 Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance
01/08/2009US20090012659 Manual Human Interfaces to Electronics
01/08/2009US20090012657 Autonomous outer loop control of man-rated fly-by-wire aircraft
01/08/2009US20090008507 Aircraft wing
01/07/2009EP2012212A2 Flight control backup mode with separate set of inertial signals
01/06/2009US7474944 Control system and method with multiple linked inputs
01/01/2009US20090004004 Rotorcraft
12/2008
12/31/2008WO2009000731A1 Device and method for the temperature regulation of a hydraulic fluid
12/31/2008EP2008931A2 Method for controlling a drive system and drive system
12/31/2008CN101332872A Multipurpose composite power unmanned air vehicle
12/31/2008CA2663628A1 Device and method for the temperature regulation of a hydraulic fluid
12/29/2008CA2635064A1 Method for activating a drive system and drive system
12/25/2008US20080315040 Detection of effort on a flight-control actuator
12/24/2008EP2005559A1 Fault-tolerant electromechanical actuator having a torque sensing control system
12/24/2008EP2004482A1 Method and device for flying an aircraft along a flight path
12/24/2008DE102007028919A1 Vorrichtung und Verfahren zur Temperaturregelung eines Hydraulikfluids Device and method for temperature control of a hydraulic fluid
12/24/2008DE102007027137A1 Brake unit for drive system for landing e.g. airbrake of aircraft, has brake electrically or hydraulically operated for configuring and/or releasing drive element, and mechanically operated at same time for limiting torque
12/24/2008CN101331056A Method and device for providing automatic load alleviation to a high lift surface system, in particular to a landing flap system, of an aircraft
12/18/2008DE102007027698A1 Dualer Linear-Aktuator Dual linear actuator
12/17/2008EP1282554A4 Power lever tactile cueing system
12/16/2008US7464903 Methods and apparatus for vibration and buffet suppression
12/16/2008US7464896 Apparatus for the adjustment of horizontal stabilizers for aircraft
12/11/2008WO2008110384B1 Method and device for moveable tail trimming in an aircraft
12/10/2008EP2000405A1 Improved load detection on a flight control actuator
12/10/2008CN100441920C Compact actuator
12/09/2008US7463957 Method for operating an aircraft
12/09/2008US7461819 Method for using a steerable tall fin to reduce the vibration generated on the fuselage of a helicopter
12/09/2008US7461812 Rotorcraft control system with stepped mixing linkage
12/03/2008EP1996459A2 Multi-mode unmanned and manned vehicle systems and methods
12/03/2008EP1797487A4 Autonomous flight for flight platforms
12/02/2008US7458212 Back-pressure valve and actuation system
11/2008
11/27/2008WO2008141792A1 Method and device for fault detection in the load path of a spindle actuator
11/27/2008WO2007146538A3 Wirelessly controlling unmanned aircraft and accessing associated surveillance data
11/27/2008CA2687398A1 Method and device for fault detection in the load path of a spindle actuator
11/20/2008US20080283671 Engine anticipation for rotary-wing aircraft
11/20/2008DE102007023394A1 Verfahren und Einrichtung zur Fehlerdetektierung im Lastpfad eines Spindelaktuators Method and apparatus for error detection in the load path of a Spindelaktuators
11/18/2008US7451951 Miniature airplane apparatus and method
11/18/2008US7451949 Method for using a tiltable stabilizer to reduce vibration generated on the fuselage of a helicopter
11/13/2008WO2008137217A2 Vertical speed and flight path command algorithm for displacement collective utilizing tactile cueing and tactile feedback
11/13/2008US20080277526 Aircraft Cooling Duct
11/13/2008DE102007021748A1 Antriebssystem für einen wölbvariablen Flugzeugflügel Drive system for an aircraft wing wölbvariablen
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