Patents
Patents for B64C 13 - Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers (4,795)
07/2001
07/10/2001US6259976 Fuzzy logic based emergency flight control with thrust vectoring
07/10/2001US6259223 Method and apparatus for phase compensation in a vehicle control system
07/10/2001US6257529 Servo actuator apparatus and aircraft control apparatus
07/05/2001WO2001048573A1 Aircraft flight mode selector system
07/05/2001WO2000016464A9 Control system with integrated actuation package
07/05/2001DE19960288A1 Device to support control stick operation for vehicle; has force-applying element in working train of control stick and mechanically connected to aileron to apply additional force
07/05/2001CA2395322A1 Aircraft flight mode selector system
07/03/2001US6254037 Variable gradient control stick force feel adjustment system
06/2001
06/26/2001US6253126 Method and apparatus for flight parameter monitoring and control
06/26/2001US6250589 Apparatus for locking control surfaces of stick controlled aircraft
06/21/2001WO2001044881A1 Systems and methods for fail safe process execution, monitoring and output control for critical systems
06/21/2001CA2395071A1 Systems and methods for fail safe process execution, monitoring and output control for critical systems
06/12/2001CA2040874C System for piloting a pitching aircraft
06/07/2001US20010002687 Manual override device, in particular for aircraft flight control
06/06/2001EP1104740A1 Manual override device, in particular for aircraft flight control
06/05/2001US6242878 Electronic control apparatus
06/05/2001US6241183 Method for controlling an aeroplane control surfaces to counter ground lateral drift
06/05/2001US6241182 Hybrid control system for an aircraft aerodynamic surface
05/2001
05/30/2001CN1066405C Process and device for control of rudder of aircraft
05/29/2001US6237433 Electromechanical actuator of the type having a screw-and-nut system
05/23/2001EP1101981A2 Hydraulic motor control system
05/23/2001DE10037318A1 Mechanism to operate drainage device for aeroplane toilet; has independent cables with hand lever to operate mechanism from floor and engagement lever to operated mechanism from passenger cabin
05/15/2001US6231012 No-back/offset gear box
05/10/2001DE19953388A1 Aircraft rudder pedal with an orthopaedic foot holder for disabled pilots
05/10/2001DE19952524A1 Cooling of food and drinks wagons in passenger aircraft is supplied from the cabin air conditioning compressor system into which the heated return air is returned
05/09/2001EP1097500A2 Control system with integrated actuation package
05/01/2001US6224022 Airplane high lift surface drive system
05/01/2001US6224017 Brake for a lift flap adjustment mechanism
04/2001
04/24/2001US6222306 Actuators of active piezoelectric or electrostrictive material
04/24/2001US6220550 Actuating device with multiple stable positions
04/19/2001WO2001026965A1 A hinge for movable control surfaces in an aircraft and a connecting piece to be used with such a hinge
04/19/2001CA2387166A1 A hinge for movable control surfaces in an aircraft and a connecting piece to be used with such a hinge
04/11/2001EP1090835A1 Surface actuator for deforming an elastic plate structure
04/11/2001EP1090232A1 Actuator system for aerospace controls and functions
04/10/2001US6215221 Electrostatic/pneumatic actuators for active surfaces
04/10/2001US6212920 Anti-theft device for aircraft
04/05/2001DE10043253A1 Mechanism for initiating correction variable in adjusting device has multi-lever mechanism with non-linear transmission ratio which tends towards zero in end positions and in middle position assumes final adjusting value
04/04/2001EP1088753A2 Skew detection system
04/03/2001US6209825 Low power loss electro hydraulic actuator
03/2001
03/27/2001US6206329 Process and device for the control of the rudder of an aircraft
03/22/2001WO2001019673A1 Improvements to convertible aircraft with tilting rotors
03/22/2001CA2382879A1 Improvements to convertible aircraft with tilting rotors
03/13/2001US6202007 Exact stability integration in network designs
03/08/2001WO2000059780A3 Flywheel peaking unit for an aircraft hydraulic system
02/2001
02/28/2001EP1078308A2 Navigation of helicopter with limited polar groundspeed commands
02/20/2001US6189837 Auxiliary spoiler retract system
02/15/2001WO2001011439A1 Hydrostatic sidestick coupling
02/15/2001WO2001010711A1 Variable gradient control stick force feel adjustment system
02/15/2001CA2381382A1 Hydrostatic sidestick coupling
02/08/2001WO2001008971A1 Actuator system for aerospace controls and functions
01/2001
01/31/2001EP1072507A1 Failsafe arrangement
01/30/2001US6178829 Redundant linkage and sensor assembly
01/30/2001US6178788 Anti-theft device for aircraft
01/18/2001DE19930559A1 Arrangement for protecting an aircraft fuselage
01/17/2001EP1069397A1 Displacement sensor for servo-controlled jacks
01/17/2001EP0898661A4 No-back/offset gear box
01/11/2001WO2001002233A1 Steering mechanism for a vehicle
01/09/2001US6173219 Method for automatically controlling a vehicle for the lateral avoidance of a fixed zone
01/09/2001US6170525 Opto-electric/hydraulic servoactuation
01/09/2001CA2055089C Integrated elevator and thrust control system for aircraft
01/03/2001EP1065487A2 Redundant linkage and sensor assembly
01/02/2001US6168117 Flight control system for airplane
12/2000
12/28/2000DE19927372A1 Verfahren und Vorrichtung zum Erkennen einer Fehlfunktion von Stellantrieben Method and apparatus for detecting a malfunction of actuators
12/21/2000WO2000077589A1 Device for controlling an apparatus
12/20/2000EP1061269A2 Method and device for detecting faulty operation of a positioning drive
12/19/2000US6161801 Method of reducing wind gust loads acting on an aircraft
12/14/2000DE19926784A1 Vorrichtung zum Steuern einer Einrichtung An apparatus for controlling a device
12/13/2000EP0606469B1 Aircraft flight control system
12/13/2000CN1059394C Motor-driven system for steering vehicle
12/12/2000US6161063 Method for controlling an aerodyne for the vertical avoidance of a zone
12/12/2000US6158695 Method of speed protection and flare compensation for use with aircraft pitch control system
12/05/2000US6155450 Composite shell shaped as a body of revolution
11/2000
11/23/2000WO2000070242A1 Dual load path ball screw with rod end swivel
11/21/2000US6149527 Apparatus for imparting rotary motion through a flex point
11/21/2000US6149513 Ceiling grille for air conditioner of recreational vehicle
11/21/2000US6149105 Deployment mechanisms for aircraft auxiliary airfoils
11/07/2000US6144899 Recoverable airborne instrument platform
11/07/2000US6142413 Device for control of an aerodynamic steering surface of a helicopter
11/02/2000WO2000064736A1 Unmanned aerial vehicle with counter-rotating ducted rotors and shrouded pusher-prop
10/2000
10/31/2000US6140942 Aircraft surface contamination sensing system using control surface hinge moment measurements
10/31/2000US6138956 Aerofoil profile with variable profile adaptation
10/31/2000US6138787 Motor-driven system for steering a vehicle
10/12/2000WO2000059780A2 Flywheel peaking unit for an aircraft hydraulic system
10/11/2000EP1043226A2 Control apparatus equipped with back drive
10/11/2000EP1042707A1 Compensation for rotorcraft pitch axis control saturation
10/11/2000EP1042166A1 Arrangement and method for regulating the steering force in a mechanical steering system for an aircraft
09/2000
09/27/2000EP1038765A1 Airplane high lift surface drive system
09/26/2000US6123291 Device for controlling an aerodynamic surface for balancing a helicopter in terms of pitch
09/20/2000EP1036734A2 Servo actuator apparatus and aircraft control apparatus
09/12/2000US6116065 Anti-theft device for aircraft
08/2000
08/29/2000US6109852 Soft actuators and artificial muscles
08/29/2000US6109415 Bi-directional ballscrew no-back device
08/23/2000EP1028890A1 Method for compensating structural variations in an airplane that are due to external disturbances
08/23/2000CN1264463A GPS guided munition
08/16/2000EP1027633A1 Method and apparatus for phase compensation in a vehicle control system
08/10/2000WO2000046573A1 Apparatus with gyroscopes and accelerometers for determining the attitudes of an aerodyne
08/10/2000DE10004605A1 Hydraulik-Logik-Kreuzkopplung zwischen getrennten Redundanten Servoaktuatoren Hydraulic logic crosstalk between separate redundant servo actuators
08/10/2000DE10001378A1 Radio-controlled helicopter has wobble plate contg. 3 control points, associated with servo devices, at corners of equilateral triangular base, movable point at centre of triangle height
08/10/2000CA2361727A1 Apparatus with gyroscopes and accelerometers for determining the attitudes of an aerodyne
08/09/2000EP1026565A1 Yaw control system for an aircraft
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