Patents
Patents for B64C 13 - Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers (4,795)
08/2005
08/04/2005US20050171652 Vehicle control systems and corresponding sizing methods
08/04/2005DE10361891A1 Vorrichtung zur Ansteuerung und Verstellung von Klappen an Flugzeugtragflächen Device for controlling and adjustment of flaps on aircraft wings
08/02/2005US6925382 Remote image management system (RIMS)
08/02/2005US6923405 Enhanced rudder control system
08/02/2005US6922991 Regulated pressure supply for a variable-displacement reversible hydraulic motor
07/2005
07/28/2005WO2005069095A1 Bilatral servo controller
07/28/2005DE10360873A1 Datenbussystem Data bus system
07/27/2005EP1557588A1 Load transfer detection device through breakable shear pin
07/27/2005EP1557353A1 Actuator device comprising autonomous means for blocking the drive chains
07/26/2005US6921045 Supersonic aircraft with channel relief control
07/21/2005US20050157710 Data bus system
07/14/2005WO2005062743A2 Supersonic aircraft with aerodynamic tail structure
07/14/2005US20050151672 Method and apparatus for tactile cueing of aircraft controls
07/14/2005US20050151028 Apparatus for driving and adjusting flaps hinged to an aircraft
07/14/2005US20050151027 Adaptive flap and slat drive system for aircraft
07/14/2005US20050151023 Control system for model aircraft
07/13/2005EP1392561B1 Apparatus and method for verifying the dynamic stiffness capability of hydraulic servo actuators
07/13/2005CN1639500A 飞行器 Aircraft
07/12/2005US6915989 Aircraft multi-axis modal suppression system
07/06/2005EP1550607A1 Mechanism for eliminating limit cycle oscillations on servocontrolled aerodynamic control surfaces
07/05/2005US6913226 Methods and systems for redundant control and/or failure detection
07/05/2005CA2148393C Cargo plane with front empennage
06/2005
06/29/2005EP1548992A1 System for maintaining error-free communication in a data bus
06/29/2005EP1547917A1 Aircraft wing flap control system
06/29/2005EP1545971A1 Self-centering steering module
06/23/2005US20050132877 Redundant flow control for hydraulic actuator systems
06/22/2005EP1544100A1 Method for reducing the aerodynamic forces on an elevator of an aircraft during takeoff
06/22/2005EP1542901A2 Rotorcraft control system with stepped mixing linkage
06/16/2005US20050127241 Flight control actuation system
06/16/2005DE10351839B3 Verfahren zur Minimierung des Widerstands bei einem im Flug befindlichen Flugzeug A method for minimizing the resistance in an airplane in flight
06/15/2005EP1423306B1 Joystick
06/14/2005CA2299303C Method and apparatus for phase compensation in a vehicle control system
06/02/2005WO2005050062A1 A linear ballscrew actuator with a safety unlocking device
06/02/2005WO2005003324A3 Improved vertical take-off and landing vehicles
06/02/2005US20050119828 Remote image management system (rims)
06/02/2005US20050116116 Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance
06/02/2005US20050116095 Enhanced rudder control system
05/2005
05/26/2005US20050109876 Aircraft control surface drive system and associated methods
05/24/2005CA2221336C Cam and roller overcenter handle mechanism
05/19/2005WO2005044660A2 Wing gull integration for nacelle clearance, compact landing gear stowage, and sonic boom reduction
05/19/2005WO2005044622A2 Method and apparatus for loss of control inhibitor systems
05/19/2005US20050103943 Laser-tethered vehicle
05/19/2005US20050103933 Variable cam exhaust nozzle
05/19/2005US20050103932 Methods and systems for redundant control and/or failure detection
05/19/2005US20050103929 Supersonic aircraft with channel relief control
05/19/2005US20050103928 Jam tolerant electromechanical actuation systems and methods of operation
05/18/2005EP1531126A1 Wing tip device
05/06/2005WO2005044661A2 Supersonic aircraft with aerodynamic control
05/04/2005EP1528449A1 Device for controlling an apparatus
05/04/2005EP1528448A1 Aircraft multi-axis modal suppression system
05/04/2005EP1527268A1 Thrust reverser system with a pass-through torque activated brake
04/2005
04/27/2005EP1526416A2 Method, apparatus and design procedure for controlling multi-input, multi-output (MIMO) parameter dependent systems using feedback LTI zation
04/21/2005US20050085957 Method and apparatus for obtaining high integrity and availability in multi-channel systems
04/20/2005EP1524188A2 Jam tolerant electromechanical actuation systems and methods of operation
04/14/2005US20050080495 Apparatus and method for controlling a force-activated controller
04/07/2005US20050075763 Method and device for automatically monitoring and controlling an aircraft path
04/07/2005US20050075761 Method for operating an aircraft
04/07/2005US20050072553 Gen set with external oil filter and pump
04/06/2005EP1520234A2 Method and system for controlling ergonomic settings at a worksite
04/05/2005US6875145 Rotary actuator
03/2005
03/31/2005US20050067525 Aircraft thickness/camber control device for low sonic boom
03/30/2005EP1290508B1 Method, apparatus and design procedure for controlling multi-input, multi-output (mimo) parameter dependent systems using feedback lti'zation
03/29/2005US6871816 Proactive optical trajectory following system
03/24/2005US20050065672 Method and device for controlling the attitude of an aircraft
03/24/2005US20050061912 "Dream of life" - system which gurantee safety flights for all type aircrafts
03/24/2005US20050061910 Aircraft
03/22/2005US6871123 System and method allowing for an integrated flight loads balancing process
03/17/2005WO2005024273A1 Apparatus for releasing a jam in a lead screw actuator
03/17/2005WO2005024184A2 Variable cam exhaust nozzle
03/17/2005WO2003102437A8 Actuator with two motors, a differential reducer and a torque limiter
03/17/2005US20050056730 Automatic pilot apparatus
03/17/2005DE10234738B4 Aktuator Actuator
03/17/2005CA2536802A1 Variable cam exhaust nozzle
03/16/2005EP1274944B1 Electrohydraulic setting device
03/16/2005EP1157254B1 Apparatus with gyroscopes and accelerometers for determining the attitudes of an aerodyne
03/16/2005CN1594033A Flying disk type aircraft
03/10/2005WO2005021970A2 Regulated pressure supply for a variable-displacement reversible hydraulic motor
03/10/2005US20050055143 Autonomous station keeping system for formation flight
03/10/2005US20050051671 Non-jamming, fail safe flight control system with non-symmetric load alleviation capability
03/08/2005US6863242 Method and system for controlling an aircraft control surface
03/03/2005US20050045764 Canard position and dihedral for boom reduction and pitch/directional control
03/03/2005US20050045761 Proactive optical trajectory following system
03/03/2005US20050045028 Regulated pressure supply for a variable-displacement reversible hydraulic motor
03/03/2005US20050044984 Reinforced tension and compression reacting strut and method of making same
03/02/2005EP1510455A1 Method and device for controlling the pitch angle of an aircraft
03/02/2005EP1509705A1 Actuator with two motors, a differential reducer and a torque limiter
03/02/2005EP1244947B1 Aircraft flight mode selection method
03/01/2005US6860452 Aircraft flight surface control system
02/2005
02/26/2005CA2472316A1 Process and device used to control the attitude of an aircraft
02/24/2005US20050040283 Method of propulsion and attitude control in fluid environments and vehicles utilizing said method
02/22/2005US6859689 Method, apparatus and design procedure for controlling multi-input, multi-output (MIMO) parameter dependent systems using feedback LTI'zation
02/22/2005US6857597 Control system for vertical take off and land (VTOL) aircraft
02/17/2005WO2003029922A3 Pfn/trac system faa upgrades for accountable remote and robotics control
02/17/2005US20050035242 Proactive optical trajectory following system
02/10/2005WO2005002963A3 Actuator and flap arrangement with actuator interconnection
02/10/2005WO2004108524A3 System and method for controlling model aircraft
02/10/2005US20050029407 Aircraft flap or slat drive system with redundant drives and shaft drive lines
02/10/2005US20050029406 Cellular actuator device and methods of making and using same
02/10/2005DE10336219A1 Hydraulic rotary motor to operate steering control surface has vane motor fitted with two-vane rotor to which control surface is mechanically attached
02/09/2005EP1504195A1 Integrated three function valve
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