Patents
Patents for B64C 13 - Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers (4,795)
09/2006
09/05/2006US7101297 Compact actuator
09/05/2006US7100870 Jam tolerant electromechanical actuation systems and methods of operation
08/2006
08/31/2006DE102005008331A1 Shaft`s rotation angle determining device for use in aircraft, has motor detecting primary rotation data, and position pick up unit detecting secondary rotation data, where synchronization unit synchronizes both data
08/29/2006US7098811 Method and apparatus for tactile cueing of aircraft controls
08/29/2006CA2269022C Bi-directional ballscrew no-back device
08/24/2006WO2006088488A2 Dual motor dual concentric valve
08/24/2006US20060186262 Rotorcraft control system with stepped mixing linkage
08/24/2006DE102005008556A1 Aircraft controlling device, has decision unit provided to decide execution of security-critical control function on microcomputers and/or control units due to comparison of output data of microcomputers
08/23/2006EP1692038A2 Wing gull integration for nacelle clearance, compact landing gear stowage, and sonic boom reduction
08/22/2006US7093793 Variable cam exhaust nozzle
08/17/2006WO2006086005A2 System and method for remote control of interdiction aircraft
08/17/2006WO2006018027A3 A remote control system
08/17/2006WO2005124192B1 Compact actuator
08/17/2006US20060180708 R/C cockpit
08/15/2006US7090172 Process for countering the vibrations induced in an aircraft by the windmilling of a fan and system of electric flight controls implementing this process
08/10/2006DE10360873B4 Verfahren zum Betreiben eines Terminals, Terminal und Datenbussystem A method of operating a terminal, the terminal and data bus system
08/08/2006CA2183614C Active hand controller redundancy and architecture
08/03/2006US20060169837 Flexible actuator with integral control circuitry and sensors
08/03/2006DE102004035921B4 Klappen-Kopplungssystem für Luftfahrzeuge Flap coupling system for aircraft
07/2006
07/25/2006US7081062 Standardized rotary actuator
07/25/2006CA2272435C No-back brake
07/20/2006WO2006076018A2 Unitized rotary actuator hinge fitting
07/20/2006US20060157618 Blade gearing structure of air duct of vehicles
07/19/2006EP1590717B1 Device for controlling a vehicle
07/12/2006EP0965048A4 On-the-fly accuracy enhancement for civil gps receivers
07/06/2006US20060144996 Apparatus for the adjustment of horizontal stabilizers for aircraft
07/06/2006US20060144995 Remotely controlled model airplane having deflectable centrally biased control surface
07/05/2006EP1677011A1 Actuator safety attachment device
07/04/2006US7070146 Aircraft thickness/camber control device for low sonic boom
06/2006
06/29/2006US20060137596 Indicator device
06/22/2006US20060132079 Self-traveling cleaning robot
06/14/2006EP1669624A1 Indicator device and freewheel mechanism with such a device
06/14/2006EP1601571B1 Device for steering a vehicle
06/14/2006EP1545971A4 Self-centering steering module
06/13/2006US7059563 Systems, apparatuses, and methods for moving aircraft control surfaces
06/07/2006EP1663778A2 Variable cam exhaust nozzle
06/06/2006US7055782 Cellular actuator device and methods of making and using same
06/01/2006WO2006032486B1 Aircraft with wings whose maximum lift can be altered by controllable wing components
06/01/2006WO2005124192A3 Compact actuator
06/01/2006WO2005079460A8 Linkage and sensor assembly
06/01/2006US20060113933 Fault-tolerant electromechanical actuator having a torque sensing control system
05/2006
05/30/2006US7053528 Torsion element and torsion actuator
05/30/2006US7051975 Aircraft flap or slat drive system with redundant drives and shaft drive lines
05/24/2006EP1658441A2 Regulated pressure supply for a variable-displacement reversible hydraulic motor
05/23/2006US7048234 Adaptive flap and slat drive system for aircraft
05/18/2006US20060102798 Unmanned biplane for airborne reconnaissance and surveillance having staggered and gapped wings
05/11/2006WO2006048519A1 Method and device for enhancing the braking efficiency of an aircraft during the ground run thereof
05/11/2006WO2006004570A3 Forward pivoted full flying control tail boom
05/09/2006US7040571 Single pull control horn
04/2006
04/27/2006US20060087273 Robot cleaner system and a method for returning to external recharging apparatus
04/20/2006WO2006004570B1 Forward pivoted full flying control tail boom
04/20/2006DE10343088B4 Verfahren zur Überprüfung eines Ventilblocks für einen Verbraucher mit zwei hydraulischen Versorgungssystemen Method for checking a valve block for a consumer with two hydraulic supply systems
04/20/2006DE10156733B4 Aerodynamisches Profil mit verstellbarer Klappe An airfoil with adjustable flap
04/19/2006EP0993588B1 Gps guided munition
04/18/2006US7031811 Fuel efficient airspeed trim
04/18/2006US7028602 Linear, hydraulic pivot drive
04/13/2006DE102004044961A1 Vorrichtung zur Erfassung von Gleichlauffehlern von Hochauftriebsflächen an Flugzeugen Device for detecting synchronism errors of high lift surfaces on aircraft
04/12/2006EP1645780A2 Screw Actuator
04/12/2006EP1645505A2 Unmanned helicopter, takeoff method of unmanned helicopter, and landing method of unmanned helicopter
04/06/2006WO2006035429A2 Autonomous flight for flight platforms
04/06/2006US20060071817 Tactile cueing system and method for aiding a helicopter pilot in making landings
04/06/2006US20060071123 Automatic control systems for aircraft auxiliary power units, and associated methods
04/06/2006US20060070827 Screw actuator
04/06/2006DE10043253B4 Mechanismus zur Einleitung einer Stellgröße in eine vorzugsweise in einem Flugzeug angeordnete Verstellvorrichtung Mechanism for initiating a control variable in a preferably disposed in a plane adjustment
04/06/2006CA2580776A1 Autonomous flight for flight platforms
04/05/2006EP1642181A2 System and method for controlling model aircraft
04/04/2006US7024309 Autonomous station keeping system for formation flight
03/2006
03/30/2006WO2006032486A1 Aircraft with wings whose maximum lift can be altered by controllable wing components
03/30/2006WO2006023982A8 Aircraft flight control surface actuation system communication architecture
03/30/2006US20060068960 Drive assemblies
03/30/2006US20060065778 Actuator with helical cam guides
03/30/2006DE102004047008A1 Vorrichtung zur Einstellung von Flugzeughöhenflossen Device for adjusting aircraft HSS
03/30/2006DE102004045732A1 Airplane with aerofoil for reducing loading of structure of airplane has detectors and control or regulating device whereby detectors measure actual momentary surface loading of aerofoil during flight
03/30/2006CA2573606A1 Aircraft with wings whose maximum lift can be altered by controllable wing components
03/29/2006EP1640265A1 Horizontal stabilizer trim device
03/29/2006EP1185454B1 Device for controlling an engine
03/28/2006US7017861 Control system for actuators in an aircraft
03/23/2006WO2006029988A1 No-back device having malfunction detection
03/23/2006US20060060719 An aeronautical high-lift system with an overload safety device
03/23/2006US20060060694 Autonomous control method for small unmanned helicopter
03/21/2006US7014141 Unmanned airborne reconnaissance system
03/16/2006CA2520064A1 Device for detecting synchronous errors of high-lift surfaces on aircraft
03/09/2006WO2006024745A1 Electric flight control system for aircraft elevators
03/09/2006US20060049308 Systems and methods for providing differential motion to wing high lift devices
03/09/2006US20060049307 Flow-mechanically effective surface for minimizing induced resistance
03/09/2006DE10249967B4 Vorrichtung zur Ansteuerung der Vorflügel und Landeklappen eines Flugzeuges Device for controlling the slats and flaps of an aircraft
03/09/2006CA2567209A1 Electric flight control system for aircraft elevators
03/07/2006US7010398 Control system providing perspective flight guidance
03/07/2006US7007897 Flight control actuation system
03/02/2006WO2006023982A1 Aircraft flight control surface actuation system communication architecture
03/02/2006WO2005079460A3 Linkage and sensor assembly
03/02/2006US20060043242 Aircraft flight control surface actuation system communication architecture
03/02/2006DE102005039649A1 Flugzeugflügel Aircraft wing
03/01/2006EP1332547B1 Electrostatic/pneumatic actuators for active surfaces
03/01/2006CN1742175A Standardized rotary actuator
02/2006
02/28/2006US7003949 Integrated three function valve
02/23/2006US20060038089 Hang glider wheel apparatus
02/16/2006US20060032975 Method of control for toy aircraft
02/16/2006DE102004035921A1 Klappen-Kopplungssystem für Luftfahrzeuge Flap coupling system for aircraft
02/16/2006CA2568848A1 Method and device for improving maneuverability of an aircraft during approach phases before landing followed by flare-out
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