Patents
Patents for B64C 13 - Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers (4,795)
01/2008
01/16/2008EP1878658A2 Aircraft stabilizer actuator
01/16/2008EP1786668B1 No-back device having malfunction detection
01/10/2008WO2008005659A2 Robotic follow system and method
01/10/2008WO2008003591A1 Converter for converting a load factor command into a longitudinal attitude deviation instruction
01/10/2008US20080006737 Aircraft
01/09/2008CN201002720Y Electric helm system gear
01/09/2008CN101101047A Constant-speed differential speed double-axis reverse output transmission method and device
01/08/2008US7316373 Disengage device for aircraft control
01/03/2008WO2008001336A1 Adjusting device for adjusting a high-lift flap and airfoil wing comprising such an adjusting device
01/03/2008WO2007056294A3 A method and means for piloting control of a forward-moving vehicle
01/03/2008US20080001037 Actuator link assembly, flight control system and method of making same
01/03/2008US20080001030 Method of controlling aerodynamic characteristics of spiked flying object, and spiked flying object
01/03/2008US20080001029 Fitting with torsion box, of plastic material reinforced with carbon fibre, for coupling a drive motor / spindle unit for trimming of a horizontal stabiliser of an aircraft
01/03/2008US20080001028 Aircraft control system
01/03/2008US20080000730 No-Back Device Having Malfunction Detection
01/03/2008CA2656442A1 Adjusting device for adjusting a high-lift flap and airfoil wing comprising such an adjusting device
01/02/2008EP1873057A1 Active rudder pedal mechanism with foreign object strike tolerance and articulating brake
12/2007
12/27/2007WO2007042652A8 Method and device for attenuating on an aircraft the effects of a vertical turbulence
12/27/2007DE102006027894A1 Reduction device for hydraulic fluid vibrations in hydraulic system, particularly hydraulic system of plane, includes jet way, which is formed between pipe and inner wall of hose cable and another jet way is formed in interior of pipe
12/26/2007EP1868889A1 Local backup hydraulic actuator for aircraft control systems
12/26/2007EP1868888A1 Landing flap drive system
12/26/2007EP1753979A4 Compact actuator
12/21/2007WO2007144485A1 Method for piloting an aircraft in approach phase
12/21/2007CA2654863A1 Wirelessly controlling unmanned aircraft and accessing associated surveillance data
12/21/2007CA2653638A1 Method for piloting an aircraft in approach phase
12/18/2007US7308762 Method and apparatus for rotatably supporting movable components, including canards
12/18/2007CA2185299C Process and device for the control of the rudder of an aircraft
12/12/2007EP1865590A1 Actuator arrangement
12/12/2007EP1545971B1 Self-centering steering module and method
12/06/2007WO2007138179A1 Flying process and device of an aircraft optimizing the control of ailerons in a high-lift configuration
12/06/2007US20070277625 Linkage and sensor assembly
12/06/2007DE10205071B4 Sperrmechanismus für eine Kugelumlaufspindel-Betätigungsvorrichtung Locking mechanism for a ball screw actuator
12/06/2007DE102006025388A1 Leitungssystemanordnung in einem einen Rumpf aufweisenden Luft- oder Raumfahrzeug Piping arrangement in a hull having an aircraft or spacecraft
12/06/2007CA2647478A1 Flying process and device of an aircraft optimizing the control of ailerons in a high-lift configuration
12/05/2007EP1776625B1 Electric flight control system for aircraft elevators
12/04/2007USH2206 Tactile side-slip corrective yaw control for aircraft
12/04/2007CA2479142C Helicopter tactile exceedance warning system
11/2007
11/22/2007US20070267548 Flight control systems
11/22/2007US20070267541 Pivoting coupling system for a large dihedral empennage to the tail fuselage of an aircraft
11/22/2007DE102004029196B4 System zur Rumpfstrukturlastabminderung in Verkehrsmitteln System for Rumpfstrukturlastabminderung in transport
11/20/2007US7296487 Linkage and sensor assembly
11/15/2007WO2005044622A3 Method and apparatus for loss of control inhibitor systems
11/15/2007US20070262207 Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance
11/15/2007US20070262197 Ultralight coaxial rotor aircraft
11/15/2007DE102006020554A1 Verbindungsstrebe zur Anordnung zwischen benachbarten Landeklappen eines Flugzeuges Connecting strut for arrangement between adjacent flaps of an aircraft
11/14/2007EP1854717A1 Apparatus and method for reducing the impact of turbulence and gusts on aircraft
11/14/2007EP1520234A4 Method and system for controlling ergonomic settings at a worksite
11/13/2007US7293524 Indicator device for indicating whether a no-back device is operable
11/07/2007EP1773655B1 Device for antagonistic artificial force gradient for an aircraft control surface remote control device
11/07/2007EP1768900B1 Device for remote control of an aircraft control surfaces
11/06/2007US7290738 Dual jet emerging lift augmentation system for airfoils and hydrofoils
11/01/2007US20070252046 Bias correcting phase compensating rate limiter
11/01/2007US20070252035 Unmanned vehicle
11/01/2007US20070252029 Electronics for manned or unmanned vehicles
10/2007
10/31/2007EP1521951B1 Apparatus for monitoring an aircraft flap and application of a dynamometric rod
10/31/2007DE4436356B4 Verfahren zur Flugweggenerierung Method for Flugweggenerierung
10/25/2007US20070247101 Actuator driving device
10/25/2007US20070246610 Avionics framework
10/25/2007US20070246605 Electric Flight Control System for Aircraft Elevators
10/24/2007EP1846291A2 Dual motor dual concentric valve
10/23/2007US7285933 Method and apparatus for loss of control inhibitor systems
10/23/2007US7285932 Method and apparatus for loss of control inhibitor systems
10/18/2007WO2007116134A1 Method and device for flying an aircraft along a flight path
10/18/2007DE202007010518U1 Kombinierte Rückführ- und Vorsteuerreglerregelung zur aktiven Verminderung von Schwingungen bei Luftfahrzeugen Combined return and pilot regulator system for active reduction of vibrations on aircraft
10/18/2007CA2643974A1 Method and device for flying an aircraft along a flight path
10/17/2007EP1248725B1 Method of manufacturing a stacked stator assembly for a linear motor
10/17/2007CN100343120C 飞行器 Aircraft
10/16/2007US7281683 Process for aiding the takeoff of an aircraft
10/16/2007CA2380346C Variable gradient control stick force feel adjustment system
10/11/2007US20070235594 Pilot flight control stick feedback system
10/11/2007US20070235593 Flying control device for a rotorcraft
10/11/2007US20070235584 Unmanned air vehicle interoperability agent
10/11/2007DE102005020660B4 Verfahren zur Reduzierung der Turbulenz- und Böeneinflüsse auf das Flugverhalten von Luftfahrzeugen und Steuerungseinrichtung hierfür Method for reducing the turbulence and gusts influences on the flight behavior of aircraft and control means therefor
10/10/2007CN101052564A Method and device for improving braking efficient of air vehicle running on the ground
10/04/2007US20070228221 Autonomous Flight for Flight Platforms
10/03/2007EP1419088B1 Path guidance systems for a parachute/paraglider and flight path planning devices for planning the use of at least one parachute or paraglider, and system for carrying out said path guidance and planning
09/2007
09/27/2007US20070221782 Multi-mode unmanned and manned vehicle systems and methods
09/27/2007DE102006012986A1 Betätigungsvorrichtung Actuator
09/26/2007EP1835835A2 Control system for automatic flight and windshear conditions
09/25/2007CA2451099C Hydraulic circuit architecture
09/25/2007CA2293166C Command process and system for an aircraft control surface with multiple hydraulic power control units and modular power
09/25/2007CA2277044C Method for controlling an aeroplane control surfaces to counter ground lateral drift
09/25/2007CA2257336C Method for the lateral avoidance of a mobile zone by a vehicle
09/19/2007EP1835181A2 Reservoir built-in type actuator
09/18/2007US7272470 Path guidance systems for a parachute/paraglider and flight path planning devices for planning the use of at least one parachute or paraglider, and system for carrying out said path guidance and planning
09/11/2007CA2487950C Actuator with two motors, a differential reducer and a torque limiter
09/05/2007EP1404978B1 Hydraulic circuit for an aircraft brake system
09/04/2007US7264201 Process for reducing the aerodynamic loads applied to the elevators of an aircraft during takeoff
08/2007
08/30/2007WO2007096507A1 Electrical control system for an aircraft steering vane
08/30/2007CA2640521A1 electrical control system for an aircraft steering vane
08/28/2007US7263630 Fault tolerant computer controlled system
08/28/2007US7263414 Method and device for controlling the attitude of an aircraft
08/28/2007US7262712 Helicopter tactile exceedance warning system
08/23/2007US20070193381 Screw actuator having means for blocking it in the event that it goes over to the secondary nut
08/21/2007US7260455 System for operating an aircraft
08/16/2007WO2007074173A3 Airfoil for an aircraft and aircraft
08/14/2007US7255306 Method and computer program product for controlling the control effectors of an aerodynamic vehicle
08/14/2007US7254945 Operate check valve and hydraulic driving unit
08/02/2007WO2007068413A3 Method and device for providing automatic load alleviation to a high lift surface system, in particular to a landing flap system, of an aircraft
07/2007
07/31/2007US7249735 Translating conduit apparatus for an airplane or equipment
1 ... 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 ... 48