B64C 13 - Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers

Patents for B64C 13 - Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers (4,795)
12/2009
12/09/2009	CN101600623A Jack with integrated locking device
12/09/2009	CN100568141C Unmanned machine rolling leveling control method
12/09/2009	CN100568138C Small-sized unmanned aircraft steering engine control device
12/08/2009	CA2498939C Self-centering steering module
12/03/2009	WO2009144312A1 System and method for determining characteristic parameters in an aircraft
12/03/2009	DE102008034444A1 Eingabesystem für eine Landeklappensteuerung eines Flugzeugs Input system for a landing flap control of an aircraft
12/02/2009	EP2128021A1 Retractable coupling device and associated trim cylinder
12/02/2009	EP2021239B1 Flying process and device of an aircraft optimizing the control of ailerons in a high-lift configuration
12/02/2009	CN201354145Y Course steering circuit of coaxial unmanned helicopter
12/02/2009	CN101595029A Jam-tolerant redundant differential-type actuators
12/02/2009	CN101590909A Force synthesizing arm applied to redundant actuator system
11/2009
11/27/2009	CA2666889A1 System and method for multiple aircraft lifting a common payload
11/26/2009	US20090292405 Wing-body load alleviation for aircraft
11/26/2009	US20090289145 Electromechanical actuating assembly
11/26/2009	CA2632347A1 Control device
11/25/2009	EP2123555A2 Directional control arrangement to provide stabilizing feedback to a structural bending mode
11/25/2009	EP2121435A1 Jack with integrated locking device
11/25/2009	CN101585411A Hydraulic servo steering engine system
11/19/2009	WO2009138251A1 Control system for a hydraulically actuatable horizontal stabilizer and test method for testing the integrity of a control system
11/19/2009	US20090283628 Directional control arrangement to provide stabilizing feedback to a structural bending mode
11/19/2009	DE102008023628A1 Stellsystem für eine hydraulisch betätigbare Höhenflosse und Testverfahren zur Überprüfung der Integrität eines Stellsystems Positioning system for a hydraulically actuated stabilizer and test procedures to verify the integrity of a parking system
11/19/2009	DE102008022092A1 Fehlertolerantes Stellsystem zur Verstellung von Klappen eines Flugzeugs mit einer Verstell-Kinematik mit feststehender Drehachse A fault-tolerant adjustment system for adjusting flaps of an aircraft to an adjustable linkage with fixed axis of rotation
11/19/2009	CA2724405A1 Control system for a hydraulically actuatable horizontal stabilizer and test method for testing the integrity of a control system
11/18/2009	EP2119626A1 Control lever assembly for a tilt-rotor aircraft
11/12/2009	WO2009135653A1 Error tolerant adjustment system for adjusting servo tabs of an aircraft, comprising a control mechanism with a fixed rotational axis
11/12/2009	CA2723803A1 Fault-tolerant actuating system for adjusting flaps of an aircraft, comprising adjustment kinematics with a fixed pivot
11/11/2009	EP2027518B8 Method for piloting an aircraft in approach phase
11/05/2009	WO2009110943A9 Aircraft drag management structure
11/05/2009	WO2008028184A3 Electromechanical actuating assembly
11/05/2009	US20090272843 Adjusting device for adjusting a high-lift flap and airfoil wing comprising such an adjusting device
10/2009
10/29/2009	US20090266940 Precision adjust split detent for a vehicle
10/29/2009	US20090266939 Active pilot inceptor with self warm-up
10/29/2009	US20090266934 Hydraulic fluid supply device and electric actuator
10/29/2009	DE102006025388B4 Line system arrangement for use in fuselage of e.g. aircraft, has receiving region for receiving component of line system, and adapted to internal pressure which corresponds to particular external pressure of fuselage
10/28/2009	EP2112063A2 Active pilot inceptor with self warm-up
10/27/2009	US7607611 Flight control surface actuation system with redundantly configured and lockable actuator assemblies
10/22/2009	WO2009127577A1 Linearization of actuators affected by hysteresis
10/22/2009	WO2008122820A3 Multi-axis serially redundant, single channel, multi-path fly-by-wire flight control system
10/22/2009	US20090261205 Apparatus and method for controlling twist of a wing of an airborne mobile platform
10/22/2009	DE102008019372A1 Transmission shaft for use in assembly of high lift system of aircraft for transmission of torque and axial forces, has plug-in toothing for connecting transmission shaft with counter piece with another plug-in toothing
10/15/2009	WO2009126905A1 Tilt actuation for a rotorcraft
10/15/2009	WO2009125091A1 Method and device for detecting absences of manual and automatic piloting of an aircraft
10/15/2009	WO2009125090A1 System and method for heating the hydraulic fluid of an aircraft
10/15/2009	WO2009083261A3 System for actuating at least one regulating flap of an aircraft and a method for checking the system.
10/15/2009	US20090256026 Tilt Actuation for a Rotorcraft
10/14/2009	CN101557980A Device and method for the temperature regulation of a hydraulic fluid
10/14/2009	CN100548796C Landing flap drive system
10/13/2009	US7603207 Surrogate air processor
10/13/2009	US7600715 Local backup hydraulic actuator for aircraft control systems
10/13/2009	CA2562894C Methods and apparatus for minimizing backlash in a planetary gear mechanism
10/13/2009	CA2484328C Integrated three function valve
10/08/2009	WO2009124027A1 Hydraulic system for aircraft
10/07/2009	EP2107265A1 Torque limiter with brake
10/07/2009	EP2107002A2 Collective system for rotary wing aircraft
10/06/2009	US7597285 Fluid dynamically effective surface for minimizing induced resistance
10/01/2009	US20090242705 Hydraulic system protected from external impacts
10/01/2009	US20090242694 Hydraulic system for aircraft
10/01/2009	DE102008015269A1 Hydraulic sound absorber, particularly for integration in aircraft hydraulic system, has continuous inner pipe with perforation section, which is surrounded by housing below formation of hollow chamber filled with gas
09/2009
09/24/2009	DE102008014236A1 Schwingungsreduktionsvorrichtung Vibration reduction device
09/17/2009	WO2009112213A1 Vibration damping device
09/17/2009	US20090234518 Active-inceptor tactile-cueing hands-off rate-limit
09/17/2009	US20090230253 Method and device for piloting an aircraft optimizing the control of the ailerons in an enhanced-lift configuration
09/17/2009	US20090230252 Aircraft flight control
09/11/2009	WO2009110943A2 Aircraft drag management structure
09/11/2009	WO2008112363A4 Electromechanical actuating assembly
09/10/2009	US20090224094 System for tactical balloon launch and payload return
09/09/2009	EP2097315A2 Control stick adapted for use in a fly-by-wire flight control system, and linkage for use therein
09/09/2009	CN101528539A Control stick adapted for use in a fly-by-wire flight control system, and linkage for use therein
09/03/2009	US20090222148 Autonomous Outer Loop Control of Man-Rated Fly-By-Wire Aircraft
09/03/2009	US20090218443 Magnetorheological fluid elastic lag damper for helicopter rotors
09/03/2009	US20090218442 Trailing edge aircraft structure with overhanging cover
09/03/2009	DE102005032849B4 Vorrichtung und Verfahren zum Überführen eines Flugzeugs von einem außerhalb eines zulässigen Flugzustandsbereichs in einen innerhalb des zulässigen Flugzustandsbereichs liegenden Flugzustand Apparatus and method for transferring an aircraft of a permitted outside a flight condition range in a lying within the permissible flight condition range flight condition
09/02/2009	EP2027518B1 Method for piloting an aircraft in approach phase
09/02/2009	EP1954547B1 A remote control system
09/02/2009	CN100534862C Dual motor dual concentric valve
09/01/2009	US7581702 Wirelessly controlling unmanned aircraft and accessing associated surveillance data
09/01/2009	CA2349768C Aircraft with electric flight controls and automatic pilot
08/2009
08/27/2009	WO2009104288A1 Control system and control bar link separating method
08/27/2009	US20090212167 Actuator systems and associated methods for unmanned air vehicles and other applications
08/27/2009	US20090212158 Aircraft Systems with Shape Memory Alloy (SMA) Actuators, and Associated Methods
08/27/2009	CA2697432A1 Flight controlsystem and method of separating control lever linkage
08/25/2009	US7580777 Modular aircraft control system and method
08/25/2009	US7578483 Conformable skin element system for active vortex control
08/20/2009	WO2009101324A1 Distributed flight control system
08/20/2009	US20090206209 Systems and methods for providing differential motion to wing high lift device
08/20/2009	US20090206195 Rotating air cargo delivery system and method of construction
08/20/2009	US20090206192 Methods and apparatus for adjustable surfaces
08/19/2009	CN101508339A Directly connected-type direct current electric steering engine of rocker structure
08/19/2009	CN101508338A Plasma gurney flap
08/18/2009	US7576754 System and method for identifying bounds of a geographical area
08/18/2009	CA2449861C Vibration motor primary flight control actuator
08/18/2009	CA2370439C Control device for a system to monitor the environment of an aircraft, specifically a cargo aircraft
08/13/2009	US20090200431 Aircraft wing tip having a variable incidence angle
08/13/2009	US20090200430 Intelligent multifunctional actuation system for vibration and buffet suppression
08/13/2009	US20090200420 Actuator arrangement
08/12/2009	CN101506038A Jam-tolerant actuator
08/11/2009	US7571878 Method and a calculating unit for calculation of a recovery flight path
08/11/2009	CA2478535C Method and apparatus for tactile cueing of aircraft controls
08/06/2009	WO2009065597A4 Landing flap mechanism driven by pinion gears
08/06/2009	WO2008156926A3 Control surface failure detection for fly-by-wire aircraft

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