Patents
Patents for B64C 5 - Stabilising surfaces (949)
12/2009
12/30/2009WO2009156549A2 Structure of an aircraft aerofoil
12/30/2009CN201371941Y Tail incidence angle adjusting device
12/29/2009US7637453 Aircraft spiraling mechanism with jet assistance - A
12/09/2009EP2130762A2 Wing and empennage leading edge structure made of thermoplastic material with a stiffened double-shell configuration
12/03/2009DE102008022452A1 Aircraft, has central flight controller adapted such that individual auxiliary wings are adjusted in position independent of other auxiliary wings, where position of auxiliary wings is adjusted to each other and to main wings
11/2009
11/26/2009WO2009142793A2 Ice shed reduction for leading edge structures
11/26/2009US20090289144 Trimmable horizontal stabilizer
11/26/2009CA2722099A1 Ice shed reduction for leading edge structures
11/19/2009WO2009140019A1 Shape-changing structure with superelastic foam material
11/12/2009US20090277996 Wing and empennage leading edge structure made of thermoplastic material with a stiffened double shell configuration
11/10/2009CA2340297C Vehicle with vertical wings and a stabilizing torque system of jets to use fluid energy for forward motion
10/2009
10/22/2009WO2009129023A1 Winglets with recessed surfaces, and associated systems and methods
10/21/2009CN101559832A Fast hybrid helicopter with large range
10/15/2009WO2009126905A1 Tilt actuation for a rotorcraft
10/08/2009WO2008081098A8 Aircraft with rear annular tail
10/06/2009US7597285 Fluid dynamically effective surface for minimizing induced resistance
10/06/2009CA2343590C Leading edge of supporting surfaces of aircraft
09/2009
09/17/2009WO2009112641A1 Leading edge element of aircraft, method for manufacturing one, wing and stabilizer
09/10/2009DE102008012275A1 Extendable/foldable side rudder sail for helicopter, has telescope bars/pipes provided under continuous operating voltage for emergency rescue system, and centrifugal force actuator for system to rapidly turn helicopter at vertical axis
09/09/2009EP1735211B1 Fairing for an aircraft structure
09/01/2009US7581696 Aircraft attitude control configuration
08/2009
08/26/2009CN201296356Y Horizontal tail wing of wing-in-ground effect craft
08/26/2009CN100532196C Fairing for an aircraft structure
08/19/2009EP2089273A1 Aircraft with rear annular tail
08/12/2009CN100526159C Turbojet for aircraft, aircraft equipped with such a turbojet, and method for mounting such a turbojet on an aircraft
08/06/2009WO2008155720A3 Method and equipment for forming and assembling uncured spars for the horizontal stabilizers of aircraft
08/05/2009EP1692038A4 Wing gull integration for nacelle clearance, compact landing gear stowage, and sonic boom reduction
07/2009
07/21/2009US7562845 Rudder unit connection to a fuselage without a bolt-fairing structure
07/09/2009US20090173838 Narrow Wing System for Airplanes
06/2009
06/25/2009US20090159742 Lifting structure for aircraft
06/25/2009DE102007059455A1 Flügelspitzenverlängerung zur Reduktion von Wirbelschleppen bei Flugzeugen Wingtip extension for the reduction of wake vortices on aircraft
06/23/2009US7550189 Variable stiffness structure
06/17/2009EP2070816A2 Methods and apparatus for an integrated aerodynamic panel
06/10/2009EP2066563A1 Curved element, wing, control surface and stabilizer for aircraft
06/03/2009EP2064116A2 Aerodynamic body and carrier wing comprising an aerodynamic body, actuating drive control module, computer, computer program, and method for influencing post-turbulences
05/2009
05/28/2009WO2009067399A1 System and method for deployment and actuation
05/28/2009WO2009065320A1 Aircraft with falling protection apparatus
05/14/2009WO2009035378A3 Fuselage and a method for redesigning it
05/13/2009CN101428683A Double-vane superaltitude unmanned aircraft
05/06/2009CN100484830C Rotation fitting for the empennage of an aircraft
04/2009
04/09/2009WO2005062743A3 Supersonic aircraft with aerodynamic tail structure
04/08/2009CN100475649C Ground effect flyer
03/2009
03/31/2009US7510757 Cellular composite grid-stiffened structure
03/31/2009US7510144 Elastic pre-deformed fairings for aircrafts
03/25/2009EP2038602A2 Two-axis trajectory control system
03/25/2009EP2038171A1 Trimmable horizontal stabilizer
03/25/2009CN101395058A Bolted joint
03/19/2009WO2009035378A2 Fuselage and a method for redesigning it
03/19/2009WO2009016094A3 Aircraft tail assembly
03/19/2009US20090072085 Live trim tabs
03/05/2009US20090057483 Elastic pre-deformed fairings for aircrafts
02/2009
02/19/2009WO2009023352A2 Controllable winglets
02/19/2009US20090045286 Grid fin control system for a fluid-borne object
02/05/2009WO2009016094A2 Aircraft tail assembly
02/05/2009CA2694594A1 Aircraft tail assembly
01/2009
01/29/2009US20090026311 Aircraft tail assembly
01/13/2009US7475848 Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance
01/08/2009US20090008498 Aircraft stabilizer system and methods of using the same
12/2008
12/24/2008WO2008155720A2 Method and equipment for forming and assembling uncured spars for the horizontal stabilizers of aircraft
12/24/2008EP1954563B1 Turbojet for aircraft, aircraft equipped with such a turbojet, and method for mounting such a turbojet on an aircraft
12/24/2008DE102007027137A1 Brake unit for drive system for landing e.g. airbrake of aircraft, has brake electrically or hydraulically operated for configuring and/or releasing drive element, and mechanically operated at same time for limiting torque
12/18/2008DE10302514B4 Strömungsmechanisch wirksame Fläche eines sich in einem Fluid bewegenden Geräts, insbesondere eines Fluggeräts, insbesondere Tragfläche eines Fluggeräts Fluidically effective area of ​​a moving fluid in a device, in particular an aircraft, in particular wing of an aircraft
12/11/2008WO2008105899A3 Two-axis trajectory control system
12/11/2008DE102007026765A1 Tragflügel mit verstellbarem Spoiler Wing with adjustable spoiler
12/04/2008DE102007004746A1 Aerodynamic propulsion system for aircraft, has aerodynamic lifting body, e.g. wing, which is fastened in enclosing channel and produces pressure of gas
12/03/2008EP1996457A1 Bolted joint
12/03/2008EP1996456A2 Bolted joint
11/2008
11/19/2008CN101306722A Rib structure for torsion boxes of a wing or horizontal stabiliser of an aircraft
11/11/2008US7448578 Aircraft with forward opening inlay spoilers for yaw control
11/06/2008US20080272615 Airflow control devices based on active materials
10/2008
10/30/2008US20080265102 Deployable flap edge fence
10/30/2008DE102007019716A1 Faser-Metall-Laminat-Panel Fibre metal laminate panel
10/09/2008WO2008121005A1 Aircraft component manufacture and assembly
09/2008
09/30/2008US7429074 Airflow control devices based on active materials
09/23/2008CA2444560C Method and apparatus for rotatably supporting movable components, including canards
09/18/2008US20080223991 Wing Tip Device
09/17/2008CN101267984A Turbojet for aircraft, aircraft equipped with such a turbojet, and method for mounting such a turbojet on an aircraft
09/09/2008US7424350 Vehicle control systems and corresponding sizing methods
09/02/2008CA2465163C Apparatus and methods for actuating rotatable members
08/2008
08/26/2008US7416155 Canard position and dihedral for boom reduction and pitch/directional control
08/21/2008DE102004019496B4 Tragflügel für Fluggeräte mit Triebwerken Hydrofoil for aircraft with engines
08/14/2008US20080191101 Aerofoil Surface for Controlling Spin
08/13/2008EP1954563A1 Turbojet for aircraft, aircraft equipped with such a turbojet, and method for mounting such a turbojet on an aircraft
08/12/2008US7410132 Jam tolerant electromechanical actuation systems and methods of operation
08/12/2008US7410120 Control surface assemblies with torque tube base
08/05/2008US7406777 Method and apparatus employing eccentric bushing
07/2008
07/31/2008US20080179450 Lifting-Type Aeroplane Fuselage
07/24/2008DE10145272B4 Flugzeug, insbesondere Passagierflugzeug, mit einem auf der Basis von Faserverbundbauteilen aufgebauten Rumpf Aircraft, especially passenger aircraft, with a built up on the basis of composite components hull
07/23/2008EP1945501A2 Aircraft attitude control configuration
07/23/2008EP1751432B1 Method and apparatus employing eccentric bushing
07/10/2008WO2008081098A1 Aircraft with rear annular tail
07/10/2008CA2670649A1 Aircraft with rear annular tail
07/03/2008US20080157713 Electrochemical methods, devices, and structures
06/2008
06/19/2008WO2008073069A2 Unmanned aerial vehicle
06/19/2008US20080142641 Airplane configuration
06/19/2008DE202007014079U1 Verbesserungen an einem Mini-Jet Luftfahrtzeug Improvements to a mini-jet aviation stuff
06/05/2008WO2008066512A2 Systems and methods for refueling spacecraft
06/05/2008US20080128548 Control linkage
05/2008
05/29/2008DE102006055090A1 Wing i.e. airfoil wing, end form for wing of commercial aircraft, has transition area arranged between wing and winglet, where local V-form changes continuously from wing to winglet in transition area
05/08/2008WO2008031620A3 Aerodynamic body and carrier wing comprising an aerodynamic body, actuating drive control module, computer, computer program, and method for influencing post-turbulences
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