Patents
Patents for B64C 9 - Adjustable control surfaces or members, e.g. rudders (2,586)
07/2007
07/05/2007US20070152105 Composite fiber component produced by braiding
07/05/2007DE102005061750A1 Flexible Steuerfläche für ein Luftfahrzeug Flexible control surface for an aircraft
06/2007
06/28/2007WO2007071384A2 Flexible control surface for an aircraft
06/28/2007DE102005059370A1 Seitenruder eines Verkehrsflugzeugs Rudder of a commercial aircraft
06/28/2007DE102005058192A1 Vorrichtung zur Fehlererkennung von verstellbaren Klappen Device for error detection of adjustable flaps
06/28/2007CA2634519A1 Flexible control surface for an aircraft
06/27/2007EP1799542A2 Leading edge flap apparatuses and associated methods
06/21/2007WO2007068450A1 Rudder of a commercial aircraft
06/21/2007CA2628325A1 Rudder of a commercial aircraft
06/20/2007CN1982157A Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods
06/12/2007US7229046 Servo mounting system for direct drive of an aircraft control surface
05/2007
05/31/2007WO2007062005A1 Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods
05/31/2007US20070120006 Pressure sensor system
05/24/2007DE102005054248A1 Braking flap for deceleration of aircraft against air-flow which surrounds aircraft, comprises many vortex edges, which resolve individual edge section into number of vortex part, are arranged at free edge
05/23/2007EP1787905A2 Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods
05/23/2007EP1786667A1 Systems and methods for providing differential motion to wing high lift devices
05/18/2007WO2007056477A1 Wing leading edge slat system
05/18/2007WO2007054150A1 Advanced trailing edge control surface on the wing of an aircraft
05/18/2007CA2622320A1 Advanced trailing edge control surface on the wing of an aircraft
05/16/2007EP1608555A4 Winged spacecraft
05/15/2007US7216830 Wing gull integration nacelle clearance, compact landing gear stowage, and sonic boom reduction
05/10/2007US20070102588 Servo Mounting System for Direct Drive of an Aircraft Control Surface
05/10/2007US20070102575 Aircraft attitude control configuration
04/2007
04/26/2007DE102005048434A1 Polyurethanlacke als Scheuerschutz-Beschichtungen Polyurethane coatings as abrasion protection coatings
04/19/2007WO2007042398A1 Polyurethane lacquers as abrasion-resistant coatings
04/18/2007CN1950252A Aircraft leading edge device systems and corresponding sizing methods
04/12/2007WO2007040747A1 Energy recovery apparatus and method
04/12/2007WO2006084157A3 Systems and methods for controlling aircraft flaps and spoilers
04/10/2007US7201700 Geared rotary actuators
04/10/2007US7201347 Process for improving the landing of an aircraft
04/10/2007CA2315167C Improved aileron for fixed wing aircraft
04/04/2007EP1768899A1 Method and device for improving maneuverability of an aircraft during approach phases before landing followed by flare-out
04/04/2007EP1768898A1 Mobile leading-edge flap for a main wing of the aerofoils of an aircraft
04/03/2007US7198227 Aircraft cargo locating system
03/2007
03/29/2007US20070069067 Aircraft spiraling mechanism with jet assistance - A
03/29/2007DE102005044549A1 Flugzeugflügel mit ausfahrbarer Nasenklappe Airplane wing with extendable nose flap
03/28/2007EP1658221B1 Rigid wing with variable sustentation due to deployment of a flexible wing
03/27/2007US7195209 Aircraft high-lift system with overload protection
03/27/2007US7195207 Winged spacecraft
03/22/2007US20070063109 Rotary flap
03/22/2007DE102006028885A1 Hybrid aircraft e.g. helicopter, has two wings arranged laterally at casing and engaging together with casing by rotating around axis using rotating mechanism, rotation symmetric and mirror symmetrical configuration
03/22/2007DE102005033697A1 Control surface e.g. rudder, operating mechanism for airplane, has gearing placed downstream of hydraulic motor so that drive shaft of motor drives input shaft of gearing, and output shaft coincides with rotational axis of rudder
03/21/2007EP1764303A2 Aircraft wing with a leading edge slat
03/08/2007WO2006016070A8 Method and device for improving maneuverability of an aircraft during approach phases before landing followed by flare-out
02/2007
02/28/2007EP1757519A2 Aircraft wing slat
02/28/2007EP1755946A1 High-lift device for an aircraft
02/22/2007WO2007001735A3 Aerospace vehicle yaw generating systems and associated methods
02/22/2007WO2006135421A3 Leading edge flap apparatuses and associated methods
02/22/2007DE102005038857A1 Center case for airplane wing, has side surfaces planking case at sides, where one surface comprises shells that are arranged spatially to each other by distance and connected with one another by U-profiles in longitudinal direction of case
02/22/2007DE102005038856A1 Fastening system for attaching tail unit at fastening surface of airplane, has contact surfaces for attachment at tail unit and fastening surface, where contact surfaces comprise contact line and differentiating angle of specified degrees
02/21/2007CN1918033A Landing flap guide for aircraft
02/15/2007US20070034746 System for aerodynamic flows and associated method
02/13/2007US7175132 Mechanism for eliminating limit cycle oscillations on servocontrolled aerodynamic control surfaces
02/01/2007DE112005000443T5 Vorderkantenvorrichtungssystem für Luftfahrzeuge und entsprechende Dimensionierungsverfahren Leading edge device system for aircraft and appropriate dimensioning method
01/2007
01/23/2007US7165742 Aircraft spiralling mechanism - B
01/11/2007WO2006108579B1 Single slotted flap with sliding deflector flap and lowerable spoiler
01/09/2007US7159825 Process and device for the optimization of the deflection of the spoiler flaps of an aircraft in flight
01/04/2007WO2007001735A2 Aerospace vehicle yaw generating systems and associated methods
01/04/2007US20070001052 Method for damping rear extension arm vibrations of rotorcrafts and rotorcraft with a rear extension arm vibration damping device
12/2006
12/21/2006WO2006133940A1 Lift-augmenting flap, in particular leading edge flap, for an aerodynamically effective wing
12/21/2006US20060284023 Deflection device for a stream body
12/21/2006CA2610297A1 Lift-augmenting flap, in particular leading edge flap, for an aerodynamically effective wing
11/2006
11/30/2006WO2006127204A1 Aerospace vehicle fairing systems and associated methods
11/29/2006EP1587734B1 Aircraft with forward opening inlay spoilers for yaw control
11/23/2006US20060261217 Aerospace vehicle fairing systems and associated methods
11/22/2006EP1723032A1 Aircraft leading edge device systems and corresponding sizing methods
11/22/2006EP1631493B1 Aircraft with topside only spoilers
11/14/2006CA2291729C A drogue assembly for in-flight refuelling
10/2006
10/26/2006US20060237580 Canard position and dihedral for boom reduction and pitch/directional control
10/25/2006EP1714106A1 2-d projectile trajectory correction system and method
10/25/2006EP1713688A1 Landing flap guide for aircraft
10/19/2006WO2006108648A1 Landing flap drive system
10/19/2006WO2006108579A1 Single slotted flap with sliding deflector flap and lowerable spoiler
10/19/2006DE102005016639A1 Tragflügel mit ausfahrbaren aerodynamischen Flügelklappen, insbesondere Auftriebsklappen Wing with extendable aerodynamic wing flaps, in particular lift flaps
10/19/2006DE102005016638A1 Flügelklappen-Mechanismus zur Verstellung einer einem Tragflügel zugeordneten aerodynamischen Flügelklappe Wing flap mechanism for adjusting a associated with a wing aerodynamic flap
10/19/2006DE102005016578A1 Airplane`s lift characteristics adjusting device, has spoiler devices movably fastened at wing unit and/or at high lift device, where spoiler devices are designed such that size of gap between wing unit and high lift device is adjusted
10/19/2006DE102005015338A1 Fin alignment for connection of fin with aircraft body, has bolts and pins coupling root base area with ribs and staying in connection with two spars that are connected with one another in root tip area
10/19/2006CA2598419A1 Single slotted flap with sliding deflector flap and lowerable spoiler
10/12/2006US20060226297 Wing with extendable aerodynamic pivoted flaps
10/11/2006CN1845848A Flow-mechanically effective surface for minimising induced resistance
10/05/2006DE102004063018A1 Vorrichtung zur Überwachung von verschwenkbaren Klappen an Flugzeugtragflügeln Device for monitoring pivotable flaps on airplane wings
10/04/2006EP1706315A1 Mobile leading edge flap for a main wing of the aerofoils of an aircraft and main wing provided with such a flap
09/2006
09/26/2006US7111810 Forward pivoted full flying control tail boom
09/19/2006US7108231 Adjustment mechanism for a variable-shape wing
09/19/2006US7108230 Aircraft with topside only spoilers
09/08/2006WO2006093512A1 Methods and apparatuses for controlling airflow proximate to engine/airfoil systems
09/07/2006DE10317258B4 Verstellmechanismus für einen formvariablen Flügel Adjustment mechanism for a shape-variable wing
09/05/2006CA2431352C An aircraft flap extension mechanism
08/2006
08/30/2006EP1695905A1 Aircraft with extendable leading edge of fuselage and wings
08/30/2006EP1695904A1 Aircraft with articulated leading edge of fuselage and wings
08/30/2006EP1695903A1 Aircraft with rotatable leading edge of fuselage and wings
08/23/2006EP1692038A2 Wing gull integration for nacelle clearance, compact landing gear stowage, and sonic boom reduction
08/23/2006EP1467909B1 Joint for connecting components together on opposite longitudinal sides in addition to a flexible strip used for said joint
08/22/2006US7093791 Aircraft spiralling mechanism—c
08/17/2006WO2006085981A1 Propulsion system for model airplane
08/10/2006WO2006084157A2 Systems and methods for controlling aircraft flaps and spoilers
08/10/2006WO2006083547A1 Aerospace vehicle leading edge slat devices and corresponding methods
08/10/2006US20060175469 Wing of aircraft
08/10/2006US20060175468 Systems and methods for controlling aircraft flaps and spoilers
08/10/2006CA2706676A1 Systems and methods for controlling aircraft flaps and spoilers
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