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Match Document Document Title
US20110042526 METHOD FOR REDUCING THE TAKEOFF RUN OF AN AIRCRAFT  
The method of the invention comprises imparting to the flaps (6G, 6D) of said aircraft either a nose-up deflection (αF) corresponding to the maximum sharpness if the nose-up order is higher than a...
US20130306788 UNMANNED AIR SYSTEM (UAS)  
An unmanned air system and method with blown flaps are presented. Air is guided to a fuel cell carried by the unmanned air system. The fuel cell is ventilated by the guided air such that the air...
US20120104178 CANTILEVERED DIFFERENTIAL MOTION SENSOR AND ASSOCIATED FRAME  
The disclosed sensor includes a frame having a base and a plurality of arms integral with the base. The arms are biased to a relaxed position, which may be an extended position. A fuse is fastened...
US20100320332 SPOILER FOR AN AERODYNAMIC BODY OF AN AIRCRAFT  
The invention pertains to a spoiler (5) for an aerodynamically active surface of an aircraft (1), particularly for an airfoil of an aircraft, wherein said spoiler is supported on the...
US20110290945 AIRCRAFT SLAT ASSEMBLY COMPRISING A PLURALITY OF SLATS  
An aircraft slat assembly comprises a first slat and a second slat positioned adjacent thereto. The first and second slats are moveable between extended and retracted positions. The slats are...
US20110054719 METHOD FOR DRAMATICALLY REDUCING THE TAKE-OFF RUN OF AN AIRCRAFT  
According to the invention, during take-off, the aircraft (AC) is given an attitude (θc) close to the tail-touching attitude and the ailerons (6G, 6D) are fully deflected downwards.
US20080191101 Aerofoil Surface for Controlling Spin  
The invention concerns craft of the type in which a fan directs a jet of fluid (4) over a curved canopy (1). The canopy (1) is shaped to divert the flow from a radial to an axial direction to...
US20110290946 AIRCRAFT SLAT ASSEMBLY  
An aircraft slat assembly comprises a slat, two tracks and two joints, each joint connecting a respective track to the slat. Each track is moveable on a wing structure between a fully extended...
US20080283672 Drive system for a variable camber aircraft wing  
The present invention relates to a drive system for a variable camber aircraft wing having position variable front flaps and/or rear flaps, having drive shafts, which are arranged such that that...
US20120248256 Pressure Based Load Measurement  
A system and method for a pressure based load measurement system are provided. The system includes two pressure orifices arranged on a top surface and a bottom surface of an airfoil. The pressure...
US20140027580 HIGH LIFT SYSTEM FOR AN AIRCRAFT  
A high lift system for an aircraft, which extends and retracts the landing flaps of the aircraft in a fully electric manner. In this context, a fully electric drive is used, comprising an electric...
US20150144741 AERODYNAMIC SEALING MEMBER FOR AIRCRAFT  
A sealing member for forming a seal in an aircraft, the sealing member comprising: a sealing material; and a stiffening element which provides structural support to the sealing material and...
US20090146014 Actuation System for a Lift Assisting Device and Roller Bearings Used Therein  
An actuation system for deploying and retracting a lift assisting device of a wing of an aircraft, is presented. The actuation system includes a track pivotally coupled to the lift assisting...
US20140048656 HIGH LIFT COMPONENT FOR AN AIRCRAFT, HIGH LIFT SYSTEM, METHOD FOR ADJUSTING THE HIGH LIFT CHARACTERISTICS OF AN AIRCRAFT AND AIRCRAFT  
A high lift component includes at least one intermediate seal on at least one lateral surface, wherein the intermediate seal includes at least one hollow body made of an elastic material, which...
US20120304475 RESOLVER TYPE SKEW SENSOR WITH GIMBAL ATTACHMENT  
A disclosed sensor assembly for detecting movement and a position of a wing flap includes a sensing device that generates a signal corresponding to a position of the flap. The sensor assembly...
US20130020444 Trailing Edge Split Flap with Pneumatic Actuation  
A system for pneumatically actuating a split flap hingedly mounted near or at a trailing edge of an airfoil. The system includes a bladder system disposed between the split flap and the upper...
US20120061524 AEROFOIL COMPRISING A HIGH LIFT FLAP  
A wing is provided, including a high-lift flap arranged on the wing such that it is movable by means of at least two adjustment mechanisms arranged side-by-side in the spanwise direction of the...
US20120138750 AEROFOIL COMPRISING A HIGH LIFT FLAP  
An aerofoil wing is provided, including a main aerofoil, and a high-lift flap, which is movably arranged on the wing using side-by-side adjustment mechanisms. Each adjustment mechanism includes a...
US20120074264 AIRPLANE WING  
An airplane wing configuration includes a first wing positioned above and forward of a second wing on an airplane fuselage. The first wing is operable to direct airflow over an upper surface of...
US20120145826 HIGH-LIFT-DEVICE, WING, AND NOISE REDUCTION DEVICE FOR HIGH-LIFT-DEVICE  
In a high-lift-device, a wing, and noise reduction device for a high-lift-device that are capable of reducing noise generated when a flap is extended, preventing deterioration of aerodynamics...
US20090146015 Aircraft highlift system  
The present invention relates to an aircraft high-lift system with at least one drive unit for operating the high-lift systems of the half wings (half-wing systems) and with at least one overload...
US20130306801 ARTICULABLE ROTATIONAL COUPLING FOR AN AIRCRAFT  
An airfoil surface control system includes a movable surface. An actuator is coupled to the surface. The airfoil surface control system includes a motor. A torque tube assembly operatively couples...
US20110011984 High Lift System for an Aircraft  
A high-lift system for an aircraft includes a main wing, a lift flap arranged on the main wing of the aircraft, which lift flap is adjustable, between a retracted position and several extended...
US20120168567 ELECTRICAL POWER TRANSFER ASSEMBLY  
An assembly for an aircraft including a first structure mounted to a second structure, and a power transfer assembly electrically connecting the first and second structures. The first structure is...
US20110163204 HIGH LIFT SYSTEM FOR AN AIRCRAFT WITH A HIGH LIFT FLAP AND METHOD FOR ADJUSTING THE HIGH LIFT FLAP  
A high lift system for an aircraft with at least one high lift flap arranged on each of the main wings of the aircraft. The high lift system includes an input device for the generation of flight...
US20090292405 WING-BODY LOAD ALLEVIATION FOR AIRCRAFT  
A computer implemented method, apparatus, and computer usable program product for symmetric and anti-symmetric control of aircraft flight control surfaces to reduce wing-body loads. Commands are...
US20140048655 HIGH LIFT SYSTEM FOR AN AIRCRAFT AND METHOD FOR INFLUENCING THE HIGH LIFT CHARACTERISTICS OF AN AIRCRAFT  
A high lift system for an aircraft includes a basic body, a flap which is movably mounted on the basic body and has a flap edge, and a retaining element. The high lift system is set up to form a...
US20120091282 HIGH LIFT SYSTEM FOR AN AIRCRAFT AND METHOD FOR DETECTING FAULTS IN A HIGH LIFT SYSTEM FOR AN AIRCRAFT  
The present invention relates to a high lift system for an aircraft, comprising a flap, which is arranged on a wing box and which can be moved between a retracted position and at least one...
US20090127403 LIFT FLAP CARRIER SYSTEM  
Device for carrying lift flaps arranged on the wings of an aircraft and a wing. The device includes a carrier with a U-shaped profile, a covering plate positionable over an open side of the...
US20050242234 Lifters, methods of flight control and maneuver load alleviation  
The present invention provides a flight control system and method for various models of aircraft, including thin-winged, long range, transonic and low supersonic aircraft, and may be beneficial on...
US20130228655 METHOD AND DEVICE FOR FITTING OUT AN AIRCRAFT NOSE COMPARTMENT IN AN AVIONICS BAY  
An aerodynamic body, with at least one ancillary flap arranged such that it can be moved on the aerodynamic body with the aid of a guide mechanism, and with a drive device for purposes of...
US20120325977 AIRCRAFT WITH A DEVICE FOR DIRECTIONALLY STABILIZING THE AIRCRAFT, COMPUTER PROGRAM PRODUCT AND METHOD FOR DIRECTIONALLY STABILIZING THE AIRCRAFT  
A method for reducing yawing motions of an aircraft in-flight, wherein a spoiler adjustment drive of a spoiler and a regulating flap adjustment drive of a regulating flap of the same respective...
US20150060607 LIFT FLAP BEARING APPARATUS, LIFT FLAP ASSEMBLY, AIRFOIL AND AIRCRAFT  
A lift flap bearing apparatus is improved with respect to aerodynamics, construction space and assembly, for guiding and adjusting a first lift flap and a second lift flap. The lift flap bearing...
US20100252674 Reducing runway requirement for aircraft  
Runway length requirement for take-off and landing of an aircraft is reduced by taking advantage of dynamic lift overshoot, and in some cases, dynamic stall. In take-off and landing, the angle of...
US20090200431 AIRCRAFT WING TIP HAVING A VARIABLE INCIDENCE ANGLE  
An embodiment of an aircraft wing includes a main wing section and a variable incidence wing tip. The main wing section is adapted to connect to an aircraft fuselage at a first angle of incidence....
US20110042525 SUPPORT ASSEMBLY  
A support assembly (1) for guiding a flap (42) on an aircraft wing (41) during deployment of the flap is disclosed. The assembly comprises a guide track (2) defining a two-dimensional path, a...
US20110297796 VANE HAVING A REGULATING FLAP AND A GAP COVERING DEVICE AND AN ADJUSTING MECHANISM FOR A GAP COVERING DEVICE  
A wing, having an adjustable flap that can be moved between a retracted and an extended setting is provided, as well as a gap-covering device, with an adjustment lever and a gap-covering flap...
US20090146013 FLIGHT CONTROL USING ACTUATED VARIABLE MOMENT ARM  
Systems and techniques are described for actuating a control surface about a pivot point using variable moments. A bracket having a moment arm is coupled to the pivot point such that the bracket...
US20090014594 JACK SYSTEM WITH AUTOMATIC LOCKING OF THE PISTON IN HIGH POSITION, ESPECIALLY FOR AIRCRAFT  
This invention provides a jack system (2) provided with a cylinder (14) provided with stop means (32). It also comprises: a body (36) hinged about an end (18) of the piston, the body comprising...
US20150053825 HIGH-LIFT DEVICE OF AIR VEHICLE  
A high-lift device includes a flap body which is provided at a rear portion of a main wing which generates a lift for the air vehicle such that the flap body is deployed with respect to the main...
US20100219299 HIGH-LIFT SYSTEM ON THE WING OF AN AIRCRAFT, AND METHOD FOR ITS OPERATION  
A high-lift system on the wing of an aircraft and a method for its operation are described. High-lift flaps (2) which are arranged on the wing (1) are extended from a retracted position in order...
US20120104179 AIRCRAFT  
The idea of the invention is that the aircraft comprises takeoff and landing wings that are the main aerodynamic elements producing a lift at all stages of takeoff and landing. In cruising flight,...
US20130009017 ELECTRONICALLY SYNCHRONIZED FLAP SYSTEM  
An electronically-synchronized flap system for a fixed-wing aircraft including a first wing including a first flap panel, the first flap panel being connected with a first in-board actuator and a...
US20130099061 FLAP ROLLER ARRANGEMENT, FLAP ASSEMBLY, AND METHOD FOR REMOVING A ROLLER ASSEMBLY FROM A FLAP FITTING  
A flap roller arrangement for supporting a flap on a wing of an aircraft is disclosed herein. The flap roller arrangement includes, but is not limited to, a roller assembly that is configured for...
US20120292453 WING ARRANGEMENT COMPRISING AN ADJUSTABLE FLAP AND FAIRING ELEMENT FOR COVERING A FLAP ADJUSTMENT MECHANISM OF A WING  
A wing arrangement includes, but is not limited to an adjustable flap, which is adjustable between a retracted position and at least one extended position, has at least one fairing element for...
US20130214096 SEAL ASSEMBLY  
A seal assembly for closing an aperture in an aerodynamic surface of a structure, the seal assembly comprising: a track for attachment to the structure; and a retractable seal including a flexible...
US20090050749 Aircraft wing spoiler arrangement  
An aircraft wing comprising an upper surface; and two or more spoilers pivotally attached to the upper surface, wherein at least two adjacent ones of the spoilers are separated by a gap, and...
US20080142640 Deflection device for a stream body  
The present application describes to a deflection device, for example, for a blunt stream body. The deflection device has an edge, which, for example, can be mounted to the stream body. In an...
US20110101174 High Lift System For An Aircraft  
A high lift system for an aircraft includes: a main wing, a flap disposed on the main wing of the aircraft that can be adjusted between a retracted position and several extended positions relative...
US20110114795 Aerodynamic Flap and Wing  
An aerodynamic flap with an articulation device to form an axis of rotation for purposes of a rotatable mounting of the aerodynamic flap on a wing section or structural section, with the flap...

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