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Matches 1 - 50 out of 1,069

Document Document Title
WO/2018/005534A1
Trailing edge assemblies, couplers and methods for deploying a trailing edge flap of an aircraft wing are disclosed. An exemplary method disclosed herein comprises guiding an aft portion of the trailing edge flap (28) along an elongated ...  
WO/2018/005524A1
Systems and methods for deploying adjacent trailing edge flaps that are part of different flap assemblies of different stiffnesses are disclosed. An exemplary method comprises: deploying a first flap of a first flap assembly having a fir...  
WO/2018/005529A1
A temperature monitoring unit may be removably installed inside an aircraft wing structure for monitoring temperature conditions along the span of the wing. The wing structure has a temperature-sensitive device (162) for monitoring a tem...  
WO/2017/221123A1
The present disclosure provides methods and system for managing gust loading in an aircraft. A deflection angle of one or more spoilers of the aircraft is monitored. When the spoiler deflection angle is above a first threshold value, one...  
WO/2017/216691A1
Apparatus for improving flow characteristics around aircraft wings by obstructing air flow through an aperture formed in a wing skin for a movable duct or track are disclosed. In one embodiment, the apparatus comprises a substantially ri...  
WO/2017/212478A1
According to some examples of the presently disclosed subject matter, there is provided a nanosatellite, comprising: one or more panels configured for providing mechanical support to the nanosatellite; wherein at least one of the panels ...  
WO/2017/201267A1
Apparatus and method for actuating a double-slotted flap (26) movably coupled to an aircraft wing (12) are disclosed. An exemplary method comprises actuating a first panel (26A) of the double-slotted flap (26) relative to a structure of ...  
WO/2017/187300A1
Aircraft pitch control systems and methods are disclosed. An aircraft pitch control system (28) comprises a movable horizontal stabilizer (24) and an elevator (26) movably coupled to the horizontal stabilizer. The elevator is electronica...  
WO/2017/185121A1
The invention relates to an aerodynamic profiled body (1) for an aircraft, in particular a winglet, comprising a front profiled element (2) having a profile front edge (4a), a rear profiled element (3) having a profile rear edge (3a), an...  
WO/2017/180392A1
The modular aircraft system includes a single fuselage (10) having a permanently installed empennage (12) and plural sets of wing modules (46a, 46b, 66a, 66b, 68a, 68b) and engine modules (56, 60, 64), with each wing and engine module op...  
WO/2017/153393A1
The present invention relates to a device for attenuating the vortex wake generated in the tail section of an aircraft (100), the aircraft having at least one wing (108) and an afterbody (106) with an asymmetric cross-section that sharpl...  
WO/2017/155348A1
A vertical take-off and landing aircraft according to one embodiment may comprise: a wing; a power supply unit, disposed in the wing, for supplying power; a control unit, disposed in the wing, for controlling a flight mode; a rotor dispo...  
WO/2017/151225A1
A winglet (200) includes a winglet body (210) and a control body (220). The winglet body includes a first winglet surface (202) arranged opposite a second winglet surface (204). The second winglet surface is joined to the first winglet s...  
WO/2017/129536A1
The invention relates to an aircraft wing. The wing comprises a movable flap which is able to move in rotation relative to a fixed central body, flexible piping (40) and a rail (30) for guiding the movable flap and the flexible piping (4...  
WO/2017/114244A1
A single-shaft aerial vehicle. The single-shaft aerial vehicle comprises: a propeller (1), an aerial vehicle body (2), and a wing driver apparatus (3) constituting a portion of the aerial vehicle body (2). The aerial vehicle body (2) is ...  
WO/2017/066662A1
Disclosed is a technique for landing a drone using a parachute. The technique includes a parachute deployment system (PDS) that can deploy a parachute installed in a drone and land the drone safely. The parachute may be deployed automati...  
WO/2017/017333A1
The invention relates to an aerobraking device (20) for a man-made satellite from an atmospheric planet, including at least one aerobraking sail (25) connected to at least one propellant tank (21) so as to be unfurled by an inflation gas...  
WO/2016/203255A1
An aircraft wing system and method comprising: an aircraft wing (102); an edge device (200) coupled to a leading edge or trailing edge of the aircraft wing (102); a drive shaft (804) rotatable about its axis; a crank arm (808, 810), a fi...  
WO/2016/203256A1
An aircraft wing system and method comprising: an aircraft wing (102) including upper and lower surfaces, and a leading edge between the upper and lower surfaces; a fairing (200) coupled to the leading edge; and actuation means configure...  
WO/2016/199016A1
Systems, devices and methods a for use with one or more high-lift flight control surfaces (24) of aircraft are disclosed. One exemplary method comprises receiving data representative of a commanded configuration (48) for a high-lift flig...  
WO/2016/196967A2
A slat can assembly with a slat can body includes at least one full ply of a composite fiber sheet material and a plurality of elongated, unidirectional fiber ply strips that are arranged into the shape of the slat can body. At least som...  
WO/2016/196967A3
A slat can assembly with a slat can body (102) includes at least one full ply (208) of a composite fiber sheet material and a plurality of elongated, unidirectional fiber ply strips (210) that are arranged into the shape of the slat can ...  
WO/2016/189793A1
An aircraft flap 3 is equipped with: a flap body 8 which is provided so as to be deployable with respect to a main wing 2; and inclined portions 5 which are provided so as to protrude on the upper surface 301 of at least the end 40 on th...  
WO/2016/189994A1
[Problem] To reduce noise caused by a wing tip vortex of a wing in a flap or the like. [Solution] A flap 3 of an aircraft comprises: a flap body 8 provided in a deployable manner to a parent wing 2; and a vortex-creating part 50 having p...  
WO/2016/168879A1
A control surface element (1) for an aircraft, more particularly a spoiler, comprising an upper outer skin element (2) that has an outer air flow face (4); comprising a lower outer skin element (3); comprising at least one reinforcement ...  
WO/2016/154500A1
A three stage watercraft for operation in the water as a traditional boat at low speeds in stage one, for operation on the water's surface at mid-range speeds at stage two, and for traveling in ground effect at higher range speeds is dis...  
WO/2016/150561A1
Traction air device with multiple wing contours for a wind power generation plant and wind power generation plant comprising said air device.  
WO/2016/134366A1
A propeller (70) for an aircraft (20) having a fuselage (22) and a pair of fixed wings (50a, 50b) includes a mounting member (76) secured to at least one wing. At least one blade (72) is rotatably connected to each mounting member (76) a...  
WO/2016/125094A1
Apparatus for obstructing air flow through an aperture in an aircraft wing where a movable anti-icing duct extends through the aperture are disclosed. An exemplary apparatus comprises a base member (40) configured to be secured to the du...  
WO/2016/116102A1
The invention relates to a device of a safety system and/or resource and energy-efficiency improvement system for influencing the flow around an aero- or hydrodynamic body (3), preferably an aerofoil (3), according to the principle of a ...  
WO/2016/116719A1
The invention relates to a fixed-wing aircraft (10) comprising: - at least one passive landing assistance means capable of being deployed between a first position, used in normal flight, and a second position, used for emergencies; and -...  
WO/2016/094527A1
An aircraft (10), a control surface arrangement (14), and a method of assembling an aircraft are disclosed herein. In an exemplary embodiment, the aircraft includes, but is not limited to, an airframe (12), a control surface (16), and a ...  
WO/2016/079743A1
A pressurized, fluid-filled channel network embedded in an elastic structure, asymmetrically to the neutral plane, is used to create a deformation field within the structure by the pressurization of the embedded fluidic network, which ca...  
WO/2016/065509A1
A steering engine assembly structure, arranged between a carbon tube (10) and an electric motor system (30), and comprising a first bracket (41), a metal shaft (43), a tube clamp (45), a second bracket (47), and a steering engine (49); t...  
WO/2016/055964A1
A process for assembling aircraft control surfaces (1, 1'), in particular high-lift devices and wing portions, allows implementing smooth control surfaces in short times, wherein the control surface is defined by an upper skin (2) and by...  
WO/2016/054137A1
An aircraft includes an airframe having an empennage, a counter rotating, coaxial main rotor assembly located at the airframe including an upper rotor assembly and a lower rotor assembly, and a translational thrust system positioned at t...  
WO/2016/023056A1
The invention relates to a control surface element (4) for an airplane, in particular a spoiler, comprising a composite fiber element (3) that has a surface (8) around which air flows, a mounting device (5) for movably mounting the compo...  
WO/2016/022011A1
The invention relates to aviation equipment An object of this invention is to develop a new aerodynamic device which can extend the range of aerodynamic devices for aviation, increase the efficiency of the air flow power use, increase th...  
WO/2016/018477A1
Method and apparatus for controlling a shape of a composite structure. A shape memory structure associated with the composite structure is activated. The shape memory structure changes from a buckled shape to an original shape and causes...  
WO/2016/003580A1
An aerial vehicle including a fuselage, a main wing attached to the fuselage, a support structure extending upwardly from the fuselage and having a front surface facing the main wing, an overhang positioned on a top of the support struct...  
WO/2015/190124A1
Provided is a morphing wing capable of greatly deforming the wing as a whole through a lightweight and simple mechanism without accompanying increases in structural complexity and size, thereby achieving a high wing area increasing effec...  
WO/2015/183347A3
A new flap design for fixed wing aircraft increases stability and performance of the aircraft through a wide range of air speeds and flight dynamics when implemented on the flap of a fixed wing aircraft. The flap comprises a step configu...  
WO/2015/172869A1
The invention relates to a high-load gearing for a high-lift support (21) of an aircraft, wherein the high-load gearing comprises two outer segments (11) that cannot be rotated in relation to each other and an inner segment (12) that can...  
WO/2015/156857A3
The present disclosure is generally directed to a composite trailing edge control surface (600) including a contiguous one-piece composite control surface skin (200) wrapped around a plurality of stiffening cores (300), a plurality of hi...  
WO/2015/139416A1
The present invention provides a recess filling slat for an airplane wing, comprising: a deployable leading edge slat; and at least one recess filling element, movable between an internal folding position of the deployable leading edge s...  
WO/2015/119933A1
A gust alleviating aircraft wing includes a gust alleviating wing portion on the wing. The wing portion can have a leading edge, a trailing edge, and a downwardly sloping upper surface therebetween. At least one air passageway can extend...  
WO/2015/112039A1
´╗┐The claimed invention relates to aviation and in particular concerns aeroplanes. In one of the possible variants of embodiment thereof, in a single-seat aeroplane variant, the claimed invention has a wing, a canard (with the possibili...  
WO/2015/065551A1
An aircraft includes a wing. The wing includes an aileron pivotally connected to a trailing edge of the wing, and a Lam aileron pivotally connected to the trailing edge of the wing. The aircraft includes a motor connected to the Lam aile...  
WO/2015/021175A3
A hinged component includes first and second portions of material coupled together by a composite live hinge. The live hinge includes a layer of tensile fabric and a layer of elastomer interposed between the tensile fabric and the materi...  
WO/2015/021175A8
A hinged component includes first and second portions of material coupled together by a composite live hinge. The live hinge includes a layer of tensile fabric and a layer of elastomer interposed between the tensile fabric and the materi...  

Matches 1 - 50 out of 1,069