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Matches 1 - 50 out of 1,102

Document Document Title
WO/2018/217667A1
Apparatus, systems, and methods are contemplated for electric powered vertical takeoff and landing (eVTOL) aircraft. Such are craft are engineered to carry safely carry at least 500 pounds (approx. 227 kg) using a few (e.g., 2-4) rotors,...  
WO/2018/211233A1
A structural assembly (900) and method of fabricating the same, the method comprising: providing a first member (204) comprising a bond surface (800) and a plurality of protrusions (802) extending from the bond surface (800), a length of...  
WO/2018/211232A1
A stiffening structure for an aircraft panel or door and method for fabricating the same, the method comprising: providing a thermoplastic continuous fibre-reinforced composite material comprising a plurality of continuous fibres embedde...  
WO/2018/197265A1
The present invention relates to a wing(2) for an aircraft, comprising: a main wing (4) having an outer skin (6) defining an interior space (8) of the main wing, a slat (10), and a connection assembly (12) for movably connecting the slat...  
WO/2018/197649A1
The present invention relates to a wing (3, see Fig.1) for an aircraft (1, see Fig.1), comprising a main wing (5, see Fig.1), a slat (7, see Fig.1), and a connection assembly (9, see Fig.1) movable connecting the slat (7, see Fig.1) to t...  
WO/2018/145675A1
Tail sitter aircraft, comprising a fuselage (4) and a pair of wings (5), each wing having a leading edge (50) and a trailing edge (55), wherein each of the wings (5) is provided with a propeller propulsion unit and a plurality of control...  
WO/2018/145173A1
A device (10) for adjusting the control surfaces (40) of an aircraft (50) is described, comprising an elongate structural body (20) formed by a base (201) arranged on a first end (22) and attached to the structure of the aircraft (50) an...  
WO/2018/144915A1
A system and method for resisting an uncontrolled descent or uncontrolled flight condition of an aerial vehicle. The system includes a control system, sensors, an inflation device, and a descent-restraint system. The control system detec...  
WO/2018/138034A1
The invention relates to an assembly (20) for an aircraft comprising a fuselage portion (5a) of the aircraft and an adjacent movable trailing edge flap (16), the flap comprising an inner end secured to an actuation shaft (22) for the fla...  
WO/2018/134756A1
The invention relates to an aircraft having a tailless fuselage. The fuselage has a body which includes a transverse trailing edge. The aircraft further includes a wing having two sides which protrude from opposite sides of the fuselage....  
WO/2018/109582A1
A slat (50) for an aircraft wing comprises a leading edge (51) defining a leading edge line (61), a trailing edge (52) defining a trailing edge line (62), the leading and trailing edges line defining a slat plane, the chord distance (69)...  
WO/2018/111488A1
An aircraft including a wing system, a plurality of control surfaces, a camera mounted on a camera pod, and a control system. The camera pod is configured to vary the orientation of the camera field of view only in yaw, relative to the a...  
WO/2018/104251A1
An aircraft wing assembly (5) is presented comprising a main wing portion (21), a high-lift device (9) comprising a flow surface with an upper skin portion (25) and a lower skin portion (27), wherein the high-lift device is movable betwe...  
WO/2018/098993A1
Disclosed are a dual-axis vector servo steering device for a propeller and a vertical take-off and landing of an unmanned aerial vehicle with fixed wings. The dual-axis vector servo steering device comprises a fixed steering engine fixed...  
WO/2018/089583A1
Systems, devices, and methods for an extruded wing protection and control surface (126) comprising: a channel (206) proximate a leading edge (202) of the control surface, a knuckle (210) disposed about the channel, a leading void (212), ...  
WO/2018/083077A1
The present invention is concerned with actuating aircraft components to tailor their configuration to achieve improved performance in one or more flight phases. In general terms, the invention provides a method and system for actuating ...  
WO/2018/083145A1
The invention relates to an aircraft wing comprising a mobile trailing edge flap (16), the wing comprising a device (50) for moving said flap, the device being provided with: a beam (51) supporting a guide rail; a carriage (52a) movably ...  
WO/2018/083144A1
The invention relates to an aircraft wing comprising a stationary central wing body as well as at least one mobile leading edge flap (16) intended for being moved relative to the stationary central body between an extended position and a...  
WO/2018/059991A1
A system for driving and guiding of a trailing edge control surface (24) arranged on a trailing edge region (6) of a wing (2) of an aircraft comprises a first guide device (9) attachable to the wing (2) and coupled with the control surfa...  
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 -...  

Matches 1 - 50 out of 1,102