| Document |
Document Title |
|
WO/2024/074662A1 |
The invention relates to a method (100) for producing a spar cap for a rotor blade of a wind turbine, said method comprising the steps of: - Providing (110) a plurality of pultruded planks, said pultruded planks being a thermoplastic com...
|
|
WO/2024/074822A1 |
In some examples, a wing for an aircraft, the wing having a passive variable aeroelastic geometry for accommodating efficient flight at multiple aircraft speeds, comprises a wing skin comprising a composite structure comprising a laminat...
|
|
WO/2024/074543A1 |
Vertical take-off and landing aircraft (1) comprising a fuselage (2), at least one propulsion system (5), at least four lift propellers (10) and at least two fixed wing planes (20, 30, 40). The fixed wing planes (30, 40) which are locate...
|
|
WO/2024/068661A1 |
A control unit (6, 7) is indicated for controlling the pitch of an aircraft (1), the control unit (6, 7) comprising at least one adjustable control element (6) and an adjustment mechanism (7) for actively adjusting the at least one contr...
|
|
WO/2024/069210A1 |
The present invention concerns a method of manoeuvring a vertical take-off and landing, unmanned aerial drone (100) comprising at least an aerodynamic surface (101), wherein, during a flight of the drone, the aerodynamic surface generate...
|
|
WO/2024/060585A1 |
The present invention relates to a wing system integrated with a power battery module. The wing system comprises: a wing box, the wing box comprising a plurality of wing support members, and the plurality of wing support members being co...
|
|
WO/2024/060633A1 |
An aircraft wing (10) having an integrated distributed ducted fan, the aircraft wing (10) being attached to a fuselage (20) and being provided with a ducted fan power set (30), wherein the ducted fan power set (30) is provided on an inbo...
|
|
WO/2024/054197A1 |
The invention relates to space engineering and can be used in the creation of a suborbital rocket plane with substantially vertical takeoff and landing. A rocket plane comprises a body (1), movable front and rear aerodynamic control surf...
|
|
WO/2024/052505A1 |
The invention relates to a wing arrangement (10) that comprises a main wing (12) and a slat (14) mounted to the main wing in front of the main wing (12) and counter to a direction of flow. A gap (16) with a flow inlet (18) and a flow out...
|
|
WO/2024/054195A1 |
A closed-wing vertical take-off and landing aircraft comprising: a fuselage (1); a tail unit comprising two angularly inclined stabilizers (12); and a closed wing, comprising a front wing formed by two planes (2) mounted to the fuselage ...
|
|
WO/2024/037875A1 |
The invention relates to a pivoting wing (1) for an aircraft (13), characterised in that the pivoting wing (1) is designed as a partial profile pivoting wing, wherein the partial profile pivoting wing is assembled from individual partial...
|
|
WO/2024/035451A1 |
A method includes obtaining (402) thermal energy from a structure (112) to be cooled, where the structure includes micro-channels (208). The method also includes providing (402) the thermal energy to a water-based polymer network (206), ...
|
|
WO/2024/032907A1 |
An electric vertical take-off and landing aircraft comprises a fuselage (1) and a tilt wing (7). The tilt wing (7) is tiltable relative to the fuselage (1) in a range of tilt wing angles. Control surfaces (13) are arranged at the tilt wi...
|
|
WO/2024/028710A1 |
The present disclosure provides an aerofoil profile (200) for an aerodynamic element such as a wing, turbine blade, fin, etc. that facilitates the aerodynamic element to keep the boundary layer attached to its top surface with increasing...
|
|
WO/2024/018362A1 |
An improved aircraft wing (400) is disclosed that includes a plurality of blades 404 configured on an underside of the airfoils section 402 of the wing (400). The blades 404 are configured to move between a deployed position, in which th...
|
|
WO/2024/017419A1 |
The invention discloses a bionic folding fixed wing household small manned aircraft, which comprises a bionic folding fixed wing flight system, cabin, chassis, etc. The bionic folding fixed wing system comprises a fixed wing skeleton, a ...
|
|
WO/2024/012942A1 |
The present invention relates to an adjustable guide bushing (10) comprising a first bushing (20) with a first eccentric opening (30) and a second bushing (40) with a second eccentric opening (50), wherein the first bushing (20) is accom...
|
|
WO/2024/015588A1 |
A laminate material for an aircraft component is provided. The laminate material includes a first layer, a second layer and a rib disposed between the first and second layer. One or more connectors are configured to couple the ends of th...
|
|
WO/2024/007564A1 |
A modular flight automobile, comprising an automobile body and a vehicle-mounted aircraft, wherein the vehicle-mounted aircraft can take off from and land on the automobile body; and the vehicle-mounted aircraft comprises a cockpit, and ...
|
|
WO/2024/010834A1 |
A vertical take-off and landing aircraft with a multi-element lifting system with integrated propulsion. The multi-element lifting system may have an upper wing element, a lower wing element, and a control wing element which is located b...
|
|
WO/2024/003642A1 |
A ducted wing is configured to be connected to an aircraft. The ducted wing includes an array of integrated jetfoils. Each jetfoil includes a propulsor fan, an upper wing portion, and a lower wing portion that extends past an end of the ...
|
|
WO/2024/006078A1 |
Systems and methods for protecting an aerodynamic structure, e.g., a wind turbine blade, rotor blade, aerodynamic aerostructure, etc., are provided. Long fiber reinforced composites having a helicoidal architecture with material aligned ...
|
|
WO/2023/242858A1 |
The present invention discloses wing (100) having improved aerodynamic performance characteristics. The wing (100) with an airfoil section (102), which may be symmetric/cambered comprises an external skin (104) attached to a leading edge...
|
|
WO/2023/241790A1 |
The invention is notably directed to an aircraft (10), which includes an aircraft structure (20), a thermal exchange system, a thermal insulation material (26), and fasteners (32, 35). The thermal exchange system includes a fluid-based c...
|
|
WO/2023/243802A1 |
The present invention relates to a flying car capable of vertical takeoff and landing on the ground/water. The flying car capable of vertical takeoff and landing on the ground/water, according to an embodiment of the present invention, c...
|
|
WO/2023/242564A1 |
An aircraft assembly comprising: a rib (10) of a wing; an aperture (11) in the rib; a pipe assembly (30a, 30b) extending through the aperture, the pipe assembly comprising a first rigid pipe section (30a), a second rigid pipe section (30...
|
|
WO/2023/238289A1 |
[Problem] To provide a VTOL aircraft capable of improved flight efficiency and preventing a reduction in takeoff and landing performance. [Solution] A VTOL aircraft 100 comprising a main wing 21, a first rotary wing part 11, and a second...
|
|
WO/2023/233857A1 |
A control device according to an embodiment of the present invention controls a user-wearable flight device and comprises a processing unit that acquires state data related to the state of the flight device and manipulation data related ...
|
|
WO/2023/221310A1 |
Disclosed in the present invention are a wing, and a method for improving the control efficiency of a rudder by means of air blowing. In the technical solution of the present invention, an original symmetrical airfoil rudder is deformed ...
|
|
WO/2023/208887A1 |
An aeronautical vehicle (1) performs horizontal flight and/or vertical flight, and has a fuselage (2), a wing assembly (3) having a first wing part (3a) and a second wing part (3b) rigidly coupled to one another, a rotor assembly (4), a ...
|
|
WO/2023/203475A1 |
The invention concerns an airfoil (40) comprising a front leading edge le, a rear trailing edge te, a mean line ml and a thickness t. The airfoil further comprises: a front portion (42) in which the thickness increases from the leading e...
|
|
WO/2023/198267A1 |
An aerodynamic profile for an aircraft, comprises a core (6, 7, 8) made of foam, a skin (11, 12) defining an outer surface of the wing and cloths (14) forming spars and/or ribs. The profile a wing, a canard, a horizontal stabiliser, a ve...
|
|
WO/2023/200852A1 |
Principles described herein allow for wings to be optimized for aerodynamic and structural efficiency while reducing planform compromises required to address wing tip stall problems. All-moving outboard wings allow the outboard wing loca...
|
|
WO/2023/192087A1 |
A drone with extendable and rotatable wings and a multiple accessory securing panel is provided. The extendable wings help increase the lift of the drone and reduce the air drag on the drone. The multiple accessory securing panel allows ...
|
|
WO/2023/180449A1 |
The invention relates to a vehicle, which can be used either as an aircraft or ground effect vehicle or as an aircraft and ground effect vehicle, comprising a fuselage (4) and at least two front wings (2), wherein the fuselage (4), when ...
|
|
WO/2023/177774A1 |
A vehicle for travelling on a road and in the air is provided, comprising a fuselage extending from a forward to a rear end along a horizontal longitudinal roll axis, a pair of main wings mounted on the rear end of the fuselage, a pair o...
|
|
WO/2023/168623A1 |
Provided are an unmanned aerial vehicle base station (100) and an unmanned aerial vehicle system. The unmanned aerial vehicle base station (100) comprises a base body (10), a landing pad (20) arranged on the base body (10), and a base st...
|
|
WO/2023/159304A1 |
A personal flying apparatus comprising a body structure adapted to support and detachably couple a user thereto; and a pair of wings rotationally coupled to opposite sides of the body structure and powered by a battery, the body structur...
|
|
WO/2023/155498A1 |
A self-charging tail-sitter unmanned aerial vehicle adapted to a launcher. The structure of the unmanned aerial vehicle comprises: a head propeller (1), a propeller driving motor (2), foldable wings (6), a wing actuating motor (5), a fus...
|
|
WO/2023/152746A1 |
An aircraft, comprising: a fuselage; two wings mounted to the sides of the fuselage, extending laterally; a pusher propeller, statically mounted to the fuselage, wherein a rotational axis of the pusher propeller is parallel to a longitud...
|
|
WO/2023/126919A1 |
A VTOL-type air vehicle is transitioned from forward speed mode to hover mode via a transient path in transition mode. The air vehicle includes first and second propulsion systems, and high lift, mild stall fixed wings. The first propuls...
|
|
WO/2023/126041A1 |
In a first aspect of the present invention there is provided a wind turbine comprising a tower, a nacelle mounted on the tower, and a rotor mounted to the nacelle. The rotor comprises a hub and at least three pitchable wind turbine blade...
|
|
WO/2023/122145A1 |
Additive manufactured airframe (10) structure having a plurality of additive manufactured airframe segments (30) operable to be linked together in an assembled direction (40). Each of the plurality of additive manufactured airframe segme...
|
|
WO/2023/122717A1 |
A method of operating an aircraft including takeoff of an aircraft; transitioning the aircraft to a forward flight configuration by increasing an amount of forward propulsive force generated by a propeller assembly from equal to or less ...
|
|
WO/2023/121784A2 |
A tiltrotor aircraft comprising a wing carrying an engine on each wing half, and a fuselage-mounted third engine with a transmission system configured to drive each of the tilting rotors from the third engine. The engines may be any powe...
|
|
WO/2023/121436A1 |
Vertical take-off and landing (VTOL) aircraft of the fixed-wing type, comprising a centre section defining a centreline of the aircraft, and a pair of wings, arranged on either side of the centre section, wherein the wings extend longitu...
|
|
WO/2023/109154A1 |
Disclosed are a wing and a method for improving control efficiency of a two-dimensional airfoil rudder surface. According to the technical solution, an original symmetric airfoil rudder surface is transformed into an asymmetric airfoil r...
|
|
WO/2023/109114A1 |
Disclosed in the present invention is a reconstructable flying car. A car body main body is detachably connected to a wing assembly, a propulsion assembly, an empennage assembly, and multi-axis rotor assemblies by means of a connecting m...
|
|
WO/2023/104323A1 |
The present invention relates to an airfoil comprising a leading edge flap (210) providing a rigid leading edge surface profile contour (212); a central lifting section (220) aft of the rigid leading edge flap (210); a bottom side (208) ...
|
|
WO/2023/099117A1 |
The invention relates to a device comprising an asymmetrical wing profile (2) and an adjusting device (15), which asymmetrical wing profile (2) has a profile thickness (q) and a profile chord (p) extending between a wing leading edge (n)...
|
