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WO/2023/160824A1 |
An aircraft that is certifiable for freighter transport is disclosed herein. The aircraft can include a hybrid fuselage including a plurality of modular sections, wherein the plurality of modular sections includes a first section, a seco...
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WO/2023/155908A1 |
An aircraft having passive safety performance and comprising an aircraft body, and a layout and an operation method of the aircraft. The aircraft comprises a fuselage (1); the fuselage comprises a cabin (2) and an anti-collision energy-a...
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WO/2023/152256A1 |
The invention relates to a glazed assembly (100) for an aircraft, the glazed assembly comprising a laminated glazing unit (110) having a first structural ply (111) and a second structural ply (113) bonded to the first structural ply by m...
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WO/2023/149391A1 |
The present invention addresses the problem of providing a rotary wing that is excellent in light weight, rigidity, fatigue characteristics, and dimensional accuracy, and in particular, has excellent fatigue characteristics, that is, dur...
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WO/2023/149830A1 |
The present invention relates to a method for remotely and/or autonomously harvesting a tree from air. The method comprises detecting by at least one sensor on a UAV (100) a tree to be harvested, positioning a harvesting tool (105) compr...
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WO/2023/146498A1 |
The present invention relates to a collapsible carriage and release system that enables the transport of munition for unmanned aerial vehicles.
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WO/2023/142769A1 |
An aircraft, comprising a housing, wherein an inner cavity is formed in the housing, a driving mechanism (3) and a control unit (4) are provided in the inner cavity, and a camera assembly (2) is provided in the housing; an air inlet (215...
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WO/2023/142702A1 |
A locking device and an unmanned aerial vehicle. The locking device is used for a wing and a fuselage of an unmanned aerial vehicle, and the locking device comprises at least two first connection members (1, 3) and at least two correspon...
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WO/2023/144481A1 |
The invention relates to a system (4) for controlling the speed of opening a sliding door for an aircraft comprising a mechanical braking device (5) for the door having a transmission shaft (9) and a centrifugal absorber (19) having a re...
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WO/2023/137080A1 |
A method for creating local and controlled frangible areas in composites, comprising: creating an area in a composite component comprised of composite material, the area configured to receive a fastener with a composite thickness that is...
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WO/2023/135387A1 |
The invention relates to laminated glazing unit comprising a glass sheet (1), the border of which is set back relative to that of a structural block (3, 4, 5), the edge of the glass sheet (1) and the edge of the adhesive interlayer (2) b...
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WO/2023/135388A1 |
The system for controlling the speed of movement of a sliding door for an aircraft comprises an electromagnetic braking means for braking the door having a transmission shaft (8) and electromagnetic resistive means (18). The resistive me...
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WO/2023/124124A1 |
A method for controlling a deformable rolling aircraft. The method comprises the following steps: after a control system receives a starting signal, a driving device (5) driving a rotor wing to rotate, and the rotor wing generating a lif...
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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...
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WO/2023/117425A1 |
The invention relates to a mechanical drive connection assembly (1) for driving in rotation a carrier shaft (2) of a structure rotating about a central axis (2a) passing through this carrier shaft (2). This connection (1) comprises at le...
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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...
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WO/2023/122109A1 |
An aircraft has port side and starboard side propeller blades that each have a portion of the blade hidden or overlapping with the fuselage. This hidden or overlapping blade may extend into a slot of the fuselage. The advancing or retrea...
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WO/2023/093803A1 |
A trimming-type tailplane connection structure (100), comprising: a tailplane upper mounting frame (111) and a tailplane lower mounting frame (112), the tailplane upper mounting frame (111) and the tailplane lower mounting frame (112) be...
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WO/2023/094454A1 |
The present invention discloses a vacuum infusion system for infusing a fibre reinforcement with a resin comprising: a mould having a mould cavity comprising at least one moulding element for the reception of a fibre reinforcement, the s...
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WO/2023/094746A1 |
The invention relates to a laminated glazing comprising a first outer glass sheet (1) and a second sheet (3), an adhesive layer (2), the edge of the sheet (1) being set back with respect to that of the sheet (3), a portion of the free su...
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WO/2023/095022A1 |
In an aircraft component where the aircraft component comprises a metal sheet (1.1, 1.2, 1.3, 1.4, 1.5, 1.6), the metal sheet (1.1, 1.2, 1.3, 1.4, 1.5, 1.6) comprises a normal region (5.1, 5.2, 5.3, 5.4) and a first surface milling regio...
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WO/2023/094289A1 |
An aircraft door (1) with lateral escape of the stops and opening by circular translation being provided with a pivoting manoeuvring arm (2) coupled to a forearm (3) articulated on the door and a mechanism for locking at least one actuat...
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WO/2023/087602A1 |
A detachable fixed-wing unmanned aerial vehicle (UAV), the UAV comprising: a body, an end plate (20), a first wing (31) and a second wing (32), wherein: one side of the body is connected to the first wing (31), the other side of the body...
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WO/2023/089273A1 |
The invention relates to an open composite panel (10), comprising: - a composite skin (12) having an inner surface (18) and an outer surface (16), - a plurality of stiffening ribs (14), each rib (14) extending over the inner surface (18)...
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WO/2023/085198A1 |
The present invention provides a blade in which the specific rigidity of a flap part is further increased. This blade has a thick body part and a thin flap part integrally formed in the rear end of the body part. The flap part has a skin...
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WO/2023/083642A1 |
The invention relates to a method for producing a stiffened one-piece composite structure comprising a panel (2a) and at least one stiffener which are draped in fibres by resin infusion in an infusion tool (1) that performs shaping of th...
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WO/2023/079492A1 |
This disclosure describes an information display system for an electric or hybrid aircraft, comprising:a first, programmable component monitoring subsystem; a second, non-programmable component monitoring subsystem;a first information di...
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WO/2023/077677A1 |
Disclosed in the present application are a communication device, a platform system, an electrical connection assembly, and a connection unit. The communication device is communicatively connected to a mobile platform, so that the mobile ...
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WO/2023/073153A1 |
The invention relates to a decompression lock (10) having a bolt, that comprises at least two separately formed bolt elements (12, 36), wherein a first bolt element (12) has a bolt head (14) and a second bolt element (36) has a connectin...
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WO/2023/067339A1 |
A VTOL aerial vehicle (10) is disclosed, comprising: an airframe (12); one or more arms (202) coupled to the airframe (12) at a pivot (206); and three or more propulsion units, each mounted on a gimbal (16) having a gimbal axis, and each...
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WO/2023/066030A1 |
The present application provides an unmanned aerial vehicle (UAV) surface coating, a preparation method therefor, and a UAV. The coating at least comprises: an adhesive layer, an anti-oxidation layer, an oxygen barrier transmission layer...
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WO/2023/062912A1 |
Provided are a cable protection member advantageous for making cable protection work efficient and an aircraft lavatory unit equipped with the cable protection member advantageous for making the protection work of a cable used in the air...
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WO/2023/061897A1 |
A dispersion system (10) for a vehicle (1) is described, wherein the vehicle has at least one door opening (5). The dispersion system comprises at least two tank modules (100) including a reservoir (110) for storing a medium to be disper...
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WO/2023/062611A1 |
Disclosed is a multicopter foldable between a stowed state and an operational state, the multicopter comprising a hub configured to receive one or more payloads and a battery, two or more flight arms that extend substantially horizontall...
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WO/2023/052690A1 |
The invention relates to an aircraft window consisting of an inner panel (1) and an outer panel (2) which are separated by a layer of air (3) and by an installation seal (4) into which a peripheral portion of the window is set, the inner...
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WO/2023/055868A1 |
A thermal management system is provided. The thermal management system includes a housing extending between a leading end and a trailing end. The housing includes a cooling structure defining at least one inlet, at least one outlet, and ...
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WO/2023/053870A1 |
[Problem] To provide a fan blade, an engine, and a structure with anti-icing and de-icing functions, having a simple structure and capable of efficiently carrying out anti-icing and de-icing. [Solution] Provided is a fan blade arranged o...
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WO/2023/051463A1 |
Embodiments of the utility model relate to the technical field of unmanned aerial vehicles, and in particular, disclosed is an unmanned aerial vehicle. The unmanned aerial vehicle comprises a fuselage, comprising an upper housing and a h...
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WO/2023/047270A1 |
An aircraft window configured to reduce the intensity of vibrations transmitted from outside the aircraft to inside the aircraft cabin comprising: a first element of transparent material (2) arranged, in use, facing the outside of the ai...
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WO/2023/046098A1 |
An unmanned aerial vehicle (1). The unmanned aerial vehicle (1) comprises: a fuselage (10); arms (20), wherein one end of each of the arms (20) is connected to the fuselage (10); a drive device (30), which is mounted at the other end of ...
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WO/2023/044821A1 |
A multi-rotor unmanned aerial vehicle (100). The multi-rotor unmanned aerial vehicle (100) comprises a fuselage (10) and arms (30). The roots of the arms (30) are connected to the fuselage (10); a protrusion (31) is provided on the front...
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WO/2022/182644A9 |
A payload unit known as an Organizational box (OB) may comprise one or multiple units of cassettes. The OB may be connected to a drone, an autonomous vehicle, or a standalone unit, where each cassette can hold one or multiple parcels and...
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WO/2023/035236A1 |
A frame for an unmanned aerial vehicle, an unmanned aerial vehicle, and a kit. The frame for an unmanned aerial vehicle comprises a body and an engine arm, which is connected to the body, wherein the engine arm is used to bear a power as...
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WO/2023/038196A1 |
The present invention relates to a distance surveying drone that is easy to level off according to the movement of a survey means, comprising: a drone body capable of level hovering flight through a built-in sensor module; a horizontal g...
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WO/2023/034095A1 |
An unmanned aerial vehicle (UAV) includes a fuselage assembly, a further portion that attaches with the fuselage assembly, and a propulsion assembly coupled with the further portion. The propulsion assembly is constructed and arranged to...
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WO/2023/033246A1 |
The present invention relates to a stitched electromagnetic wave absorbing composite material for low-speed impact protection and, in particular, to a composite material that exhibits electromagnetic wave absorption performance and at th...
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WO/2023/033758A1 |
The present invention relates to unmanned aerial vehicles (1) that operate more efficiently by connecting to a power station on the ground or in a vehicle and supplying compressed air from the relevant stations. Fuel and energy is saved ...
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WO/2023/023828A1 |
The present invention relates to an innovative type of electric and/or hybrid digital glider drone with a steerable balloon for personal flight. The project consists of a compact ellipsoidal balloon with a self-levelling drone with rigid...
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WO/2023/026662A1 |
The present invention provides a skin member and a blade structure which are lightweight yet ensure strength. A skin member (100) forms an outer plate of the blade structure, and comprises: a lattice-like framework material (110) forming...
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WO/2023/027773A1 |
A case for carrying loads by an Unmanned Aerial Vehicle (UAV) comprises a first end comprising a first cap and a first opening and a second end comprising a second cap and a second opening, the second opening being smaller than the first...
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