| Document |
Document Title |
|
WO/2022/040858A1 |
The present invention relates to the technical field of unmanned aerial vehicles, in particular to an anti-collision unmanned aerial vehicle for aerial photography and a method therefor. Aimed at the problems of an existing unmanned aeri...
|
|
WO/2022/041097A1 |
An unmanned aerial vehicle foot rest folding and unfolding device, comprising a vehicle body (1). A placement groove (2) is arranged at the bottom of the vehicle body (1). Four symmetrically arranged positioning seats (3) are fixedly mou...
|
|
WO/2022/043984A1 |
There are provided examples of an enhanced cargo capacity aircraft, converted from a datum aircraft. The enhanced cargo capacity aircraft includes the datum aircraft and a cargo module. The datum aircraft includes at least a fuselage hav...
|
|
WO/2022/046660A1 |
The present embodiments are directed to an aerial flying unit. The aerial flying unit can include a modular mechanical platform. The modular mechanical platform can include a frame. The flying unit can include a plurality of multiple-rot...
|
|
WO/2022/041882A1 |
An unmanned aerial vehicle, comprising a nose area (1), a tail area (2), a battery compartment (3), a gimbal camera module (6), a sensor module (23), a battery (7), and two arms (8). A battery compartment (3) is formed between the nose a...
|
|
WO/2022/038382A1 |
A light helicopter typically for 5 occupants is disclosed which achieves a hitherto unprecedented combination of range, speed and payload by adopting a novel approach to construction and positioning of components which affect overall aer...
|
|
WO/2022/036732A1 |
A telescopic device (10) and an unmanned aerial vehicle (100) applying the telescopic device. The telescopic device comprises a driving mechanism (1), a linkage mechanism (2) and a plurality of telescopic arms (3); the plurality of teles...
|
|
WO/2022/036731A1 |
Disclosed are a scissor-type extendable device and an unmanned aerial vehicle using same. The scissor-type extendable device comprises a first extendable arm, a second extendable arm and a driving assembly, wherein the driving assembly i...
|
|
WO/2022/032181A1 |
A device may include a metallic substrate and a plurality of nanorod arrays arranged on the substrate. The nanorod arrays may be made of porous metallic nanostructures and may appear black in color.
|
|
WO/2022/023974A1 |
Process for manufacturing a structural component (1, 1', 1", 1"', 1"") made of composite material comprising a skin (2) and at least one stiffening stringer (3, 3', 3", 3"', 3"") applied rigidly and integrally to one face (2a) of the ski...
|
|
WO/2022/023402A1 |
Double-curved aircraft door comprising pairs of stops in contact over a contact area. The isobarycentre (31A) of each contact area of a first lateral edge is substantially arranged in a first plane perpendicular to the longitudinal axis ...
|
|
WO/2022/023975A1 |
Process for manufacturing a structural component (1, 1', 1", 1''', 1"" ) made of composite material comprising a skin (2) and at least one stiffening stringer (3, 3', 3", 3"', 3"") applied rigidly and integrally to one face (2a) of the s...
|
|
WO/2022/023212A1 |
A device for emergency opening of an aircraft door, comprising: - a tubular actuating member (7) which comprises a first end plate (8) and a second end plate (9); - elastic compression means which comprise a tubular spring (10) compresse...
|
|
WO/2022/017676A1 |
The present invention relates to a door system for a vehicle, in particular for a rail vehicle, comprising a door leaf that can be moved from a closed state to an open state and vice versa, with the features of claim 1. Compared to known...
|
|
WO/2022/013301A1 |
The invention relates to a method for retrofitting a passenger airplane (1), which is equipped with a passenger cabin (2) for transporting passengers, in order to temporarily transport freight. In the starting state, the passenger cabin ...
|
|
WO/2022/013299A1 |
The invention relates to a commercial aircraft designed for the transport of freight in the passenger cabin (1), container (20) designed therefor, an arrangement consisting of a corresponding commercial aircraft and container (20) and a ...
|
|
WO/2022/013512A1 |
Structure (19) intended to stiffen a component (22) made of thermosetting composite material by being fitted to at least one of its surfaces, comprising: - at least one longitudinal body (5), with a first and a second longitudinal edge f...
|
|
WO/2022/013298A1 |
The invention relates to a cargo bridge (10) for simplified introduction of cargo into the passenger cabin (1) of a commercial aircraft through the door opening (5) of a passenger door (4) that opens outwards to the side, which door is f...
|
|
WO/2022/010688A1 |
A modular flat-packable drone kit includes a plurality of components that can be assembled into a drone. Components of the drone kit include elements that may be cut from a flat sheet of material, thereby enabling low cost manufacturing ...
|
|
WO/2022/008365A1 |
A remote-controlled unmanned aircraft comprising at least two motors (5) configured to allow the aircraft to fly, and one main structure (2) for supporting the motors (5); the main structure (2) being flexible and inflatable such that th...
|
|
WO/2022/010679A1 |
A cockpit window panel that is easily installed and removed that reduces glare and heat and improves overall cockpit environment and pilot comfort. The panels include a clear polycarbonate sheet contoured to match an aircraft window, a b...
|
|
WO/2022/003464A1 |
A drone includes a frame and a fuselage. The fuselage is coupled to the frame extending away from the frame. The fuselage has a front panel and a bottom panel, and the front panel is positioned at an angle between the bottom surface of t...
|
|
WO/2022/002805A1 |
The invention relates to a method for manufacturing a beam (P1, P2) with closed section, the beam being produced by combining a first profile (P10, P20) and a second profile (P11, P21), characterised in that it comprises the following st...
|
|
WO/2022/003325A1 |
Disclosed is a portion of a vehicle (5) comprising occupant zones in rows. A first of the occupant zones (7) and a second of the occupant zones (9) are adjacent rows and the portion of the vehicle further comprises access points (23) arr...
|
|
WO/2022/004254A1 |
A sandwich panel (100) according to the present invention is provided with a core layer (10) that has a honeycomb structure, and a cured material (resin sheets (40)) of a prepreg (20) that is provided on both surfaces of the core layer (...
|
|
WO/2022/002804A1 |
Aircraft door designed to assume a first configuration and a second configuration, comprising a bistable mechanism biasing the aircraft door towards either the first or second configuration, the bistable mechanism comprising: - a first y...
|
|
WO/2021/261347A1 |
[Problem] To provide a flying object control device, method, and program for an automatic navigation vessel that navigates near a harbor. [Solution] The flying object control device of an embodiment of the present invention has: a calcul...
|
|
WO/2021/260497A1 |
The present invention relates to a protective foldable cage (100) adapted to flying drones. It comprises several ribs linked at their extremities by a ring and comprising on their length several connexion points allowing strings to join ...
|
|
WO/2021/256064A1 |
Provided are: a coating composition which retains excellent accreted ice and accreted snow removal capability and for which film damage is less likely to occur; a coating film; and a member having a coating film. Provided is a coating co...
|
|
WO/2021/248278A1 |
A locking member (1) and an unmanned aerial vehicle (100). The locking member (1) is used for fixedly connecting two mechanism parts. The locking member (1) comprises: a first lock cylinder (10) provided with a guide portion (11); and a ...
|
|
WO/2021/243502A1 |
An arm assembly and unmanned aerial vehicle. The arm assembly is used for a multi-rotor unmanned aerial vehicle, and the arm assembly (100) comprises: an arm (110), an arm frame (120) and a position-limiting member (130); the arm (110) i...
|
|
WO/2021/243867A1 |
The present invention relates to a manufacturing method for an aircraft bulkhead. The aircraft bulkhead is of an arc structure and comprises a Z-shaped cross section, and comprises a flanging area, bending areas, and a web area extending...
|
|
WO/2021/243705A1 |
A quadrotor unmanned aerial vehicle (100) and a multi-rotor unmanned aerial vehicle (200). The quadrotor unmanned aerial vehicle (100) comprises a central body (10), two first arms (20), two second arms (30), four power assemblies (50), ...
|
|
WO/2021/232359A1 |
Disclosed is a control method, comprising: acquiring echo energy and location information corresponding to each of a plurality of scanned points obtained by scanning the environment by a radar (630) of a movable platform; acquiring a con...
|
|
WO/2021/236753A1 |
The present technology is directed to an unmanned aerial vehicle (UAV) a wing. The UAV can include first and second propellers extending from a front portion of the wing and positioned to provide thrust to the UAV. The UAV can include a ...
|
|
WO/2021/236047A1 |
The UAV structural elements quick release fastening system, which include at least two tail booms coupling with a center wing section / fuselage of a UAV and a tail assembly by at least two quick release coupling elements from center win...
|
|
WO/2021/230957A1 |
An aerial vehicle with a plurality of selectively collapsible arms capable of transitioning between an extended state and a contracted state is described. In the extended position, the distance between the main body of the vehicle and th...
|
|
WO/2021/225366A1 |
The present invention relates to a multicopter comprising: a main body portion; wing portions each having one end portion connected to the main body portion and the other end portion to which a propeller assembly is connected; a folding ...
|
|
WO/2021/224844A1 |
A method of realization of an aeronautical item with hybrid composite materials by means of additive technology comprising the steps of: design of the product by means of a three-dimensional mathematical model which defines, in a referen...
|
|
WO/2021/224207A1 |
The invention relates to a method for producing an arc-shaped fibre composite component. A preform with a flat fibre layer arrangement along an arc is formed, the arrangement having an outer edge associated with a convex outer side of th...
|
|
WO/2021/222796A1 |
A dual use UAV or "drone" can include a battery and primary processor located at a fuselage, as well as two separate modular units removably coupled to the fuselage and in communication with the primary processor. The two separate modula...
|
|
WO/2021/220390A1 |
[Problem] To provide a frame assembly for an unmanned aircraft which is light, capable of being reduced in size, and inexpensive to produce, and an unmanned aircraft provided with said frame assembly. [Solution] A frame assembly 60 (61) ...
|
|
WO/2021/214445A1 |
A door assembly for a payload bay (10) having an opening (12), the door assembly comprising at least one door (20, 220). The at least one door comprises: a panel section (22, 222) having a first end (24, 224) and a second end (26, 226); ...
|
|
WO/2021/212633A1 |
An unmanned aerial vehicle undercarriage, and an unmanned aerial vehicle. The unmanned aerial vehicle undercarriage comprises an undercarriage body and a reader antenna; the reader antenna is arranged in the undercarriage body; the under...
|
|
WO/2021/213733A1 |
The invention relates to a method for operating a flying object (10), more particularly a battery-operated flying object (10), and to a corresponding flying object (10), comprising at least one battery system (12) and at least one at lea...
|
|
WO/2021/213860A1 |
The invention relates to a method for producing a large component of a vehicle body by way of integral construction, wherein the large component is constructed from a plurality of lightweight metal profiles (1) which are non-releasably c...
|
|
WO/2021/209372A1 |
Method for manufacturing an aircraft door having a monolithic structure, comprising the following steps: - producing a forged blank (7); - die-cutting the forged blank (7) between a substantially smooth lower die (8) and an upper die (9)...
|
|
WO/2021/206820A1 |
Improved methods and devices for shielding electrical and electronic aircraft components and their associated cables and wires from cross-coupling and electrical and magnetic interference and dissipating excess heat from the electrical a...
|
|
WO/2021/207220A1 |
An unmanned aerial vehicle according to certain embodiments generally includes a chassis, a power supply mounted to the chassis, a control system operable to receive power from the power supply, at least one rotor operable to generate li...
|
|
WO/2021/206970A1 |
The invention(s) include embodiments and applications of: a system for package handling, the system including: a flying vehicle comprising a nose portion; a storage region of the flying vehicle; a landing support subsystem coupled to the...
|
