| Document |
Document Title |
|
WO/2022/184145A1 |
An unmanned aerial vehicle, comprising: a vehicle body (10); a driving assembly (20), which comprises an electric motor (200) and a propeller, wherein the electric motor is mounted on the vehicle body, the propeller is mounted on the ele...
|
|
WO/2022/183361A1 |
A multi-rotor unmanned aerial vehicle, the vehicle comprising: a vehicle arm (20), wherein a connecting portion (21) is arranged at an end surface of one end of the vehicle arm (20) in a lengthwise direction, and a rotor device (40) used...
|
|
WO/2022/174712A1 |
A quadrotor unmanned aerial vehicle, comprising two sets of binocular sensors and two sets of fish-eye binocular sensors, wherein the two sets of binocular sensors are respectively diagonally arranged on the body of the unmanned aerial v...
|
|
WO/2022/171007A1 |
An aircraft, a cover of an aircraft, and a method for replacing a cover of an aircraft. The aircraft (100) comprises: a nose (110) arranged at the front end of the aircraft and used for pointing to the flight direction of the aircraft; a...
|
|
WO/2022/169443A1 |
Systems and methods for extending the interior cargo bay of fixed-wing cargo aircraft into a replaceable tailcone bay are disclosed. The system includes an aircraft and a removable tailcone configured couple to the aft end of the fuselag...
|
|
WO/2022/162090A1 |
The invention relates to an aircraft door mounted in a fuselage with a reference frame X, Y, Z, comprising a fixed frame, an opening element and a support arm enabling the opening element of the door to be installed and adjusted in posit...
|
|
WO/2022/157083A1 |
The invention relates to an assembly for providing stabilising guidance to a semi-plug aircraft door equipped with an opening/closing mechanism. The door frame (3) is provided with stops (7) at the front and at the rear on which the door...
|
|
WO/2022/157711A1 |
A door (1) for an aircraft configured to be selectively closed on a frame (2), the door (1) comprising a safety system (10) for an anchoring element (6), the safety system (10) comprising a source (11) of light radiations and a receptor ...
|
|
WO/2022/157065A1 |
An electrical barrier device (8) for an aircraft cable raceway, designed to be positioned where two profile sections (1, 2) meet, and comprising: - at least one bottom-wall bridging base; - at least one dielectric panel running transvers...
|
|
WO/2022/159691A1 |
A removable canopy, such as for placement above an entry into a vehicle, includes a brace having releasable mounting features for mounting to the vehicle. The canopy further includes a linkage extending from the brace and convertible fro...
|
|
WO/2022/157245A1 |
An aircraft propulsion module comprises a hydrogen storage system, an electrochemical converter (7) connected to the hydrogen storage system, wherein the at least one electrochemical converter is adapted to convert hydrogen supplied from...
|
|
WO/2022/152613A1 |
The present invention relates to a lightweight flooring for being mounted to at least a part of the bottom of a passenger vehicle.
|
|
WO/2022/140941A1 |
An unmanned aerial vehicle (100/200/300/400/500). The unmanned aerial vehicle (100) comprises a first arm (10), a second arm (20) and a plurality of visual sensors (30). The unmanned aerial vehicle (200/300/500) comprises a first arm (10...
|
|
WO/2022/146288A1 |
The invention relates to a body (2); a canopy (3) disposed on the body (2) so as to be able to move relatively to the body (2), enabling access and providing protection to the cockpit; more than one hook (4) located on the canopy (3); mo...
|
|
WO/2022/144699A1 |
A method for the manufacture of a structural component (1) in composite material reinforced with stiffening stringers (2), defining, in use, at least part of an outer shell (3) of a vector (4) and comprising a skin (5) and a plurality of...
|
|
WO/2022/133676A1 |
A method for detecting the arm state of an unmanned aerial vehicle, a control device, an unmanned aerial vehicle, and a storage medium. Two arms (10) of an unmanned aerial vehicle (200) are provided with a first positioning sensor (20) a...
|
|
WO/2022/137267A1 |
Described is a door (100) for aircraft, configured to be moved from a closed position of an outer shell of a nacelle to an open position to allow an inspection of an internal compartment of the nacelle, comprising: a first multilayer por...
|
|
WO/2022/131577A1 |
Provided is a block drone. The block drone includes an FC battery block including a battery storage portion and a plurality of body blocks, in which each body block has a coupling groove through which a first connection terminal electric...
|
|
WO/2022/132832A1 |
Aspects of the disclosure relate to an aerial vehicle. The aerial vehicle may include an envelope having a plurality of tendons and formed from a first plurality of gores. The aerial vehicle may also include one or more ballonets arrange...
|
|
WO/2022/120796A1 |
A modular unmanned aerial vehicle, comprising: a fuselage (10); a high-voltage operation module (12) arranged on the fuselage; and a low-voltage operation module (14) arranged on the fuselage, wherein the working voltage of the high-volt...
|
|
WO/2022/117453A1 |
An aircraft door architecture comprising: a door (1); an ejector (3); an inflatable evacuation device (4); an emergency energy source (6) connected to the ejector (3) and to the inflatable evacuation device (4); a control unit (9) compri...
|
|
WO/2022/110437A1 |
A windshield wiper device and a windshield cleaning system comprising same. The windshield wiper device (100) comprises: a wiper arm (10); an electric motor (20), wherein the electric motor (20) is used for driving the wiper arm (10) aro...
|
|
WO/2022/107109A1 |
A method is described for manufacturing a structural element (2) in composite material extending along a straight or curvilinear longitudinal direction (D), having a Z-shaped cross section and comprising, in its final configuration, a ce...
|
|
WO/2022/101592A1 |
The invention relates to a liquid retention device (1) intended to be carried on the interior floor of a vehicle and designed and configured to receive a piece of equipment carried by said vehicle, comprising: o an attachment means (26) ...
|
|
WO/2022/101574A1 |
The invention relates to a laminated glazing assembly (1) and its peripheral seal (11), the laminated glazing (1) comprising a transparent structural block (2), the peripheral seal (11) having a first intermediate portion (12) between th...
|
|
WO/2022/100931A1 |
A door arrangement contains a door (4) for a room (3) with a door leaf (30a, b), a wall portion (44) of a wall structure (45) laterally adjacent to the door (4), and a locking arrangement (9) for the door (4) containing: a locking device...
|
|
WO/2022/099577A1 |
An unmanned aerial vehicle (1000), comprising a machine body (110), machine arms (130), foot frames (150), and an antenna assembly (170). The machine arms (130) are connected to the machine body (110). The foot frames (150) are connected...
|
|
WO/2022/094944A1 |
A multirotor unmanned aerial vehicle (100), comprising: a center body (10); two pairs of first mechanical arms (20) rotatably connected to the center body (10) and arranged at two opposite sides of the center body (10); and multiple roto...
|
|
WO/2022/095064A1 |
A frame structure (103) and an unmanned aerial vehicle (1000) comprising the frame structure (103). The frame structure (103) comprises an assembling member (20) and at least two frame members (10). The at least two frame members (10) ar...
|
|
WO/2022/096012A1 |
An unmanned aerial vehicle (100), comprising a fuselage (1), a wing, and a battery (4), wherein the fuselage is provided with a battery mounting space; the battery is removably mounted to the battery mounting space; and the wing is rotat...
|
|
WO/2022/095335A1 |
A multi-rotor unmanned aerial vehicle-based control method. Accessories having a certain priority are jettisoned according to certain conditions, so that the hover work time of an unmanned aerial vehicle can be relatively prolonged. The ...
|
|
WO/2022/095190A1 |
A frame structure for an unmanned aerial vehicle and an unmanned aerial vehicle. The frame structure for an unmanned aerial vehicle comprises a frame body (10), a mounting member (20) and an adapter member (30), wherein the mounting memb...
|
|
WO/2022/094915A1 |
The present disclosure relates to a watertight sealed electronic-circuit apparatus, the watertight sealed electronic-circuit apparatus comprising: a base; and at least two control modules, said at least two control modules being sealingl...
|
|
WO/2022/091729A1 |
Provided is an antenna system capable of suppressing inclination of an antenna caused by strong winds during stationary flight (hovering) in a drone-type wireless relay device. This antenna system comprises: a long antenna 110 connected ...
|
|
WO/2022/084553A1 |
The invention relates to an alignment device (1) and an aircraft arrangement for aligning a piece good part (4), which is lifted by means of a winch (2) of an aircraft (3), about a rotational axis (16) which is parallel to a yaw axis (12...
|
|
WO/2022/085832A1 |
The present invention relates to an individual personal air vehicle operable on water, the personal air vehicle comprising: a lower body which supports an occupant and has a float on the floor surface, a front arm holder and a rear arm h...
|
|
WO/2022/077152A1 |
A clamping and fixing device (300) for clamping components of a multi-rotor unmanned aerial vehicle (100). The clamping and fixing device comprises a main body part (310); a first side of the main body part (310) is provided with a clamp...
|
|
WO/2022/073465A1 |
An unmanned aerial vehicle arm mechanism, comprising an upper unmanned aerial vehicle arm (1) and a lower unmanned aerial vehicle arm (2), wherein first slots (3) are arranged on two sides of the lower unmanned aerial vehicle arm (2); in...
|
|
WO/2022/069101A1 |
A cover panel for an aircraft, comprising: a first region, a second region for forming an overlap with a second panel, and a ramp, wherein at least a portion of the ramp is between the first and second regions, wherein the ramp includes ...
|
|
WO/2022/067939A1 |
An agricultural unmanned aerial vehicle, comprising a body (1), first foot stands (2), second foot stands (3), a battery (4) and a pesticide box (5). The first foot stands (2) are fixedly connected to the bottom portion of the body (1); ...
|
|
WO/2022/068058A1 |
A reinforcing accessory of an unmanned aerial vehicle (UAV) and a UAV, which relate to the technical field of UAVs and can effectively improve the damage resistance of the arms of a UAV. The reinforcing accessory specifically comprises: ...
|
|
WO/2022/067401A1 |
The present application relates essentially to a fixed-wing aircraft made up of a fuselage (02) in the shape of an aerofoil with four wings (10) having the same aerofoil shape with aerodynamic wing behaviour contributing to the lift and ...
|
|
WO/2022/066390A1 |
An unmanned aerial vehicle (UAV), comprising a fuselage outer shell defining a lateral axis, a longitudinal axis and a plurality of shell sides; fuselage center assembly positioned within a cavity defined by the fuselage outer shell; and...
|
|
WO/2022/056597A1 |
An aircraft structure (10) comprising a fuselage (24), first and second forward wings (20, 22) mounted to and/or extending from opposing sides of the fuselage (24), a continuous rear wing span (34) defining first and second rear wings (3...
|
|
WO/2022/059047A1 |
A composite component (1) comprises: a first composite component (10) that is equipped with a base portion (11) to which a second composite component (20) is fixed, and a positioning portion (12) provided on the base portion (11) and pro...
|
|
WO/2022/053527A1 |
The invention relates to an aircraft radome (1) comprising a composite structure (10) comprising, or according to the circumstances configured to define, at least one housing (20) extending along the radome from a base (2) of said radome...
|
|
WO/2022/055766A1 |
A 3D printed additively manufactured (AM) elliptical bifurcating torsion flexure assembly system includes a base section; elliptical bifurcating torsion springs, each including a bifurcated legs section supported by the base; a bifurcate...
|
|
WO/2022/054388A1 |
This method for manufacturing a sandwich panel (100) includes: a step for preparing a plurality of sheet-like prepregs (211); a step for obtaining a composite surface material (40) by performing a first heating and pressing treatment via...
|
|
WO/2022/041468A1 |
An inspection unmanned aerial vehicle, comprising a fuselage, a vehicle arm, a battery device (4), a load control cabin (5) and an inspection device. The bottom part of the fuselage is provided with a support frame; the support frame com...
|
|
WO/2022/045487A1 |
The present invention relates to an anti-icing/de-icing honeycomb core composite material and a method for manufacturing same. The anti-icing/de-icing honeycomb core composite material may be manufactured by a method comprising: a formin...
|
