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WO/2020/181855A1 |
A dihedral trapezoidal lifting and floating integrated aircraft, comprising an aircraft body (1) and a power system. The aircraft body (1) comprises a head part provided with an equipment front compartment (2) and a tail part provided wi...
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WO/2020/178283A1 |
Disclosed is an aircraft pressurised cabin door (1), comprising a fuselage panel (2) and a door structure (3) that comprises: two circumferential beams (4) arranged on the lateral edges of the door (1); a plurality of longitudinal beams ...
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WO/2020/176666A1 |
A method of in-flight operational assessment for an electric aircraft comprising detecting by a sensor an electrical parameter of an energy source. The method further includes receiving by a controller the electrical parameter from the s...
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WO/2020/171722A1 |
Aircraft is equipped with a telescope built in the fuselage (1) with the initial angular mirror (2) installed in the open part of the fuselage (1) and the main mirror (7) installed in the cylindrical part of the fuselage. The open part o...
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WO/2020/167867A1 |
Load control apparatuses, systems and methods to control a location, orientation, or rotation of a suspended load by imparting thrust vectors to the suspended load or to a structure that holds the load. The load control apparatuses, syst...
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WO/2020/097042A9 |
This disclosure discloses a method comprising: positioning a stencil having an opening onto an aerospace part such that the aerospace part is accessible through the opening; positioning a masking medium onto the aerospace part through th...
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WO/2020/161428A1 |
Ejection system for a vehicle emergency exit Ejection system (11) for a vehicle emergency exit, the emergency exit extending along a base surface (7) and being designed to cooperate in a mounted position with a receiving frame of the veh...
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WO/2020/157011A1 |
An attachment housing (1) for fastening to an outside (2) of an aircraft forms a functional space (3) on the outside (2) of the aircraft. The functional space (3) has two parts and comprises a ventilation space (6) and a protected space ...
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WO/2019/211852A9 |
A composite structural member including at least one first flange element made from a first composite material, and at least one first web element made from a second composite material. The at least one first web element is connected to ...
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WO/2020/160039A1 |
A magnetic perimeter attachment for an interior space of a vehicle, such as an aircraft or other such vehicle. The vehicle flooring section includes a magnetic tape attached to the structural floor of a vehicle and a spacer panel magneti...
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WO/2020/156018A1 |
A low-energy-consumption high-speed flying method, a wing ring mechanism (1) which uses said method, a wing ring flying saucer, and a high-altitude power generation ring and an opposite-pull aircraft that use the wing ring mechanism. Acc...
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WO/2020/150859A1 |
Provided are an antenna stand, an antenna assembly and a movable platform. The antenna stand comprises: a base for connecting a movable platform, and a stand portion for connecting an antenna, wherein the stand portion is rotatably conne...
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WO/2020/145484A1 |
According to one embodiment of the present invention, the objective of the present invention is to provide a drone having separable main body and wings, the drone comprising: a first contact surface which is formed on one from among the ...
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WO/2020/145485A1 |
A drone including a vertical wing serving as a landing support according to an embodiment of the present invention comprises: a main body part of the drone; at least one pair of horizontal wing parts formed on the main body part so as to...
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WO/2020/106343A9 |
A novel mechanism for reducing boundary layer friction and inhibiting the effects of uncontrolled fluid turbulence and turbulent layer separation, thus reducing the body drag, kinetic energy losses and lowering engine and pump fuel consu...
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WO/2020/142337A1 |
Technologies for providing emergency egress routes for a blended wing body aircraft are described herein. In some examples, the emergency egress routes are through a side cabin bulkhead and aft one or more cargo holds. In some examples, ...
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WO/2020/141397A2 |
In an aircraft, latches, keyed mounting plates, and bi-stable power drive units (PDUs) are used to move and secure cargo within the cargo hold of the aircraft. The latches have a latch head that secures the cargo in the vertical (Z) and ...
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WO/2020/142416A1 |
Technologies for providing blended wing body aircraft control surfaces are described herein. In some examples, one or more of the control surfaces have angular configurations that reduce the formation of air vortexes when in upward or do...
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WO/2020/142335A1 |
Technologies for providing noise shielding are described herein. In some examples, noise shields are installed proximate to one or more of the main engines of the aircraft. The noise shields can be extended during terminal operations and...
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WO/2020/134235A1 |
An unmanned aerial vehicle (500) and a wing assembly thereof (100). The wing assembly (100) is used for being mounted on a fuselage (200) of the unmanned aerial vehicle (500) and comprises wings (10); and a rotary lock cylinder (20), whe...
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WO/2020/135637A1 |
A logistics unmanned aerial vehicle comprises a fuselage (1) and four rotary blade shafts (2) extending through the fuselage (1) and arranged in a criss cross fashion. Two ends of the rotary blade shaft (2) respectively extend out of the...
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WO/2020/133089A1 |
A barrel-launched folding-wing unmanned aerial vehicle and a launch method therefor. The barrel-launched folding-wing unmanned aerial vehicle comprises: a folding-wing unmanned aerial vehicle (7) and a launch barrel (6). When in a barrel...
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WO/2020/133834A1 |
A frame for an unmanned aerial vehicle, and an unmanned aerial vehicle. The frame comprises a body (1). The body comprises an upper housing (1.1) and a lower housing (1.2) adaptive to the upper housing. The upper housing and the lower ho...
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WO/2020/136422A2 |
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WO/2020/127103A1 |
The invention relates to a fuselage element (100) designed to be removably incorporated in a fuselage bay of an aircraft so as to seal the bay, the fuselage element (100) comprising: - a plurality of glazed panels, each glazed panel comp...
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WO/2020/128662A1 |
An aircraft (1) is described that comprises: a fuselage (2) with a first axis (A) of longitudinal extension; and a tail portion (14) arranged at a tail end (13) of the fuselage (2); the tail portion (14) comprises two surfaces (15a, 15b)...
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WO/2020/128793A1 |
Fiber-reinforced composites is provided. The composites include a plurality of prepreg layers, each comprising a polymeric resin and a plurality of fibers disposed therein; and at least one electrically-conductive layer at least partiall...
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WO/2020/125523A1 |
The present application discloses a foldable multi-rotor unmanned aerial vehicle. The unmanned aerial vehicle uses a tilt rotor technique. A rotor tilt device (100) controls the tilt angle of rotors (210). A mechanism for controlling the...
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WO/2020/122433A1 |
The present invention relates to a drone provided with a foldable rotary wing and, more specifically, to a drone (an unmanned aerial vehicle) provided with a foldable rotary wing, wherein the wing of the drone can be folded through a sim...
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WO/2020/119248A1 |
A frame for an aircraft (100), and an aircraft (100). The frame comprises: a body (10) and a fixing assembly (20). The fixing assembly (20) is provided on the body (10). The fixing assembly (20) comprises a fixing frame (210) and a faste...
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WO/2020/113444A1 |
A lampshade structure (100), comprising: a lampshade body (10), the lampshade body comprising a first light-transmitting surface (11) close to a light-emitting element (90), and a second light-transmitting surface (12) away from the ligh...
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WO/2020/116343A1 |
This composite material-made aircraft component has: a laminate structure in which multiple composite material layers are laminated; and a curved structure which has varying circumferential lengths in the longitudinal direction. The lami...
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WO/2020/115960A1 |
[Problem] To provide a pressure variation absorbing structure in which it is possible to prevent degradation in pressure variation absorbing performance caused by an air current on a surface and to prevent deviation of a resonance freque...
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WO/2020/109342A1 |
The invention relates to a sandwich composite component (1) for the interior of a passenger aircraft. One problem to be solved by the invention is that of proposing a cost-effectively produced sandwich-composite component which is suitab...
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WO/2020/107457A1 |
Method of folding an unmanned aerial vehicle (100) including a plurality of arms (101-106) radially extending from a central body (10) of the unmanned aerial vehicle (100) is provided. The method includes folding a first subset of the ar...
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WO/2020/109738A1 |
The invention relates to a seal (20) configured to be mounted on a first member of a turbomachine (100), such as a door (16) of a discharge valve (10), and to come to bear against a second member (11, 12, 128) of the turbomachine, such a...
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WO/2020/104704A1 |
A system for joining a lightweight panel to a structure comprises: at least one body (5') configured to be located inside the thickness of the lightweight panel (3) between two mutually opposing surfaces (8) of the panel; and at least on...
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WO/2020/102933A1 |
Disclosed is a radar assembly (10), characterized in that the radar assembly (10) comprises a radar (11), a gimbal (12) and a mounting structure (13). The gimbal (12) comprises a rotating shaft mechanism, and the rotating shaft mechanism...
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WO/2020/102862A1 |
Aircraft components, e.g., wing leading edge modules, are provided with an electrical energy harvester so as to generate electrical power that can be stored by on-board batteries. In preferred forms, the aircraft component is a wing lead...
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WO/2020/107008A1 |
An aircraft for carrying a cargo assembly. The aircraft comprises a spine structure including a first end, a second end, and mounts. The mounts structurally engage the cargo assembly in juxtaposition with the spine structure between the ...
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WO/2020/101727A1 |
A panel assembly that includes inside and outside core layers, an armor layer sandwiched between the inside and outside core layers, and an armor member that includes at least an outside portion and a transverse portion. The outside core...
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WO/2020/100820A1 |
A flight vehicle 100 has an attachment part 25 on an upper part, the attachment part being constituted as a frame-shaped structure configured so that the vertical-direction position thereof can be adjusted, and the flight vehicle 100 has...
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WO/2020/101728A1 |
A door assembly configured to be positioned between a first compartment and a second compartment that includes a main door portion having a first decompression opening defined therein, at least a first panel portion positioned in a first...
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WO/2020/094688A1 |
The invention relates to an emergency opening device (1) for an aircraft door, comprising: a tubular operating member (2); and elastic compression means (3). The operating member (2) comprises a first end element (10) and a second end el...
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WO/2020/095025A1 |
A payload mechanism for a vehicle is provided. The payload mechanism comprises: a door (2) operable to be in a closed configuration or an open configuration within a recess of the vehicle, the recess having an aperture(10); a first beari...
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WO/2020/094042A1 |
Provided are a contact wire and contact net for an unmanned aerial vehicle, and a matching unmanned aerial vehicle and charging rod. The contact wire mainly consists of a surface twisted layer and a core body on which same is wrapped; Th...
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WO/2020/094695A1 |
The invention relates to an emergency opening device (1) for an aircraft door, comprising: a tubular operating member (2); and elastic compression means (3). The operating member (2) comprises a first end element (10) and a second end el...
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WO/2020/092313A1 |
An aircraft that includes a body defining a cabin interior, front and back rows of seats positioned in the passenger zone, a forward door and an aft door that are pivotable between a closed position and an open position. The cabin interi...
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WO/2020/091885A1 |
An aircraft that includes a body that defines a cabin interior, a divider member that divides the cabin interior into a cargo hold and a passenger cabin, front and back rows of seats positioned in the passenger cabin, a forward door that...
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WO/2020/091933A1 |
An aircraft that includes a body that defines a cabin interior and a side opening, a partition that divides the cabin interior into a cockpit and a passenger cabin, a front row positioned in the passenger cabin, and a first door position...
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