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WO/2021/121184A1 |
A manned aircraft (100), relating to the field of flying devices. The manned aircraft comprises a body (101), a folding/unfolding mechanism (102), and a flying power device. The folding/unfolding mechanism is provided on the body. The fl...
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WO/2021/109529A1 |
A flying car, comprising a body (6) and wheels (4). First wing bays (3) and a second wing bay (5) are arranged on the body; folding wings (8) are respectively arranged in the first wing bays and the second wing bay; the folding wing comp...
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WO/2021/110572A1 |
An aircraft door comprising means for retaining a deployable evacuation device (6), said means comprising at least: - a beam (8); - a first retention member (10) fixed on a second end (11) of the beam (8) by a detachable clip (16, 17), t...
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WO/2021/109894A1 |
A honeycomb array multi-rotor composite part. The composite part is mainly composed of a face-shaped part (801), an arc-shaped part, a V-shaped part (802), a trifurcate part (803), a regular triangular prism part (804) and a cylindrical ...
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WO/2021/110569A1 |
Disclosed is an aircraft pressurized cabin door (1) comprising an outer panel (2) and a door structure (3) comprising: - two circumferential beams (4) fastened to the lateral edges of the door; - a plurality of longitudinal beams (5a, 5b...
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WO/2021/108669A1 |
An electrically powered STOL aircraft having dedicated motors energized to deploy movable landing gear driven to propel short takeoffs and to actively rotate downwardly to engage the runway surface as the aircraft approaches touchdown on...
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WO/2021/105315A1 |
The invention relates to an apparatus for attaching aerodynamically functional films (14.1-5) to surfaces (4) of bodies (1) around which flow occurs and to the use of such an apparatus. The apparatus comprises a self-adhesive, removable ...
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WO/2021/104012A1 |
Disclosed are an antenna and an aircraft. The antenna comprises a substrate, a circuit board disposed on the substrate, a first radiation part disposed on one side of the substrate, and a second radiation part disposed on the other side ...
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WO/2021/105316A1 |
The invention relates to a method for applying an aerodynamically functional film to a body around which complex flow occurs, for example on a commercial aircraft. The method comprises the following steps: – determining the flow lines ...
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WO/2021/099741A1 |
The invention relates to: - a light aerial vehicle laminated glazing consisting of at least: - one structural transparent plastic sheet (1) covering the whole of the surface of the glazing, - one protective transparent plastic sheet (3) ...
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WO/2021/095395A1 |
A propulsion device according to one embodiment of the present invention has: a rotor having a blade; a motor that causes the rotor to rotate; and a de-icing mechanism that de-ices the blade using heat generated by the driving of the mot...
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WO/2021/095376A1 |
This method is for manufacturing a fan blade rotor 41 which includes an annular rotation support ring 33 around a rotary shaft, a permanent magnet 45 provided side by side with the rotation support ring 33 in the radial direction, and a ...
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WO/2021/095303A1 |
Disclosed are: a honeycomb-like core material that can be simply produced; and a structure using said core material. The core material (10) has a plurality of planar members (a plurality of first planar plates (11) and a plurality of s...
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WO/2021/091151A2 |
The present invention relates to a patient transfer device. Particularly, according to one embodiment of the present invention, provided is a patient transfer device comprising: a support part including a patient loading surface capable ...
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WO/2021/087703A1 |
An aerial vehicle (1000). A radar (400) is mounted on a landing gear (120) by means of a mounting structure (500). The radar (400) is located under the bottom of an airframe (110). An antenna structure (420) of the radar (400) can rotate...
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WO/2021/081788A1 |
A folding structure. The folding structure comprises a mounting assembly (10), a folding assembly (20) rotatably connected to the mounting assembly (10), and a locking assembly (30) assembled on the mounting assembly (10) and correspondi...
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WO/2021/083664A1 |
In order to improve sealing at the transition between high-lift devices and fairings, the inventions suggest a shutter assembly (54) which may be installed in a high-lift system (16), thereby forming the shutter arrangement (24). The shu...
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WO/2021/086533A1 |
An aircraft tolling system uses tolling tags that are configured for attachment to aerial vehicles. The tolling tags include a data format that can be used by any and all aerial vehicles. The system detects and tracks aerial vehicles in ...
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WO/2021/084423A1 |
A handle (10) for opening and closing a door of an aircraft, the handle comprising a base part (14) lockable to a rotatable shaft (11) of an opening mechanism of the door, a hand gripping part (15) connected to the base part (14), and a ...
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WO/2021/080118A1 |
The present invention relates to a coding education system using a drone production kit. In the coding education system using the drone production kit, a drone is manufactured using the drone production kit, and the manufactured drone is...
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WO/2021/078162A1 |
An unmanned aerial vehicle, comprising a body (1) and wings (2), one of the body and the wings being provided with a first connecting portion (10), the other being provided with a second connecting portion (20), and the first connecting ...
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WO/2021/078204A1 |
An unmanned aerial vehicle having dual coaxial propellers. The unmanned aerial vehicle comprises a protective housing (1), a propeller assembly (2), a first balance ring (3), a second balance ring (4), a mounting rod (5), a drive assembl...
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WO/2021/074069A1 |
The subject of the invention is: - a monolithic or laminated glazing unit (1), which is bolted or gripped by a frame (4) that is itself bolted onto or through a structure (3), characterized in that, in at least one part of the periphery ...
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WO/2021/074228A1 |
The invention relates to a system for monitoring a payload of an aircraft, wherein the system has at least one storage surface (26, 28, 30, 32, 36, 38, 42) for a payload and at least one pressure sensor (10), wherein the at least one sen...
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WO/2021/072047A1 |
A window operable to separate an interior from an exterior is disclosed. The window comprises a pressure pane and an anti-condensation assembly. The anti-condensation assembly is disposed in an interior direction relative the pressure pa...
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WO/2021/070363A1 |
[Problem] To provide a flying body having a more fundamental structure and provided with safety measures. [Solution] This flying body, which is equipped with a flight portion that is equipped with rotor blades for generating thrust, a le...
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WO/2021/070905A1 |
The purpose of the present disclosure is to provide an aircraft member having both strength and ductility. In addition, the purpose of the present disclosure is to provide an aircraft member satisfying required flame retardance. In addit...
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WO/2021/061810A1 |
An aerial vehicle is programmed or configured to respond to reports of events or conditions within spaces of a facility. The aerial vehicle travels to a location of a reported event or condition and captures data using onboard sensors. T...
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WO/2021/058411A1 |
The present application relates to an aircraft assembly. The aircraft assembly has a first structural component and a second structural component. A fastener fastens the first component to the second component. The first structural compo...
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WO/2021/058955A1 |
The invention relates to a lock, in particular to a lock for a secondary cockpit barrier, and a secondary cockpit barrier comprising the same and a barrier body for blocking access to an aircraft cockpit.
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WO/2021/054879A1 |
The present invention regards a method of securing a movable latch member of a self- securing latch arrangement (1) configured to latch an aircraft door (3, 803) to an aircraft fuselage (7). The present invention also regards the self-se...
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WO/2021/052217A1 |
The invention aims to fully protect a camera againt an impact applied from the outside of an unmanned aerial vehicle and prevent the quality of a captured image from being affected. The control device comprises: a frame control portion u...
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WO/2021/013589A9 |
Disclosed is a method (81) for arranging a set of antennas capable of transmitting or receiving in a radio frequency range in an existing aerodyne implemented either during an initial installation operation, or in a subsequent maintenanc...
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WO/2021/048553A1 |
A packer (200) for application to an aircraft airframe (100), the packer (200) comprising: a sheet of material having a first surface and a second surface opposite to the first surface; and a plurality of voids (208) defined through the ...
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WO/2021/046558A1 |
A cargo aircraft configured to carry a portion of its payload in a cargo bay volume enclosed by a moveable nose door and supported by a structural extension of the fuselage that extends forward into the moveable nose door is disclosed. E...
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WO/2021/046557A1 |
Systems and methods for loading a cargo aircraft are described. The system includes at least one rail disposed in an interior cargo bay of a cargo aircraft that extends at an angle relative to an interior bottom contact surface of a forw...
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WO/2021/043336A2 |
The present utility model relates to the technical field of aircrafts, and in particular, to a wing detachment assembly and an aircraft. The wing detachment assembly comprises a first connecting portion and a second connecting portion, o...
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WO/2021/046527A1 |
An electronics system (10) for an aircraft includes a mounting structure (12) and a generally planar plate element (40) mounted to the mounting structure (12) which has opposing face surfaces (41, 43) and includes a central region (50) a...
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WO/2021/043335A2 |
The present utility model relates to the technical field of aircrafts and, in particular, to a wing-dismounting assembly and an aircraft. The wing-dismounting assembly comprises a first connecting portion and a second connecting portion;...
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WO/2021/046560A1 |
A fixed-wing cargo aircraft having a kinked fuselage to extend the useable length of a continuous interior cargo bay while still meeting a tailstrike requirement is disclosed, The fuselage defines a continuous interior cargo bay along a ...
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WO/2021/037067A1 |
A frame for an aircraft and an aircraft, the frame comprising an aircraft body, and the aircraft body comprising a base plate (10), a front aircraft arm (11) and a rear aircraft arm (12), and a connecting arm (30) arranged between the re...
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WO/2021/038302A1 |
The invention relates to a method for producing a torsion box for a structure of an aeroplane. Said method comprises the following steps: providing a first component made of a fibre composite material, which first component has a first p...
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WO/2021/035459A1 |
Adaptive wing systems and aircraft. A variable-span wing for aircraft comprises a fixed-section (1) with skin (118) that forms a lift-generating wing surface, and further comprises a top and a bottom moveable section (2) that are vertica...
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WO/2021/032428A1 |
Disclosed is a method for producing a structural component (2), in particular for an aircraft, ground vehicle, or watercraft, or for a rotor blade of a wind turbine, in which method an arrangement (6) consisting of fibres and a plastics ...
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WO/2021/032476A1 |
The invention relates to a primary structural assembly (100) for an aircraft outside-skin heat exchanger (50), the assembly comprising: an outer-skin portion (5) which defines an outer shape of the aircraft (1) and forms a portion of a h...
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WO/2021/032920A1 |
The invention relates to an annular or semi-annular acoustic attenuation structure (200) comprising an inner skin (210) and an outer skin (230), defining between them an annular or semi-annular volume, and a plurality of partitions (220)...
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WO/2021/034783A1 |
A propulsion system includes a duct and a fluid flow generator. The duct has an elongated cavity with an inlet portion and an outlet portion. The fluid flow generator is disposed in the duct. The fluid flow generator configured to receiv...
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WO/2021/032658A1 |
Disclosed is a gap filler (1), system and method for at least partially filling a gap (10) between at least two aircraft components (2, 12). The gap filler comprises a first component (3) and a second component (4) which comprises a chan...
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WO/2021/031591A1 |
A stickable self-resistance heating/superhydrophobicity integrated gradient film material. The film material is made of a bonding resin, an insulating and thermal-insulation resin, a thermally and electrically conductive filler (3), and ...
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WO/2021/028306A1 |
In summary, the present application relates to an aircraft interior paneling (10) comprising: - a planar replaceable surface element (40); - a structural element (20); - at least one connection element (30); wherein the replaceable surfa...
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