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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...
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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)...
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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...
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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...
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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...
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WO/2021/207546A1 |
A surface heating device (100) and related method includes a heater assembly (105) having a layer of dielectric material, thermal insulation material (110) positioned adjacent to the heater assembly (105), an encapsulation layer (115) su...
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WO/2021/200047A1 |
A first laminate in which a prepreg containing reinforcing fibers and a resin is layered is processed to form a second laminate including a flat portion in at least one side edge portion and a corrugated portion along a longitudinal dire...
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WO/2021/198073A1 |
The invention relates to a vehicle region comprising a roof section of a primary structure and two luggage compartments. One of the luggage compartments comprises a releasable luggage compartment hatch and a luggage compartment cover whi...
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WO/2021/195966A1 |
An unmanned aerial vehicle, comprising: aerial vehicle components; arms (1001), at least one aerial vehicle component being connected to the arms (1001); and a body (1002), the arms (1001) being capable of rotating with respect to the bo...
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WO/2021/198964A1 |
An aircraft including a fuselage with one or more wings extending from the fuselage. The aircraft may include one or more apertures in a surface of at least one of the fuselage and the one or more wings. The one or more apertures may be ...
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WO/2021/200862A1 |
Provided is a composite having excellent heat resistance.　This composite is provided with multiple layers stacked on top of each other, and multiple long fibers disposed inside the layers in parallel to a direction orthogonal to the th...
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WO/2021/184199A1 |
A rotor mount assembly(11,41,51,61) includes a rotor seat and a resilient member(118). The rotor seat includes a base(112,412,512,612) and a lock structure(114,414,514,614) arranged at the base. The lock structure includes a recess(1242,...
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WO/2021/186718A1 |
A long frame (20) is provided with: a plurality of frame members (21) that have a longitudinal direction (LD) and a short direction (SD), have a first flange part (21a) folded along a folding line extending along the longitudinal directi...
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WO/2021/183625A1 |
Embodiments relate to a flight vehicle structural component for nano-scale energy converters and thermionic power harvesting devices. The apparatus includes a first electrode, a second electrode spaced from the first electrode to provide...
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WO/2021/179257A1 |
A frame (10) and an unmanned aerial vehicle (1). The frame (10) comprises: a frame body (100) comprising a plurality of arm fixing parts (110), where each of the arm fixing parts (110) is provided with an elastic member (111); a pluralit...
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WO/2021/173404A1 |
Lock apparatus and related methods for use with drones are disclosed. A disclosed drone assembly includes a wing, a keel-beam, an adapter positioned on an end of the keel-beam, and a lock configured to receive the adapter. The lock inclu...
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WO/2021/171760A1 |
A method for manufacturing a composite material includes layering a first sheet (210) that has a first slurry (214) and a third sheet (230) that has a third slurry (234), and heating the layered first sheet (210) and third sheet (230) to...
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WO/2021/171633A1 |
[Problem] To configure the frame of a flight body so as to make it possible to stabilize said frame. [Solution] A frame assembly for an uncrewed aircraft, the frame assembly being characterized by comprising at least two parallel first f...
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WO/2021/167504A1 |
The present invention regards a profile manufacturing tool assembly (1003) configured for manufacture of a curved aerospace profile article (101) and a method of manufacture of a curved aerospace profile article (101) made of fibre reinf...
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WO/2021/165896A1 |
A cargo door (10) for an aircraft comprises a series of locking devices (13) spaced near an edge of the cargo door, a vent panel (11), a control handle (16), and a torsion shaft (14), which actuates a series of pins (19) to lock and unlo...
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WO/2021/161717A1 |
This composite material structure is provided with: a first composite material that is obtained by stacking a plurality of first composite material sheets, each of which is obtained by impregnating electroconductive first reinforcing fib...
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WO/2021/153445A1 |
The present invention provides a heat input reducing structure for an aircraft, an aircraft, and an aircraft manufacturing method with which, even if there is a limit to natural ventilation due to heat dissipation from a compartment in t...
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WO/2021/151859A1 |
Aircraft door comprising an external opening/closing lever (7) and an internal opening/closing lever (9) that are coupled by an engaging mechanism (12) which comprises: - a stop (24) that drives a counter-stop (23) when the internal open...
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WO/2021/148336A1 |
An aircraft comprising: a fuselage having a pressure shell, a fairing, and an unpressurised space between the pressure shell and the fairing. One or more fuel lines extend inside the unpressurised space from the fuel tank to an engine. T...
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WO/2021/149377A1 |
The resin formed panel comprises: a base plate constituted from a fiber reinforced resin containing a continuous fiber and a thermoplastic resin, wherein a recessed portion recessing from the plate surface has been formed; and an attachm...
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WO/2021/148774A1 |
An airframe or a part thereof 3, for example a skin assembly or a profile such as a structural profile, comprises: a wall W having an aperture A therethrough, wherein the wall W provides a frame F surrounding, at least in part, the apert...
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WO/2021/148335A1 |
An aircraft fuselage comprising a fuselage shell; and a fuel tank outside the fuselage shell, wherein the fuselage shell has a double-lobed cross section and at least part of the fuel tank is located in a channel between the two lobes.
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WO/2021/148775A1 |
An airframe 1 or part thereof comprises a set of modular cells 10, including a first cell 10A comprising a set of profiles 100 including: a first structural profile 100A, having a first length L1 and enclosing a first volume V1 providing...
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WO/2021/146295A1 |
The technology described herein relates to autonomous aerial vehicle technology and, more specifically, to autonomous unmanned aerial vehicle with folding collapsible arms. In some embodiments, a UAV including a central body, a plurality...
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WO/2021/146264A1 |
Disclosed are polyurethane-polysiloxane hybrid coating compositions (PUPSHCC) and their uses, processes for their preparation, and substrates incorporating the coating compositions.
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WO/2021/144383A1 |
The invention concerns an aerospace structure comprising a strike layer and a capture layer and an intermediate layer there between. The structure is arranged to arrest a projectile passing through the structure.
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WO/2020/254984A9 |
An aerodynamic louver system used in one or more of the following operations: control, adjust, or stabilize, aid in controlling, adjusting or stabilizing a spacecraft's orientation, angle of attack, lift, or position. There could be mult...
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WO/2021/139047A1 |
A modular quick-to-disassemble unmanned aerial vehicle, comprising a fuselage body (1), wing modules (2), an empennage module (3), and a driving module (4). The wing modules (2) are detachably connected to the two sides of the abdomen of...
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WO/2021/140861A1 |
In this junction structure which has a reinforcement part that is formed by bonding a composite material and a reinforcement material via an adhesive, the composite material comprises a plate part formed by laminating multiple textile sh...
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WO/2021/139046A1 |
A target drone capable of being quickly disassembled, comprising a fuselage (1), steering gears (2), wings (3), a vertical tail wing (4), and horizontal tail wings (5). The wings (3), the vertical tail wing (4), and the horizontal tail w...
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WO/2021/136935A1 |
The invention provides an aircraft passenger accommodation unit (1000) comprising a seat (100), a shell (110) defining an opening (120), and a door (130). The door (130) is translatable along a first path across the opening (120) between...
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WO/2021/134472A1 |
Disclosed is a foldable device. A first body (10) and a second body (20) of the foldable device are rotatably connected by means of a rotary connecting assembly (30). The rotary connecting assembly (30) comprises: a first component (31) ...
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WO/2021/045926A9 |
A material for use in interacting with a flow is provided. The material comprises an interface surface adapted to move in response to a pressure associated with at least one wave in a flow exerted on the interface surface; and a subsurfa...
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WO/2021/130037A1 |
An aircraft cargo bay door assembly, comprising: a cargo bay door configured to pivotably connect to an airframe; and a door support mechanism including: an extendable strut having a first strut end and a second strut end, the first stru...
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WO/2021/122322A1 |
The invention relates to a component system for interior furnishing of an aircraft, having at least one furnishing component, a plurality of component rails, a plurality of guide elements that can be brought into engagement with the comp...
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WO/2021/120659A1 |
A self-driving control apparatus (100) and a driverless apparatus provided with same, the self-driving control apparatus (100) comprising: a mounting base (120), a control apparatus (30), a communication apparatus, and an antenna assembl...
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WO/2021/124213A1 |
A convertiplane (1, 1', 1'') is described that comprises: a fuselage (2), having a first longitudinal axis (A) and, in turn, comprising a nose (12) and a tail portion (13); a pair of wings (3) arranged on respective opposite sides of the...
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WO/2021/122277A1 |
Modular assembly of autonomous aircraft, comprising common modules and specific modules that can be attached to each other, each of the modules comprising a shell forming a fuselage section, the common modules comprising: - propulsion mo...
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WO/2021/126979A1 |
An aircraft flooring system is provided, made up of a low-weight carpet tile which functions both as a moisture barrier and as the loop part of a hook-and-loop system, for coupling to a hook part of a hook-and-loop system, which is bound...
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WO/2021/122567A1 |
The invention relates to an aircraft door (1) comprising: a safety latch (7) comprising a first locking member (8) and a complementary second locking member (9) which is movable; a link (11) comprising at least one section (13) of electr...
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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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