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WO/2018/169066A1 |
Provided are a method for manufacturing a resin sheet 10 capable of substantially transmitting heat, the resin sheet 10, a method for manufacturing a structural body using the resin sheet 10, the structural body, and an airframe of an ai...
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WO/2018/166436A1 |
Disclosed is an unmanned aerial vehicle sliding-type mechanical arm device comprising a mechanical arm (1), a mechanical arm seat (2), and an electric motor impeller assembly (3) mounted on the mechanical arm (1), wherein the mechanical ...
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WO/2018/158766A1 |
An airborne vehicle made of thermally non-conductive materials and method for thermal conduction in an airborne vehicle are disclosed. The airborne vehicle comprising at least one structural element made of material with high thermal con...
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WO/2018/157833A1 |
An unmanned aerial vehicle: arm assemblies (12, 13, 14, 15) of the unmanned aerial vehicle may be folded and unfolded relative to a casing so as to facilitate transportation and storage of the unmanned aerial vehicle. At the same time, t...
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WO/2018/152916A1 |
A battery compartment (10) and an unmanned aerial vehicle (200). The battery compartment (10) comprises a first housing (11), a second housing (12), and a sealing piece (13); an abutting face (111) is formed at the periphery of the first...
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WO/2018/152785A1 |
Disclosed is an unmanned aerial vehicle (100), comprising a body (10) and a battery module (40). The body (10) comprises a bottom portion (11) facing the ground. The battery module (40) comprises a battery having a top portion (41) oppos...
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WO/2018/152911A1 |
An unmanned aerial vehicle (100) and a fuselage (10), the fuselage (10) comprising an upper shell (11) and a lower shell (12). The upper shell (11) comprises an upper shell groove (112) arranged at the periphery of the upper shell (11), ...
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WO/2018/150748A1 |
Provided is an agricultural multicopter in which legs (skids) for supporting a body can be reinforced by using a supporting structure for work devices, such as tanks. This agricultural multicopter comprises: a body; a plurality of arms w...
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WO/2018/152525A2 |
Disclosed is a networked array of radar enclosures that can be arranged to cover a desired geographical location. The array can detect moving objects in the coverage area. When warranted, elements of the array can also control the moveme...
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WO/2018/135739A1 |
A shape memory morphing member using a kirigami pattern is disclosed. The shape memory morphing member using a kirigami pattern comprises: an upper SMP skin layer; a lower SMP skin layer disposed below the upper SMP skin layer; and a cor...
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WO/2018/133277A1 |
Provided is a heat management structure, comprising: a heat dissipation layer; an accommodation member for accommodating at least one heat source; and a heat pipe having two ends respectively connected to the heat dissipation layer and t...
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WO/2018/132096A1 |
An aircraft passenger cabin airflow metering apparatus and system is provided. The apparatus includes a blowout disc designed to release at a predetermined air pressure differential on opposite sides of the blowout disc. The blowout disc...
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WO/2018/132147A1 |
A divider assembly that includes a main body portion having a lower section and an upper section and a removable panel having front and back surfaces. The upper section tapers in width in an upward direction and the main body portion inc...
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WO/2018/120741A1 |
A barrier material, a polyurethane adhesive containing same, a skin and an aircraft. The barrier material comprises a povidone and an ethylene/vinyl alcohol copolymer coupled with a coupling agent. After coupling the povidone and the eth...
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WO/2018/119578A1 |
Transformable apparatus is provided with one or more moveable components (104, 204, 404, 604). The movement of the one or more components relative to another component (102, 202, 402, 602) of the transformable apparatus transforms the tr...
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WO/2018/113481A1 |
Provided in the present utility model are a detachable arm assembly and an aircraft. The detachable arm assembly comprises a first arm section and a second arm section. A first line core is fixedly provided inside the first arm section. ...
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WO/2018/113480A1 |
Provided in the present utility model are a detachable arm assembly and an aircraft. The detachable arm assembly comprises a first arm section and a second arm section. A first line core is fixedly provided inside the first arm section. ...
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WO/2018/112798A1 |
A multi-rotor unmanned aerial vehicle (10) comprises a housing (12) and a plurality of propeller arms (20) movably mounted at the housing (12) such that each arm (20) is movable between a deployed position where the arm (20) extends outw...
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WO/2018/119436A1 |
A multi-layered intelligent display system includes a first LCD display panel; a second OLED display panel; a smart panel disposed behind the second display panel; an LED panel disposed between the second display panel and the smart pane...
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WO/2018/108148A1 |
An unmanned aerial vehicle, comprising a fuselage (1) and multiple arms (2) disposed at left and right sides of the fuselage (1), said unmanned aerial vehicle also comprising a sliding mechanism; open grooves (3,11) are provided on the f...
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WO/2018/107972A1 |
An arm and an unmanned aerial vehicle, the arm comprising a first arm segment (11) and a second arm segment (12), the first arm segment (11) being provided with a locking part (112) and the second arm segment (12) being provided with a l...
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WO/2018/109255A1 |
The invention relates to a method for producing reinforced monocoque structures and to the structure obtained, the method comprising: using base components (1) made from a partially cured composite material and joining the base component...
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WO/2018/111346A1 |
A device is provided for controlling fluid flow over a window of a movable optical instrument housing. The device includes a generally annular body having an inner peripheral edge configured to correspond to a peripheral edge of the wind...
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WO/2018/104403A1 |
The invention relates to a cabin floor (2) suitable for being installed horizontally in a peripheral fuselage segment of an aircraft, said cabin floor (2) comprising a first planar structural portion (21) and a second planar structural p...
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WO/2018/103641A1 |
A retractable drone, comprising: a main cabin (1) and a motor blade mechanism; a left and a right side of the main cabin (1) are provided with a protective cover (2) respectively, and the protective cover (2) slidably connects the motor ...
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WO/2018/103026A1 |
Disclosed is a multi-rotor unmanned aerial vehicle, comprising: a body (1), and a plurality of arms (2) arranged on the body (1) in a foldable manner. When the arms (2) are in an unfolded state, the arms (2) extend toward the periphery o...
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WO/2018/096933A1 |
This composite member 1 is provided with a web part 21 and a flange part 22 provided at the end of the web part 21. The flange part 22 comprises multiple laminated fiber sheets, and the surface on one side in the lamination direction is ...
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WO/2018/090435A1 |
Disclosed is an aircraft (100), comprising a centre frame (1), an antenna (3), and an arm assembly (2) connected to the centre frame. The arm assembly comprises arms (21). The antenna is disposed at a position on the arm away from the ce...
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WO/2018/091475A1 |
The invention relates to an electrohydraulic module (1) for driving at least one component of an aircraft, in particular an airplane, wherein the electrohydraulic module (1) comprises at least one electric motor (2) and at least one comp...
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WO/2018/088149A1 |
The purpose of the present invention is to facilitate the attachment of a second member to a sheet-like first member, while supporting the first member in a state of being capable of being deformed by gravity. This component production m...
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WO/2018/088140A1 |
The purpose of the present invention is to facilitate the riveting of a second member to a first member when superposing and assembling the two members. This component production method is provided with: a step (S2) in which an attaching...
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WO/2018/087213A1 |
The present invention relates to an aircraft (100) comprising: a fuselage (101) comprising a plurality of panels (105) adapted to define an aerodynamic shape for a cockpit or a cargo hold of the aircraft (100);at least one wing (103) str...
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WO/2018/086496A1 |
A telescopic propeller arm assembly (12) and an unmanned aerial vehicle (10). One end of the telescopic propeller arm assembly (12) is connected to a body (11) of the unmanned aerial vehicle (10), and the other end is connected to a powe...
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WO/2018/089934A1 |
Commercial supersonic aircraft and associated systems and methods. A representative commercial supersonic aircraft includes a fuselage configured to carry a crew and between 20 and 60 passengers, a delta wing mounted to the fuselage, and...
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WO/2018/088138A1 |
The purpose of the present invention is to achieve accurate alignment when superposing and assembling two members. This component production method is provided with: a step (S14) for calculating a first virtual line which is parallel to ...
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WO/2018/085038A1 |
Some embodiments are directed to an apparatus, such as a panel that might be appropriate for aircraft or space vehicle fuel tanks. According to some embodiments, a plurality of stiffening elements may be attached to a matrix stiffened la...
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WO/2018/083077A1 |
The present invention is concerned with actuating aircraft components to tailor their configuration to achieve improved performance in one or more flight phases. In general terms, the invention provides a method and system for actuating ...
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WO/2018/076471A1 |
Disclosed is an unmanned aerial vehicle (100), comprising a metal housing (10), a GPS module (20) and a cover plate (30). The metal housing (10) comprises an accommodation portion (111) with an opening; the GPS module (20) is provided wi...
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WO/2018/080905A1 |
The present invention provides high security polycarbonate laminates integrated with insulated glazing units (IGU) to produce high security windows. The laminate comprises at least nine layers, in the following order: (i) an insulated gl...
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WO/2018/080989A1 |
In one example, a structure is provided that includes a plastic body having a unitary, single-piece construction. The plastic body further includes a substantially hollow interior, and a parting line that extends around a portion of the ...
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WO/2018/076470A1 |
Disclosed is an unmanned aerial vehicle (100), comprising a body (10), an arm (20) connected to the body (10), and a connection assembly (30). The arm (20) is detachably connected to the body (10). The connection assembly (30) comprises ...
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WO/2018/077968A1 |
The present invention pertains to a fluoropolymer composition (C) comprising a polymer (A) of ethylene and tetrafluoroethylene and/or chlorotrifluoroethylene, and a certain amount of specific acid scavenger (AS), optionally a colorant,an...
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WO/2018/076253A1 |
Disclosed is a connection assembly (30), an unmanned aerial vehicle arm (20) having the connection assembly (30) and an unmanned aerial vehicle (100). The connection assembly (30) is used for connecting and locking two components, and th...
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WO/2018/072324A1 |
Disclosed is an unmanned aerial vehicle, which comprises a fuselage (10), a vehicle arm (20) and a vehicle arm clamping device (30). The vehicle arm (20) comprises an oppositely-arranged free end (222) and a fixed end (224). The vehicle ...
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WO/2018/074423A1 |
This fan rotor blade consists of a composite material including a thermoplastic resin and reinforcing fibers, and is provided with: an outer covering member forming a blade surface shape having a positive pressure surface and a negative ...
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WO/2018/067100A1 |
The group of inventions relates to aviation. An aeroplane comprises a fuselage which consists of a body of an upper load-bearing piloted part and a capsule in the form of a body of a lower part which is capable of automatically separatin...
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WO/2018/067029A1 |
The invention relates to aviation engineering. Each variant of an aircraft canopy comprises a glazed housing having a front portion, an upper portion and convex lateral portions which protrude beyond the upper portion. The housing has tr...
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WO/2018/060186A1 |
The invention relates to a cabin wall element for thermal and acoustic insulation of an aircraft fuselage section located between two frames of an aircraft fuselage, wherein the cabin wall element has an outer wall which comprises a ther...
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WO/2018/061281A1 |
A composite material structure according to an embodiment of the present invention includes: a corrugated stringer that is formed of a composite material and has a plurality of hat portions; and a panel that is formed of a composite mate...
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WO/2018/061955A1 |
The present invention is a molded male hook-and-loop fastener that excels in fire retardancy and low fuming property and has on the surface of a substrate a large number of engaging elements projecting from the substrate, wherein both th...
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