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WO/2017/183551A1 |
This unmanned aerial vehicle is optimized for transport of a load and can efficiently drop a load and manage the vehicle body. The unmanned aerial vehicle, provided with multiple rotor blades, is characterized in that a frame of the unma...
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WO/2017/183004A1 |
An electrochromic device includes one or more flame-retardant agents.
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WO/2017/183684A1 |
This aircraft fuselage assembly jig is equipped with: a base provided with a plurality of frame indices for determining the positions of both ends of a plurality of aircraft fuselage frames; a plurality of header plates which project fro...
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WO/2017/183685A1 |
This aircraft fuselage assembly jig is equipped with: a horizontally oriented base on which an aircraft fuselage panel is placed so as to be lying down, and which is provided with a plurality of frame indices for determining the position...
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WO/2017/177458A1 |
Disclosed is a frame of an unmanned aerial vehicle, comprising: a centre frame (1), a dividing circuit board (2) and a flight-control installation component (3). The centre frame (1) comprises a top surface and a bottom surface opposite ...
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WO/2017/173725A1 |
An unmanned aerial vehicle having a linked folding structure, comprising a vehicle base (100), and a plurality of vehicle arms (200) and landing gear (300) distributed along the perimeter of the vehicle base (100), and also comprising co...
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WO/2017/177162A1 |
A coated transparency includes: a transparency; a base layer on the transparency, the base layer comprising at least one selected from an organic compound, an organosilicon compound, and a polysiloxane compound; a metal layer physically ...
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WO/2017/173732A1 |
An unmanned aerial vehicle (UAV) with a multi-arm synchronous folding mechanism, comprising: a base (1) having a flat plate shape and being provided with a plurality of rotating shafts (12) which extend parallel to the base (1); a plural...
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WO/2017/173733A1 |
An unmanned aerial vehicle comprising: an upper body portion (1), a middle portion (2), and a lower body portion (3). The upper body portion (1) comprises: at least one mechanical arm (11). At least one propeller (13) is arranged on each...
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WO/2017/174906A1 |
Polarisible interior trim window comprising a removable fixing device Interior trim window (13) able to collaborate with a support (11), the said interior trim window (13) comprising a polarisable film, a device for applying a tension to...
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WO/2017/176889A1 |
A truss reinforced radome crown structure shock absorbing and recoiling system that is utilized with an aircraft antenna adapter plate or other satellite communication (SAT-COM) structure to an aircraft airframe or fuselage and for allow...
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WO/2017/167945A1 |
The invention is based on a vehicle device, in particular an aircraft device, having at least one window unit (48a; 48b; 48c) and having at least one transparency-switching unit (54a; 54b; 54c) which is provided, in at least a first oper...
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WO/2017/172840A1 |
This document describes a system and method through which unmanned aerial vehicles (UAVs) can be docked, with a device that can secure the UAVs, and information can be transmitted to and from such UAVs. The UAVs are secured through the u...
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WO/2017/166275A1 |
Airframe connection components for an unmanned aerial vehicle, comprising: a support tube (110), an auxiliary member (130), and a secure member (140). An opening end of the support tube (110) is used for being fitted to a connection part...
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WO/2017/154551A1 |
This flying object (100) comprises: a plurality of rotor units (20) each including a propeller (21) and a motor (22) that drives the propeller (21); a plurality of balloons (30) respectively provided to the plurality of rotor units (20);...
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WO/2017/155562A1 |
Described are mounting assemblies for securing aircraft passenger seats, including a beam, an adaptor, and fasteners. The beam can include holes spaced along a flat upper surface. The adaptor can be supported by the beam and include a ch...
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WO/2017/148923A1 |
A remote-controlled unmanned foldable aircraft (1) comprises at least two motors (3) that allow the aircraft (1) to fly, and at least one support structure (2) for supporting said motors (3); the support structure (2) is flexible and inf...
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WO/2017/151081A1 |
The utility model relates to the sphere of aviation and aircraft repair technology, namely to the Method of on-condition repair and modernization up-dating of an aircraft center wing section, in particular, of Antonov-32 (An-32) type air...
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WO/2017/143501A1 |
An unmanned aerial vehicle (UAV) (100) may comprise a central body (102), and a plurality of arms (104) extendable from the central body. Each arm (104) may be configured to support one or more propulsion units (108).Each arm (104) may b...
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WO/2017/146666A1 |
The inventions relate to aviation and to ground transport. An aircraft adapted for saving passengers in the event of an emergency consists of an upper and a lower part. The upper part is designed to be capable of controlled flight in the...
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WO/2017/143643A1 |
Disclosed is an unmanned aerial vehicle (100, 200), comprising a body (10, 10'), arms (20) and power assemblies (30, 30'). The arms (20) are connected to the body (10, 10') and support the power assemblies (30, 30'). The arms (20) at lea...
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WO/2017/143645A1 |
Disclosed is an unmanned aerial vehicle (100), comprising a body (10) and arms (22) for carrying power devices (21), the power devices (21) being used for providing power of flight. The arms (22) are movably connected to the body (10), a...
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WO/2017/141526A1 |
Disclosed is structure designing method for installing a composite material including a polyarylate fiber and a resin in a structure, such as a vertical tail fin, as a vibration damping member, the method comprising: a step S3 for analyz...
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WO/2017/134629A1 |
A method for adaptively shadowing bright light in a field of view seen by an observer. The method includes receiving, from a first image sensor facing a scene in front of the transparent display, light intensity data indicative of bright...
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WO/2017/132803A1 |
An unmanned aerial vehicle folding structure, comprising an arm (1) and an arm mount (2); further comprising an arm rotation block (3), the arm rotation block (3) being fixedly connected to the bottom surface of an end of the arm (1); th...
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WO/2017/132808A1 |
An unmanned aerial vehicle irregular-shaped arm folding device, comprising an internally hollow arm (1), a rotation base (2) and a rotation stem (3), the rotation stem (3) being T-shaped, the vertical end of the T shape being inserted in...
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WO/2017/134898A1 |
The objective of the present invention is to provide a holding jig fixing device with which the positional accuracy and shape accuracy of a moving holding jig can be ensured and an aircraft panel can be assembled accurately. This holding...
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WO/2017/134459A1 |
The present invention aims to provide a modular jet trainer aircraft (1) which can be reconfigured to provide a plurality of different handling aircraft which will be particularly beneficial in the training of pilots. For example, the pr...
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WO/2017/134901A1 |
The objective of the present invention is to retain an aircraft panel in an appropriate shape and ensure the shape accuracy required in a production process in combination with a holding jig, and thereby to simplify the structure of a ho...
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WO/2017/134902A1 |
The objective of the present invention is to simplify the structure of a holding jig that retains the shape of an aircraft panel and retain the aircraft panel in an appropriate shape. This holding jig (1) is provided with a plurality of ...
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WO/2017/134899A1 |
The objective of the present invention is to provide an aircraft panel production method and aircraft panel production system with which an aircraft panel can be assembled accurately. This aircraft panel production method has: a step in ...
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WO/2017/131284A1 |
The present invention relates to a joined-wing type unmanned aerial vehicle. More specifically, the present invention relates to a joined-wing type unmanned aerial vehicle comprising: a fuselage; main wings formed on opposite sides of th...
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WO/2017/127509A1 |
A pawl latch (10) having a pin assembly (12) with a pin (22) and a receiver assembly (14) adapted to receive the pin assembly (12). The receiver assembly (14) includes a receiver housing (40) having a slider (50) positioned slidably on t...
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WO/2017/127504A1 |
Air stair support systems, stair support cable assemblies, and hooks are disclosed herein. A stair support system includes, but is not limited to, an aircraft fuselage, a door seal, a stair door, and a stair support cable assembly. The a...
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WO/2016/156438A9 |
A monument assembly (46) for an aircraft comprises at least one component of a primary structure of the aircraft, in particular a fuselage stiffening element (6, 84), a plurality of interconnected framework elements (12) for creating a s...
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WO/2017/121038A1 |
Provided is a folding unmanned aerial vehicle, comprising a fuselage main body (1), first and second wing frames (21, 22), at least one propeller set, and driving motors of a quantity the same as that of propellers (3). The two wing fram...
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WO/2017/117066A1 |
A hand-held emergency vision apparatus comprises an enclosed tubular structure having opposite first and second ends; first and second clear members disposed at respective the first and second ends; the structure including a plurality of...
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WO/2017/115749A1 |
The objective of the present invention is to provide: a resin composition for FRP, which is capable of suppressing whitening of fiber bundles; an FRP sheet; and a molded body. A resin composition for FRP according to the present inventio...
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WO/2017/107721A1 |
An unmanned aerial vehicle comprises an arm support (10), a connection member (20) rotatably connected thereto, and an arm (30) connected to the connection member (20). A fastener (210) is provided at the connection member (20). A fittin...
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WO/2017/107170A1 |
Disclosed is a battery (100), comprising a housing (11), an accommodation cavity (111) being provided in the housing (11), and a plurality of battery cells (13), the plurality of battery cells (13) being accommodated in the accommodation...
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WO/2017/107977A1 |
Disclosed is a multi-rotor air vehicle which is simple in structure and can be assembled and disassembled. A four-axis multi-rotor air vehicle or a six-axis multi-rotor air vehicle can be assembled by reusing components of an unmanned ai...
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WO/2017/107493A1 |
An aircraft support leg (2), the support leg (2) being movably connected to a main body of an aircraft. The support leg (2) can rotate to at least a first position and a second position. In the first position, an angle is provided betwee...
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WO/2017/107752A1 |
A multirotor manned aerial vehicle having foldable arms, comprising an aerial vehicle body (100), fixing mechanisms (1), connecting elements (2), and arms (3). The fixing mechanisms (1) are fixed on the aerial vehicle body (100). The arm...
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WO/2017/107412A1 |
An outer shell and a main body of an aircraft, and an aircraft. The outer shell comprises: an inner cavity (2a), the inner cavity being provided with a space for at least accommodating the main body components of the aircraft; an outer s...
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WO/2017/098232A1 |
An unmanned disposable air vehicle (1) comprising a structural part (3) that has an outer structure (17) and an inner structure (15) located inside the outer structure (17), the inner structure (15) being arranged to support the outer st...
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WO/2017/089926A1 |
A grommet for surrounding a conduit received through a hole in a part, including a grommet body configured for engagement with a perimeter of the hole in the part and defining a closed or substantially closed perimeter, and a plurality f...
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WO/2017/091337A1 |
A transparency includes a transparent substrate and a plurality of electrically conductive lines on the transparent substrate, at least one of the electrically conductive lines intersecting at least one other electrically conductive line...
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WO/2017/090031A1 |
A method of constructing a panel for an aircraft subassembly is provided.. The panel has interior and exterior sides relative to the subassembly and comprises a skin and a support structure. The support structure comprises a plurality of...
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WO/2017/085107A1 |
The invention relates to an aircraft (10) comprising at least one thermal insulation component (12) consisting of a nano-porous material whose pore structure is open-pored such that when the aircraft (10) is in flight operation, a pressu...
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WO/2017/081450A1 |
An airframe (10) for an air vehicle comprising an outer skin layer (12) and a support layer (13) defining a fuselage of said air vehicle, wherein said outer skin layer (12) is magnetically coupled to said support layer (13).
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