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WO/2019/041875A1 |
Provided are a foldable frame and an unmanned aerial vehicle. The foldable frame comprises: a body (2); a connection arm (1) rotatably connected to the body (2); a first magnetic element (3) mounted on the connection arm (1); and at leas...
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WO/2019/037242A1 |
Disclosed are an arm assembly, a frame, and an unmanned aerial vehicle, wherein the arm assembly (10) is fitted on a main frame body (101), and the arm assembly (10) comprises a main arm body (11), a power assembly (12) arranged on the m...
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WO/2019/029387A1 |
An aircraft and an arm assembly (10) and frame thereof, the arm assembly (10) comprising: an elastic locking member (100), a fixing seat (200) and an arm (300); the arm (300) is rotatably connected to the fixing seat (200) such that the ...
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WO/2019/024806A1 |
Disclosed is an unmanned aerial vehicle, comprising a fuselage (1), a shell assembly (3) and a functional component. The fuselage comprises a fuselage body (10). The shell assembly (3) is connected at a front end of the fuselage body. Th...
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WO/2019/026350A1 |
A landing gear for a rotary-wing aircraft according to one embodiment of the present invention comprises two skid-tubes, and a cross-tube for linking the two skid-tubes and attaching the two skid-tubes to a fuselage of the rotary-wing ai...
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WO/2019/025343A1 |
The invention relates to a fastening unit (100) for movably fastening an aircraft component (300) to a support structure (400) of an aircraft (500). The fastening unit (100) has a connection element (5) having a hole (5a). The fastening ...
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WO/2019/024541A1 |
An arm (11) and an unmanned aerial vehicle (100). The unmanned aerial vehicle (100) comprises a body (20), arms (11) connected to the body (20), and a power device disposed on the arms (11); the folded arms (11) can be attached to the ex...
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WO/2019/024215A1 |
An arm (10), comprising a first sub-arm (12), a second sub-arm (14), and a sleeve (16); the second sub-arm (14) is rotatably connected to the first sub-arm (12); a connection joint (13) is formed between the first sub-arm (12) and the se...
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WO/2019/019397A1 |
An unmanned aerial vehicle arm assembly, an unmanned aerial vehicle frame, and an unmanned aerial vehicle. The unmanned aerial vehicle arm assembly (100) is applied to the unmanned aerial vehicle (300) and comprises an unmanned aerial ve...
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WO/2019/018621A1 |
An example embodiment includes a landing pad having a housing and a power terminal configured to draw electric power from a power source. The landing pad further includes an electrically conductive landing terminal dorsal to the housing ...
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WO/2019/018847A1 |
A mounting system for mounting an element to a surface includes a mounting element 76 having a base 78 and a threaded shaft 80 extending from the base along an axis. The base is configured for mounting to a surface. An incremental nut 92...
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WO/2019/015129A1 |
Disclosed is a portable multi-rotor unmanned aerial vehicle, comprising a frame (10) and a plurality of arms (20). Electric motors (30) and blades (40) are arranged at tail ends of the arms (20). Each of the arms (20) comprises a first a...
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WO/2019/012286A1 |
A one-piece fitting (56) for a stiffened panel (51) comprising a panel body (52) with a plurality of stiffeners (53, 54, 55) arranged thereon, the fitting comprising a fitting body (56) configured to be fastened, in use, to two or more o...
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WO/2019/010568A1 |
A wire brace including two interconnected arms identical to each other, each having a first end having a first connection member, a second end opposed to the first end and having a second connection member complementary to the first conn...
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WO/2019/008291A1 |
The invention relates to a laminated glazing including first and second glass sheets (1; 3) bonded by a first intermediate adhesive layer (2), a peripheral zone of the laminated glazing being covered with a stepped metal element (7), whe...
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WO/2019/008290A1 |
The invention relates to a laminated glazing including first and second glass sheets (1; 3) bonded by a first intermediate adhesive layer (2), a peripheral zone of the laminated glazing being covered by a stepped metal element (7), where...
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WO/2019/008289A1 |
The invention relates to laminated glazing comprising a first glass sheet and a second glass sheet (1; 2) bonded by means of an adhesive interlayer (2), a peripheral zone of the laminated glazing being covered with a tiered metal element...
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WO/2018/234199A1 |
A metallic structure with a reinforced skin according to the invention (1), comprises at least one skin (10) and local reinforcement (3a) connected to the skin (10). Each local reinforcement (3) has a transition zone (31a) extended by a ...
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WO/2018/232787A1 |
Disclosed is a fixed-wing unmanned aerial vehicle which takes off and lands vertically, comprising a body (1), a wing (2) fixedly arranged on the body (1) and an empennage fixedly arranged at the tail of the body (1), and further compris...
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WO/2018/234316A1 |
Method for producing a component (1) from a fibre composite material, comprising the steps of: introducing a matrix-impregnated fibre (1) onto a cylinder-like inner mould (7) of a mould space formed between the inner mould (7) and a cyli...
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WO/2018/230818A1 |
The present invention relates to an unmanned aerial vehicle for inspecting a high-voltage line and a control method therefor. The unmanned aerial vehicle for inspecting the high-voltage line according to the present invention comprises: ...
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WO/2018/226549A1 |
A radome assembly (20) includes a frame (30) conforming in contour with an aircraft fuselage (14) for being fixedly mounted thereto. A radome (32) having an aerodynamically streamlined elongate contour including a central bulb (34) is sp...
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WO/2018/225706A1 |
A sound-absorbing panel to be used affixed to a jet engine of an aircraft, provided with: a resin core layer 20 having a first surface, a second surface disposed on the side opposite from the first surface, and multiple partitions extend...
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WO/2018/218321A1 |
Cargo aircraft having a cargo ramp and cargo door oppositely hinged relative to one another to allow access to the aircraft's cargo space may be provided with a flying boom mast that is physically mounted at the aft portion of the fusela...
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WO/2018/214233A1 |
The present invention provides a heat dissipation window assembly (10) and an unmanned aerial vehicle. According to the present invention, the heat dissipation window assembly (10) is used to implement heat dissipation on a heat source, ...
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WO/2018/209428A1 |
A low noise aircraft comprising a fuselage comprising a nose section, a cabin and a tail comprising an empennage, the profile of the fuselage tightening towards the tail, two wings mounted on opposite sides of the fuselage, two engines, ...
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WO/2018/210649A1 |
An airframe for a hovering air vehicle (HAV) comprising a body portion and a plurality of arms for supporting an assembly of rotatable blades which in use provide lift and propulsion for the HAV, the arms being movable relative to the bo...
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WO/2018/211234A1 |
A door assembly for a vehicle, the door assembly comprising: a door; a stiffening structure fixed to a surface of the door, the stiffening structure comprising a first wall spaced apart from and substantially parallel to the surface of t...
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WO/2018/211232A1 |
A stiffening structure for an aircraft panel or door and method for fabricating the same, the method comprising: providing a thermoplastic continuous fibre-reinforced composite material comprising a plurality of continuous fibres embedde...
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WO/2018/209911A1 |
A vertical take-off and landing (VTOL) unmanned aerial vehicle having a foldable fixed wing and based on a twin-ducted fan power system. The unmanned aerial vehicle employs a twin-ducted fan power system (7) arranged at a tail portion of...
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WO/2018/211076A1 |
The invention concerns a modular arrangement intended to accommodate at least one passenger of an aircraft, comprising at least one module (18, 22), configured to be arranged in a removable manner in a cargo area (2) of the aircraft, in ...
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WO/2018/211077A1 |
The invention concerns an aircraft cabin comprising: - an upper deck (70), - a cargo area (2) configured to accommodate at least one passenger and situated at a different level to the upper deck (70), and - at least one access means (16)...
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WO/2018/203189A1 |
Assemblies and methods for facilitating the assembly of aircraft wings to a fuselage are disclosed. In some embodiments, a wing unit includes features that are configured to define one of more parts of a pressure vessel that is partially...
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WO/2018/122769A9 |
Working with the traditional soda lime float glass, there is a limit on how thin an automotive laminate can be while still meeting all of the functional and safety requirements. By using alternate glass compositions and chemical temperin...
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WO/2018/203191A1 |
Assemblies and methods for facilitating the assembly of aircraft wings to a fuselage are disclosed. In some embodiments, a wing unit includes features that are configured to define one of more parts of a pressure vessel that is partially...
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WO/2018/203190A1 |
Assemblies and methods for facilitating the assembly of aircraft wings to a fuselage are disclosed. In some embodiments, a wing unit includes features that are configured to define one of more parts of a pressure vessel that is partially...
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WO/2018/203805A1 |
The present invention regards a body structure (1) of a vehicle (3), comprising a door structure (5), whereby an interface (7) is defined between the body structure (1) and the door structure (5), which door structure (5) is configured t...
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WO/2018/201417A1 |
Disclosed are a deformable aircraft, a mobile platform and an operating method therefor. The deformable aircraft comprises: a fuselage (110), the fuselage comprising a first fuselage portion (111) and a second fuselage portion (111), whe...
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WO/2018/196810A1 |
Disclosed is an aircraft, comprising a fuselage (1) and a wing (2), a first open channel (12) for extending the fluid flow path being provided at a front portion (211) and/or a middle portion (212) of a windward side (21) of the wing (2)...
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WO/2018/197801A1 |
The invention relates to a system for securing a glazing to the vehicle structure, comprising a first, outer primary half-frame (1) and a second, inner primary half-frame (2), the first and second primary half-frames (1) and (2) being at...
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WO/2018/197956A1 |
The present invention provides an aircraft (100) with increased lift generation and additional cabin space. The aircraft (100) comprises a fuselage (110), a plurality of wings (120) attached on either side of the fuselage (110), and a fi...
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WO/2018/199091A1 |
Provided is a laminate composite that has flame resistance and low-smoke capacity, and also has high mechanical characteristics. The laminate composite has a laminate structure including at least one core layer and at least one skin laye...
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WO/2018/196298A1 |
Disclosed are an arm (11, 11a), a power assembly (10) and an unmanned aerial vehicle (100), the arm (11, 11a) comprising: a primary arm (111, 111a) and a secondary arm (112, 112a), wherein the primary arm (111, 111a) is mounted on a vehi...
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WO/2018/195786A1 |
Provided is an unmanned aerial vehicle (100). The unmanned aerial vehicle (100) comprises: an aerial vehicle main body (1), a main board (10) arranged in the aerial vehicle main body (1), and an upper cover (2) mounted on the aerial vehi...
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WO/2018/193192A1 |
A surface trim element (10) comprises a superficial wall (1) which is provided with multiple holes (2), a spacer structure, and tubes (3) which are respectively associated with the holes of the superficial wall. The surface trim element ...
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WO/2018/194728A1 |
A plug door assembly for a pressurized aircraft is provided. The door assembly includes a surround and a door, and connector assemblies along the edges that act to transfer in-plane stresses directly across the fuselage opening via the d...
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WO/2018/188188A1 |
An upper cover (100) of an unmanned aerial vehicle, mounted on a body (200) of the unmanned aerial vehicle. The body (200) is provided with a first positioning member (202) and a plurality of first clipping members (204). The upper cover...
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WO/2018/185377A1 |
A composite element and a method of manufacturing the same. The composite element comprises a first skin plate (17) and second skin plate (23), which are manufactured as separate pieces and are assembled in a separate phase. At least the...
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WO/2018/185978A1 |
The purpose of the present invention is to provide a seat unit, and a bottom structure thereof, not subject to constraints on the positional relation with a seat track preinstalled in an aircraft. In one representative embodiment, one of...
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WO/2018/183996A1 |
A propulsion system for an orbiting vehicle such as a low-Earth orbit (LEO) satellite includes a set of surfaces over which a gas passes during orbital flight, and a plurality of electrodes on the surfaces. The electrodes are configured ...
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