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Matches 1 - 50 out of 5,521

Document Document Title
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 ...  
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...  
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...  
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 ...  
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...  
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...  
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...  
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 ...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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 ...  
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...  
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...  
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: ...  
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...  
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...  
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...  
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, ...  
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, ...  
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...  
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...  
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...  
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...  
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 ...  
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)...  
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...  
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...  
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...  
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...  
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...  
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)...  
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...  
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...  
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...  
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...  
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...  
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 ...  
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...  
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...  
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...  
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...  
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 ...  
WO/2018/183750A1
A panel assembly that is configured to be secured to a frame that includes a panel having a top and a bottom, a first bracket assembly and a second bracket assembly. The first bracket assembly includes a first pivot member and a first br...  
WO/2018/177449A1
The invention relates to a cabin lining element (18') for an aircraft cabin arranged in the interior of an aircraft fuselage structure (12), having a fuselage structure side (30) and a cabin side (32). On the fuselage structure side (30)...  
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...  

Matches 1 - 50 out of 5,521