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Matches 1 - 50 out of 5,454

Document Document Title
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...  
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 ...  
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...  
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...  
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...  
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...  
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), ...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
WO/2018/122769A1
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...  
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. ...  
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. ...  
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...  

Matches 1 - 50 out of 5,454