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WO/2017/053913A1 |
A truss-reinforced radome crown structure (TRRCS) that functions in combination with an aircraft and a communication radome or antenna. The TRRCS maintains and protects a radome and antenna located on an aircraft's fuselage. The TRRCS in...
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WO/2017/051313A1 |
A window system for an enclosure subjected to a change in air pressure, the enclosure having a window having an air-filled cavity, the system including a first path configured to allow air within the cavity of the window to vent out of t...
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WO/2017/048122A1 |
Described is a laminate, comprising a stack of mutually bonded adhesive layers and metal sheets. The laminate comprises abutting and/or overlapping metal sheet edges that extend along a length direction within a splicing region. A splice...
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WO/2017/047281A1 |
Provided are: a functional film; and an aircraft window structure. This functional film (100) is sequentially provided, on a first main surface of a transparent film base (10), with a functional thin film (20) that is composed of a lamin...
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WO/2017/042165A1 |
The invention aims to achieve an emergency opening of a vehicle closing element with a minimum of operations and in a minimum of time, without substantially increasing the space requirement or the weight. To do this, a near-instantaneous...
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WO/2017/033033A1 |
The present invention relates to a safety system for flying vehicles, for securely rescuing the passengers and/or the crew and/or some specific cargo in the flying vehicle in case of an emergency or an accident. The safety system of the ...
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WO/2017/029180A1 |
An aircraft door arrangement (2) for an aircraft fuselage (18) comprises an aircraft door (4), at least one door seal (8) arranged at an inner side of the aircraft door (4) extending circumferentially in an edge region of the aircraft do...
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WO/2017/020763A1 |
An unmanned aerial vehicle comprises an aerial vehicle body (1), the aerial vehicle body (1) comprising a fuselage (2) and a storage device (4); aerial vehicle arms, the aerial vehicle arms comprising at least two front aerial vehicle ar...
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WO/2017/018813A1 |
A first embodiment relates to a shape-reconfigurable drone and, more specifically, to a shape-reconfigurable drone comprising unit module drones having a rectangular-parallelepiped body capable of applying a thrust in every direction, th...
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WO/2017/018107A1 |
Provided is an assembly system (600) equipped with gripping devices (300, 301) for conveying a sheet-shaped structural member, an assembly jig for positioning the sheet-shaped structural member, and a control device (500). The assembly j...
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WO/2017/019165A1 |
A transparency, e.g. an aircraft laminated windshield, includes one or more moisture sensors (85, 87) to monitor moisture penetration to monitor performance of the moisture barrier (36). At least one of the moisture sensors (85, 87) incl...
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WO2017010439A1 |
[Problem] To configure the frame supporting an unmanned aerial vehicle so as to be lightweight and strong. [Solution] An unmanned aerial vehicle 1 is equipped with: an upper frame 10 that is formed by connecting, at intersection points, ...
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WO/2017/007345A1 |
A joining member having a first portion with a first base, a first base wall, a plurality of first extensions, a first locking tip at a distal end of each of the plurality of first extensions, and at least one stop member. A second porti...
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WO/2017/006738A1 |
Provided is a mounting jig for positioning a plate-like structural member (200) having a pair of positioning holes (220) formed at the opposite ends thereof. The mounting jig is provided with: a support section (110) for supporting the l...
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WO/2017/003671A1 |
A latching mechanism is provided for engaging an aircraft surface panel to a support member. The aircraft panel is provided with a post extending from the lower surface, which extends through a panel support member into a post engagement...
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WO/2017/001792A1 |
The invention relates to: laminated glazing (1) including a first structural ply (4) attached to a first sheet of glass (2) of 0.5 to 1.5 mm in thickness by means of a first adhesive interlayer (3), said first sheet of glass (2) making u...
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WO/2016/207792A1 |
A partition assembly (16) for an aircraft cabin, including a bulkhead (18) with first (28) and second (30) internal compartments having respective first (32) and second (34) open ends defined in a same side of the bulkhead (18), one of t...
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WO/2016/209889A1 |
A unitary core panel for a composite sandwich structure includes a plurality of cell walls defining a plurality of core cells, the plurality of cell walls extending across a thickness of the core, the plurality of core cells including on...
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WO/2016/201087A1 |
An aircraft window includes an outer window assembly that includes a pressure pane coupled to a pressure pane frame. An inner window assembly includes a bezel adapted to couple to a perimeter of the inner window assembly against the oute...
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WO/2016/199660A1 |
This working machine is provided such that a working head can be automatically moved in an X-axis direction as well as in a θ-axis direction, and the structure of a θ-axis drive mechanism can be simplified in order to prevent the worki...
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WO/2016/199979A1 |
Disclosed is a corrugated buffering member having a variable thickness. The disclosed corrugated buffering member having a variable thickness comprises a corrugated plate having a corrugated surface formed in a direction perpendicular to...
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WO/2016/201112A1 |
A window mounting assembly includes a multi-piece bezel having a first portion having an attachment feature, and a second portion having a retention feature. The retention feature is configured to engage the attachment feature such that ...
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WO/2016/192022A1 |
A system and kit for dissipating heat generated by a motor assembly and methods for manufacturing and using same. The motor assembly includes a housing that defines an internal chamber. The internal chamber communicates with an air inlet...
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WO/2016/190911A2 |
A system and method to release a subject device includes a passage associated with the subject device, the passage having a first end and a second end, at least one hinged door associated with the second end of the passage, and at least ...
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WO/2016/184940A1 |
The invention relates to a composite structure comprising a composite sandwich panel (1) consisting of a first skin (10) and a second skin (11) on either side of a core (12), comprising at least one extension of an edge of the composite ...
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WO/2015/162542A9 |
Several embodiments of buffer zones are provided that are contemplated to be disposed with respect to two or more adjacent elements on an aircraft. The buffer zones adjust for dynamic spacing between the elements to help control differen...
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WO/2016/184358A1 |
A fixed structure type vertical take-off and landing aircraft based on dual flying control systems, comprising an aircraft structure and flying control systems; the aircraft structure comprises an aircraft body (1-1, 2-1), fixed wings, a...
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WO/2016/181085A1 |
The invention relates to a part (10) made of a composite material, comprising a T-shaped stiffener (12) mounted on a supporting face (14) of a base (16), the stiffener (12) comprising a first L-shaped element (18a) and a second L-shaped ...
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WO/2016/174544A1 |
An acoustic abatement apparatus for an aircraft includes a layer of material disposed exterior to a fuselage of the aircraft, where the layer of material connects to the fuselage to establish a gap between the layer of material and the f...
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WO/2016/166256A1 |
The invention relates to an aircraft comprising a cockpit having at least two seats arranged laterally one next to the other and transversely to the direction of flight, a upwardly-pivotable cockpit hood which, when pivoted upwards, rele...
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WO/2016/167865A1 |
One aspect is a flight control system for a coaxial rotary wing aircraft including a main rotor system and an active elevator. The flight control system includes a flight control computer with processing circuitry that executes control l...
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WO/2016/161975A1 |
The present invention provides an aircraft fuselage and an aircraft with the same. The aircraft fuselage includes an upper fuselage and a lower fuselage. The upper and lower fuselages are connected through ultrasonic welding or gluing. T...
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WO/2016/162241A1 |
A passenger cabin area (10), which is suitable for installation in an aircraft cabin, comprises a plurality of passenger seats (12) arranged one behind another along a longitudinal axis (L) of the passenger cabin area (10). The passenger...
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WO/2016/157223A1 |
Multi-material coupled panel to be used inside aircraft compartments comprising a first layer (11) in thermo-formed polycarbonate, a second layer (13) in insulating material glued to said first layer by means of an adhesive layer and a t...
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WO/2016/160061A1 |
A coated substrate includes: a substrate; an electrically conductive multilayer stack on the substrate; and a coating on the electrically conductive multilayer stack. A thickness of the coating is 5 to 10 mils and the coating includes a ...
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WO/2016/156298A1 |
The invention relates to a device for equalizing a pressure difference for an aircraft, comprising - a planar separating wall (1), which is fixed to the aircraft and separates a first space (2) from a second space (3) in respect of flow,...
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WO/2016/158476A1 |
Provided is a structural body production device (100) that is provided with a constant current source (10) that applies current at a prescribed current value to a gap, which is between an electrically conductive composite material (31) a...
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WO/2016/150908A1 |
The invention relates to a mounting device for mounting functional devices (30) within a cargo hold (10) of an aircraft. The mounting device comprises at least one surface unit (20) and a plurality of functional devices (30), which can b...
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WO/2016/150891A1 |
Floor modules for an aircraft cargo hold that have a cover element (10) and a floor element (20), which is spaced apart from the cover element at least in some segments and is attached to an underside of the cover element, are known. The...
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WO/2016/151496A1 |
A single-skinned composite lattice sandwich structure (400) includes a face sheet (402), fiber stringers (408), and at least one fiber tow arranged in a lattice structure (404) separating the face sheet (402) and fiber stringers (408), T...
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WO/2016/149614A1 |
A shock resistant fuselage system includes first and second fuselage side walls (804, 806), each of the first and second fuselage side walls (804, 806) having a plurality of guide posts (802, 1006), and a printed circuit board (PCB) 800 ...
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WO/2016/146716A1 |
The invention relates to a device for fireproofing a section of a structural part (100) formed of a composite material. Said device is characterized in that it comprises: a. a skin (110, 210) comprising an outer surface that is intended ...
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WO/2016/142517A1 |
The invention relates to a vehicle component having at least one sandwich part which forms a crash element that absorbs kinetic energy. The at least one sandwich part (1; 1'; 101) has a layer structure (10; 10'; 10) of at least two fiber...
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WO/2016/142559A1 |
The aircraft forms a supporting volume that includes at least part of the central body in which the cargo to be transported is accommodated, preserving said volume, a conventional wing profile in the longitudinal direction of the aircraf...
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WO/2016/141742A1 |
Disclosed is a fixed-wing unmanned aircraft capable of being quickly disassembled and installed, comprising an aircraft body, and a wing and a tail installed on the aircraft body, wherein the tail comprises a tail wing and a tail rod fix...
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WO/2016/141743A1 |
Disclosed are an electric motor mounting base, a reinforcement and a multi-rotor unmanned aircraft. The electric motor mounting base comprises a vertically arranged end plate, and a first and a second fixed plate extending in a horizonta...
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WO/2016/139465A1 |
An unmanned high altitude aircraft operating above 15 km with transmitting and/or receiving antennas, enclosed or more than half enclosed on a projected area basis normal to the plane of the antenna (s), in a wing structure where the cho...
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WO/2016/139296A1 |
The invention aims to produce a sealed end comprising a limited number of parts while producing an optimised compromise between energy absorption and rigidity in such a way as to be able to resist violent shocks caused by the impact of f...
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WO/2016/132073A1 |
The invention relates to an aircraft propulsion unit comprising: a turbine engine (1) having at least one unducted propulsion fan (4a), and an attachment pylon (3) intended to attach the turbine engine to a structural element (2) of the ...
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WO/2016/130296A1 |
A magnetic latching system is provided for removably latching a panel to an aircraft surface portion. The latching system includes a removable axis panel engageable to a latching land. The panel and land define opposing magnetically attr...
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