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WO/2016/124730A1 |
The invention relates to producing a panel with cross stiffening (10) having a high resistance to deformation, by implementing production steps without assembly or attachment. To achieve this, according to the invention such a panel (10)...
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WO/2016/125180A1 |
A cockpit internal anti-sabotage system (CIASS) without compromising the cockpit security and the present anti-hijacking procedure and protocol, wherein a single cockpit crew alone in the cockpit cannot deny bonafide entry of other cockp...
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WO/2016/120755A1 |
A sealed component assembly within an aircraft, comprising first 10 and second 12 components each facing surfaces, and a sealing member 20 extending between the facing surfaces. The sealing member includes a conductive portion 22 sandwic...
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WO/2016/119065A1 |
Systems, methods and devices for use with unmanned aerial vehicles (UAV). A central controller is coupled to the autopilot system for a UAV. Navigation is implemented by using two GPS antennas and obtaining a difference between the locat...
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WO/2016/116902A1 |
Embodiments of the present disclosure relate generally to the use of the fuel cell systems on board aircraft and other passenger transportation vehicles and to methods of using heat, air, and water generated by such fuel cell systems. Th...
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WO/2016/107944A1 |
Fuselage rear end of an aircraft, comprising: - a structural part (1) comprising a skin and longitudinal (30) and transversal reinforcing members (31, 32), and - a fairing (5). The structural part (1) longitudinally spans over the whole ...
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WO/2012/054080A9 |
A cargo storage and handling system for aircraft. A rack assembly mounts in an upper portion of the fuselage to form a cargo area in the upper lobe thereof. The rack includes a series of frames that are suspended from pre-existing attach...
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WO/2016/105638A2 |
A battery containment pod including a body formed of a lightweight material. The body has an aerodynamic exterior shape and an interior cavity formed in the lightweight mate-rial, the size and shape of the interior cavity designed to acc...
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WO/2016/095886A1 |
Known towed bodies can be maneuvered in all three dimensions but, as pure airborne targets, do not have a large load capacity. The towed body (01) according to the invention is designed for bearing large loads and serves exclusively scie...
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WO/2016/096528A1 |
A deformation structure (1), which can also be called an energy absorption structure, comprising a series of deformation elements (3) arranged one behind the other in a deformation direction, i.e. the direction in which a load acts, wher...
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WO/2016/098426A1 |
This structure is provided with first composite materials 11, a second composite material 12 joined to the first composite materials 11 by a film adhesive 21 provided between the first composite materials 11, and a corner fillet part 13 ...
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WO/2016/097939A1 |
Sound absorbers and airframe components comprising such sound absorbers are disclosed. In one embodiment, an airframe component comprises an aerodynamic surface (48) and a sound absorber (38). The sound absorber (38) comprises a perforat...
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WO/2016/098442A1 |
A composite structure (10) provided with a first composite member (11), a second composite member (12) joined to the first composite member (11), and a corner fillet section (13) disposed in a corner section (15) formed by the first comp...
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WO/2016/090051A1 |
A cargo stop for use with a tie down strap with attachment members attachable to anchors in a floor of a cargo compartment usable for carrying cargo. The cargo stop having an elongated cargo engagement wall member portion with a rearward...
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WO/2016/088470A1 |
A member is provided with a first composite member (11) which is made from a plastic that is reinforced with heat-conductive carbon fibers comprising metal-coated carbon fibers and/or pitch-based carbon fibers, wherein one end of the hea...
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WO/2016/085984A1 |
A thermal/acoustic insulation product, such as for an aircraft, comprising a block of flexible, open-celled, cellular foam having a predefined shape and having a thermoformed amorphous film covering that completely envelops the foam bloc...
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WO/2016/078562A1 |
Disclosed in the present invention is a high-speed aircraft, comprising a shell and an engine, an outer fluid channel and an inner fluid channel being arranged in succession within the shell, the outer fluid channel and the inner fluid c...
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WO/2016/079247A1 |
The subject of the invention is a conductive device (11) for forming electrical connections on the surface of a structure (15) made of composite material. The device includes a thin interface layer (13) having a face via which the device...
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WO/2016/077275A1 |
A solar window shade for a window seat in an airliner for supplying electrical energy to charge a personal electronic device, including a window shade (12) configured to cover a window, a solar panel (14) attached to an outside face of t...
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WO/2016/075001A1 |
The invention relates to a device for the machine-production of a packing material product consisting of a single-ply or multi-ply continuous paper web, said device comprising a feed system for drawing the paper web into the device, thus...
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WO/2016/062176A2 |
Disclosed is an unmanned agricultural helicopter, comprising a fuselage body. The fuselage body comprises a frame. Provided on the frame is a rotor head for fastening a main rotor, the main rotor being disposed on a large blade clip of t...
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WO/2016/050514A1 |
The invention relates to a storage lift for an airplane, comprising a first raising device (1 ), wherein the raising device (1 ) is designed to releasingly hold a first container (4), and wherein the raising device (1 ) can be lifted wit...
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WO/2016/038097A1 |
The invention relates to an aircraft having a fuselage and wings connected thereto, wherein a support strut extends in each case between the fuselage and the wings, said support strut being connected both to the fuselage and the wing. Th...
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WO/2016/034649A1 |
The invention seeks to allow positive transmission of load between the assembly structures of a transport vehicle floor (2) and tolerance on positioning and/or on relative-adjustment movements in the plane of this floor (2). In order to ...
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WO/2016/033030A2 |
An adjustment tool is provided including a block having a plurality of sides including a first side and a second side. A hole is formed in the block such that a first distance between the center of the hole and the first side is differen...
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WO/2016/033441A1 |
Thiol-terminated polythioether compositions and sealants prepared using the thiol-terminated polythioether compositions that exhibit enhanced retention of elongation following exposure to high temperature are disclosed. The enhanced rete...
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WO/2016/024276A1 |
A disposable unmanned aerial glider (UAG) with pre-determined UAG flight capabilities. The UAG comprises a flight module comprising at least one aerodynamic arrangement; and a fuselage module comprising a container configured for storing...
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WO/2016/022209A1 |
A passenger boarding procedure is disclosed which eliminates disadvantages associated with conventional techniques. In some embodiments, passengers may be physically arranged in a pre-boarding waiting area largely as they would be seated...
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WO/2016/020319A1 |
An aircraft interior lining component (10) is composed at least partially of a thermoplastic foam material and comprises a first surface (12) which faces an interior of an aircraft cabin (14) when the aircraft interior lining component (...
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WO/2016/012763A1 |
Aircraft frame structure, method of making an aircraft frame structure, method of repairing an aircraft and aircraft component An aircraft frame structure is provided comprising a grid support (typically a geodetic support) (2) and (i) a...
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WO/2016/010592A1 |
A method of improving optical characteristics of an optical window (100) operating in a flow of fluid and having first and second panes (104, 106) of optically transmissive material - each having an edge (114, 116) adjacent to, parallel ...
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WO/2016/010842A1 |
A modular mounting structure (12) is described which allows for the easy installation and removal of various payloads (30) from an air vehicle structure (12). An embedded electrical bus feature (18) further supports the installation of t...
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WO/2016/009075A1 |
An aircraft fuselage comprises a structure, considered in respect of all or part of the fuselage, with fuselage upper panels (12) constituting an upper part of the fuselage and a fuselage bottom structure (13) constituting a lower part o...
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WO/2016/007663A1 |
A telescoping aircraft door is disclosed having first and second panels that slide relative to one another to extend and retract as the door closes and opens, respectively. The first panel is hinged to the door frame in a traditional man...
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WO/2016/007796A1 |
A helicopter-hoist system is described. The system may include: hoist equipment, illumination systems, range-measuring equipment, camera(s), communication systems, display devices, processing/control systems including image-processing sy...
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WO/2016/004096A2 |
A panel assembly that includes a front skin having a front surface, a back surface and at least one crush section portion, a core assembly that includes first, second, third, fourth and fifth layers laminated together, and at least a fir...
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WO/2016/000485A1 |
An I-beam fuselage structure of an unmanned helicopter, comprising two side frames and a rotor blade frame installed between the side frames; the side frames are I-beams; the fuselage structure utilizes I-beams as the main structural bod...
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WO/2015/196418A1 |
The present invention discloses an aircraft and a signal line protection assembly thereof. The signal line protection assembly comprises a stand and a protective cover; the stand comprises a stand cover; at least one part of the protecti...
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WO/2015/200209A1 |
Unmanned aerial vehicles and associated systems and methods are disclosed. A representative unmanned aerial vehicle includes a wearable, flyable support structure, and a propulsion system carried by the support structure. The propulsion ...
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WO/2015/193559A1 |
The invention relates to a method for manufacturing a seat rail (200) including a plurality of portions: a head (210) provided on the longitudinal plane of symmetry thereof with a preformed rack groove (211) receiving the seat attachment...
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WO/2015/187837A1 |
A window assembly includes a pressure pane and a bezel proximate a periphery of the pressure pane and defining an inner opening. The bezel includes an inner wall with a channel. An electro-optic element is disposed in the inner opening a...
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WO/2015/181030A1 |
A pressure bulkhead (1) for an aircraft fuselage is depicted and described, having a skin element (3), which has a first surface (7) and a second surface (9), as well as a circumferential edge (11) and a center axis (13), and having a re...
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WO/2015/181801A2 |
Embodiments of the present invention provide systems and methods for allowing use of what has traditionally been a cargo area of a passenger aircraft to be used as a lower deck passenger cabin. Various modifications to the aircraft are d...
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WO/2015/173694A1 |
The present disclosure describes a bulkhead assembly for an aircraft interior comprising a pocket door mechanism (48) for supporting and guiding the movement of a pocket door; and a structural member (50) to which the pocket door mechani...
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WO/2015/171605A1 |
A thin, cured gel gasket is disclosed, including methods of making the thin gel gasket and the use of the thin gel gasket in an aircraft joint. In one embodiment, the thin gel gasket has no skeleton or other structure and is comprised of...
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WO/2015/169279A1 |
The invention relates to a multifunctional boom (1) with at least one drive (2), in particular for use in a multicopter system. At least three of the multifunctional booms (1) are connected together to form a support system (3). A first ...
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WO/2015/167949A1 |
A positionally releasable vehicle armor arrangement includes, at least one plate positioned proximate a hatch of a hatchway of a vehicle configured to shield an occupant of the vehicle from projectiles, at least one retainer in operable ...
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WO/2015/165651A1 |
The invention relates to an aircraft having a pusher propeller (18), a rear tail assembly (20) and a connection (22) by means of which the tail assembly (20) is fastened. According to the invention, the connection (22) comprises a sound-...
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WO/2015/163764A1 |
An integrated panel made of interconnected laminates comprising stacked first and second metal layers (5, 5', 5") and fibre-reinforced adhesive layers (19) between adjacent metal layers. At the location of the transition from the outer s...
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WO/2015/155477A1 |
The invention relates to a structural assembly (1) of an aircraft turbojet engine nacelle and a thermal protection mat (2) attached to the structure (1), the mat being attached to said structure (1) via at least one attachment device, th...
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