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WO/2012/013889 |
The invention relates to a suspension system of a fan jet. Said fan jet comprises an intermediate housing outer rim (13) attached to the front suspension and a primary structure attached to the rear suspension. The rim and the primary st...
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WO/2012/014272 |
A flight vehicle using the interaction between a wind flow and a stabilizer which is disposed along the direction of the flow of the wind flow in the wind flow to ensure the stability of a device or an airframe or the very stabilizer, wh...
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WO/2012/013333 |
An aerodynamic body (10), with at least one ancillary flap (14) arranged such that it can be moved on the aerodynamic body with the aid of a guide mechanism (25), and with a drive device (24) for purposes of actuating the ancillary flap ...
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WO/2012/013365 |
The invention relates to compensation for the torque which is produced by the main rotor (110) of a helicopter (100). The apparatus according to the invention for torque compensation is intended for a helicopter whose main rotor rotates ...
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WO/2012/013985 |
A headrest assembly (l) for an ejection seat, comprising: a support mounting ( 2 ); and a pair of inflatable side beams ( 3 ), each attached at one end to the support mounting and spaced apart from one another, the side beams ( 3 ) being...
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WO/2012/013351 |
To save weight und to enhance safety, a hydrogen tank 18 for supplying an engine 12 with hydrogen is attached externally to an aircraft 10.
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WO/2012/013878 |
The invention relates to a device (1) for non-destructively checking structures, and, for example, measuring the thicknesses of structures using an ultrasonic probe. The device comprises a drone (2), which is capable of hovering flight a...
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WO/2012/013464 |
The invention relates to an aerial device having a structure and a rotary element provided with at least one blade, suitable for rotating in relation to the structure, about a rotational axis, wherein the device is provided with a gas ge...
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WO/2012/013950 |
An apparatus for generating electrical energy at altitude, comprising a tether connecting a substantially ground level location, part to a platform at an elevated location, the tether comprising a conduit coupled to an electrical generat...
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WO/2012/013957 |
The invention provides a refuel control system for controlling refuel of at least one tank (111,112,113, 14,115,116) onanaircraft100,the refuel control system comprising monitoring apparatus (241, 242, 280, 371, 372, 380, 311, 312, 313, ...
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WO/2012/014224 |
This invention relates to a flying costume/jacket, which helps human being to fly in the sky, like a bird. A costume filled with helium / hydrogen etc. Equivalent to 40 cubic feet approximately will help a person to fly. Helium or hydrog...
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WO/2012/012904 |
The invention relates to an hydraulic shimmy damper including: - a hollow body (10) having an inner cylindrical surface and two end walls (13,14) defining an inner functional volume; - a piston (20) having a piston head (21) sealingly en...
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WO/2012/012474 |
A safe, quiet, easy to control, efficient, and compact aircraft configuration is enabled through the combination of multiple vertical lift rotors, tandem wings, and forward thrust propellers. The vertical lift rotors, in combination with...
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WO/2012/012275 |
A solar-powered airship with a hull configured to contain a gas and at least one propulsion assembly with a propulsion device and electric motors configured to drive the propulsion device. The airship may also include a power supply syst...
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WO/2012/012429 |
A tether, and system using such a tether, adapted to provide mechanical and electrical coupling of an airborne flying platform to the ground. The tether may have a center structural core with electrical conductors on or near the outer di...
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WO/2012/010305 |
The invention relates to a structural component (1), comprising at least one main-load-bearing covering shell (B) and a carrier structure (T) for fixing the covering shell, wherein the covering shell (B) is designed in the form of a sand...
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WO/2012/012752 |
The invention relates to a roadable aircraft vehicle (100) and related systems. An example roadable aircraft vehicle (100) includes a vehicle drive system (262) including an engine (264) and gearbox (206) selectively engageable with an a...
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WO/2012/012036 |
Methods and apparatus are provided to control flow separation of an ambient flow along a surface and about a turret (12), such as by reducing flow separation aft of the turret. By reducing flow separation, the resulting turbulence may be...
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WO/2012/010306 |
The invention relates to a main-load-bearing planking shell (B) for a structural component (1), wherein the planking shell (B) is designed with an outer edge section (60) having an outer edge (61) for attaching said shell to a support co...
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WO/2012/010304 |
The invention relates to a structural component (1) of a flow body, comprising at least one lining shell (B) that carries a main load, said lining shell having a core layer (33) that absorbs shear load and that comprises a plurality of c...
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WO/2012/010496 |
The invention relates to a monitoring device (30) for a repair patch (10) that can be placed on or in a wall of an aircraft for repairing a defect, having a sensor device (36) for capturing properties of the repair patch (10) placed in t...
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WO/2012/010021 |
An air-ground double-purpose aircraft comprises an aircraft body (47), an aircraft controller (1), an engine (38) and an undercarriage. Wherein a front ducted fan (9) which faces the wind at upper front is connected with the lower part o...
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WO/2012/010307 |
The invention relates to a planking panel (B) for a structural component (1), said planking panel being designed as a sandwich component in the inner region (B1) thereof that extends in a planar manner and comprising a first skin section...
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WO/2012/011996 |
An aircraft propulsion system is disclosed herein. The aircraft propulsion system includes a core engine having an intake, a compressor section, a combustor section, and a turbine section arranged along a centerline axis. The aircraft pr...
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WO/2012/011965 |
A modular spacecraft comprising: a capsule module comprising a common bulkhead, and [0090] an additional spacecraft module comprising a common bulkhead, wherein said capsule module's common bulkhead is attached to said additional spacecr...
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WO/2012/010882 |
The invention provides an arrangement and methods for thermally insulating aircraft, particularly but not exclusively for when the aircraft is operating in extremely hot or cold conditions, and describes an aircraft skin construction com...
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WO/2012/011452 |
Disclosed is a fixed-type seat, the seat back of which does not recline, which can take on a normal orientation and a rest orientation (corresponding to a normal reclined orientation). A cushion-material support mechanism which supports ...
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WO/2012/010782 |
The present invention relates to a turbine engine including two outer coaxial counter-rotating unducted propellers, i.e. an upstream propeller and a downstream propeller, respectively. Said engine is characterized in that the blades of t...
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WO/2012/011347 |
The disclosed table device makes it possible to use a table at just the right height without said table hitting the legs or the like of a user when said user pulls the table towards himself. The top (21) of the table (20) is supported by...
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WO/2012/010125 |
The invention relates to a method, device, and arrangement for removing organic soiling from front edges (21) of wings and from other incident-flow areas of an aircraft (10), wherein the soiling points are optically detected and said soi...
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WO/2012/010639 |
The invention relates to the generation of hydrogen for operating fuel cells in aircraft, wherein hydrogen is generated by reacting hydrogenated polysilanes (HPS) with water in a reaction chamber. The reaction chamber comprises a feed de...
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WO/2012/010774 |
The invention relates to a bypass turbojet engine nacelle (1) fitted with a thrust reverser device (20) comprising at least one cap (30) and flow deflection means (40), said cap (30) being able to move translationally in a direction subs...
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WO/2012/007360 |
The invention relates to a space situational awareness system including optical watch systems which are arranged as a network and are suitable for scanning areas of the Earth orbit, in particular the LEO layer, and which are arranged in ...
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WO/2012/009066 |
An article retention device (100) may be provided for a stowage bin (30). The stowage bin may include a bin interior (32) and may include a door panel (52) that is movable between open and closed positions. The door panel may have a door...
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WO/2012/006941 |
The present invention relates to a passenger seat, an assembled chair-bed dual-purpose seating unit, and a multi-purpose seating unit. A chair-bed dual-purpose seat comprises a support (3), a seat (2), a back support (1), and a back supp...
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WO/2012/007157 |
The invention relates to a method for early identification of the vortex ring phase for a helicopter, having the following steps: determination of flight control signals for flight control with respect to the vertical axis of movement of...
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WO/2012/007449 |
A beam (20) comprising first and second flanges (23, 24), the beam (20) having a first region (28, 30) extending between the flanges (23, 24) and a second region (26) extending between the flanges. The first region (28, 30) is designed t...
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WO/2012/009087 |
An aircraft flap actuator assembly (1) includes at least one fixed support (2), at least one track (40) having a curvilinear track surface (41) connected to the fixed support (2), at least one flap support (20, 24) adapted to traverse th...
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WO/2012/006930 |
An icing detector probe includes three sections arranged sequentially along the direction of air flow, namely, a first section (I), a second section (II) and a third section (III). Wherein, the shape of the outer surface of the first sec...
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WO/2012/006875 |
A suction-exhaust ventilated seat cushion according with human engineering comprises a chair cushion outer package (4) in which are provided with a backrest supporting frame (14) and a seat cushion supporting frame (5). Many tidily arran...
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WO/2012/007891 |
Disclosed is to a composite material, a structural element comprised of the composite material, an airplane wing spar and their methods of production. Some embodiments of the present invention include composite materials comprised of mul...
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WO/2012/007358 |
A wing tip device for fixing to the outboard end of a wing (401), the wing defining a wing plane, the wing tip device comprising: an upper wing- like element (404) projecting upwardly with respect to the wing plane and having a trailing ...
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WO/2012/009198 |
Various embodiments of the present invention include systems and methods for assessing the performance of an actuator of a attitude control system (ACS), such as a control moment gyroscope (CMG). In one embodiment, a system includes a su...
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WO/2012/009037 |
A rotor blade including a main portion having a main portion leading edge shield; a main portion impact-resistant layer formed on a nose of the leading edge shield; a main portion erosion-resistant layer formed on a top and bottom of the...
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WO/2012/007184 |
The invention relates to a vehicle (10) of modular construction, namely with a chassis (11) and a trailer (12) which is fully detachable from the chassis (11), wherein the trailer (12) comprises at least one functional unit (13), the veh...
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WO/2012/007362 |
The invention relates to a method for making a space watch system for the LEO areas of the Earth orbit, characterized in that said method comprises a step of providing and arraying stations of optical watch systems on the surface of the ...
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WO/2012/007361 |
The invention relates to an optical system for a watch system for a space watch system, characterized in that said optical system comprises at least one telescope having a field no lower than 5°, and preferably no lower than 10°, which...
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WO/2012/005600 |
An inflatable wing for a traction kite, the wing including: a flexible envelope having a first sheet and a second sheet, the first and second sheets joined together at a leading edge and a trailing edge; an inflatable leading edge spar l...
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WO/2012/004510 |
The aim of the invention is to allow the set of doors to be adjusted without increasing the number of landing gear retraction/extension manoeuvres, by incorporating a specific entrance in the fairing (2) of the landing gear bay (4) that ...
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WO/2012/004091 |
Apparatus, for example for a pitch change mechanism, comprising a cylinder having a magnetically encoding portion defining an annular array of features extending parallel to the longitudinal axis of the cylinder, the cylinder rotating in...
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