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WO/2012/125597 |
A spacecraft reaction control system comprising: a spacecraft having a center of mass; a length of free tether extending from said spacecraft and offset from said spacecraft's center of mass, such that a force exerted upon said spacecraf...
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WO/2012/123757 |
The present invention provides a method and system of determining the ground-to-tyre friction coefficient for an aircraft landing event, the method comprising: • providing a plurality of aircraft data parameters (2) including air craft...
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WO/2012/124594 |
A control system (6) of an aircraft (1) comprises: a computer (15) which controls flight on the basis of either a flight control law (20) for controlling flight by controlling the angles of control surfaces (3) or a control surface/thrus...
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WO/2012/125052 |
The invention pertains to aeronautical engineering and consists of an airborne platform that can be built to large sizes without requiring a rigid structure of comparable dimensions and which uses both buoyancy and the aerodynamic Magnus...
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WO/2012/125052 |
The invention pertains to aeronautical engineering and consists of an airborne platform that can be built to large sizes without requiring a rigid structure of comparable dimensions and which uses both buoyancy and the aerodynamic Magnus...
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WO/2012/125600 |
In an aspect, the invention features a method for mission planning. The method includes displaying a graphical representation of a geographical area and displaying a graphical representation of one or more regions within the geographical...
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WO/2012/123793 |
The invention relates to an airship (1) comprising a flexible envelope (2) having at least one adjustment region (4) provided with two longitudinal adjustment elements (5, 6) mounted in opposition and mobile in relation to each other bet...
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WO/2012/122532 |
The present invention is directed to methods and compositions for reduction of uric acid levels in subjects, and methods and compositions that are useful for treating, suppressing and/or preventing afflictions related to elevated uric ac...
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WO/2012/121825 |
An aircraft fuselage may include a barrel section (34) having a side region. The fuselage may include a first cutout (52a) and a second cutout (52b) formed in the side region in side-by-side relation to one another. The fuselage may prov...
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WO/2012/119718 |
An aircraft region (1) has an aisle (4) which leads into an aircraft door region (3) and via which passengers can leave the aircraft (2) or enter the aircraft. The aircraft region (1) further has at least one monument (5, 5'), wherein on...
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WO/2012/120227 |
The invention relates to a turbine engine pipe having a longitudinal axis A, which, at the upstream end thereof, includes an outer wall (11) and a core (200), only the upstream portion (210) of which is surrounded by said outer wall (100...
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WO/2012/119588 |
The invention relates to a salvaging and braking device for objects flying freely in space, in particular for capturing satellites and other orbital objects. At least one, preferably a large number of capturing units (2) are arranged on ...
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WO/2012/121322 |
A spar (2), which is an embodiment of this carbon-fiber-reinforced plastic structure, is equipped with both a carbon fiber prepreg (6) and a conduction layer (8) that is provided on the surface (6a) of the carbon fiber prepreg (6) and th...
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WO/2012/120232 |
According to the invention, a link is established between the fixed part (4A) and the removable part (4B) of an enclosure (4) in which the second satellite is previously enclosed, said link being such that said removable part (4B) remain...
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WO/2012/120504 |
An aerial balloon system comprising a payload platform suspended from an inflated balloon by means of a balloon cable, and an anchoring cable attaching the platform to an anchor point beneath it. The balloon cable and anchoring cable are...
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WO/2012/119468 |
A track changing system and method using ultra-high pressure fluid jet power for an aircraft. The track changing system further comprises a combined orifice arranged in a honeycomb geometric shape. The combined orifice is formed by a plu...
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WO/2012/121813 |
An aircraft transparency includes a first ply having a first major surface and a second major surface. A second ply is spaced from the first ply and has a third major surface and a fourth major surface. A polymeric interlayer is located ...
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WO/2012/116739 |
A draining device for draining a fluid from an aircraft engine support strut (3) comprises: a suction arrangement comprising an inlet (13) and extending along a longitudinal main axis (l-l) to form a plenum chamber (12); a drain tube (5)...
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WO/2012/116918 |
The present invention provides a door frame construction (108) in particular for an aircraft or spacecraft, comprising: a former (106); a fibre metal laminate (110) which is connected to the former (106); and an outer skin (102) which is...
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WO/2012/118386 |
An adjustable stairway (10) has a first frame section (11) with fixed steps (15). A second frame section (22) is coupled to the first frame section (11) such that relative movement there between can take place such that the stairway is a...
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WO/2012/118584 |
A blunt impact indicator tape includes a tape strip (2), a plurality of rupture-able fluid microspheres (6a, 6b, 6c) carried by the tape strip and colored indicator fluid (10a, 10b, 10c) in each of the plurality of fluid microspheres.
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WO/2012/117280 |
A control computer for an unmanned vehicle, including: a sensor interface for receiving sensor data from sensors of the vehicle, said sensor data including data values associated with movement of the vehicle; an actuator control interfac...
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WO/2012/117197 |
The invention relates to an aircraft comprising: a sealed volume forming an air cushion above which a cabin is arranged, said sealed volume extending substantially across the entire width of the aircraft and comprising: - at least one in...
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WO/2012/119031 |
A method and apparatus to control movement of a vehicle using a plurality of thrust-producing devices formed in at least one control surface is disclosed. A supply of power to the plurality of thrust-producing devices that are configured...
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WO/2012/116764 |
Method for protecting aircraft occupant comprising the steps of: − providing a user (7) with a breathing mask (4) for aircraft occupant, − providing a respiratory gas (62) including a mixture of breathable gas and dilution gas to the...
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WO/2012/118731 |
Lighter-than-air systems, methods, and kits for obtaining aerial images are described. For example, various methods for determining planned ascent, drift, and/ or descent of a lighter-than-air system are described. In addition, various s...
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WO/2012/117197 |
Aircraft, characterized in that it comprises: ■ a sealed volume forming an air cushion above which a cabin is arranged, said sealed volume extending substantially across the entire width of the aircraft and comprising: - at least one i...
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WO/2012/118516 |
Ceramic matrix composite sandwich structures, gas turbine engine components that comprise such sandwich structures, and methods of producing such sandwich structures. The ceramic matrix composite sandwich structure includes a core having...
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WO/2012/118731 |
Lighter-than-air systems, methods, and kits for obtaining aerial images are described. For example, various methods for determining planned ascent, drift, and/ or descent of a lighter-than-air system are described. In addition, various s...
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WO/2012/118516 |
Ceramic matrix composite sandwich structures, gas turbine engine components that comprise such sandwich structures, and methods of producing such sandwich structures. The ceramic matrix composite sandwich structure includes a core having...
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WO/2012/117200 |
The present invention relates to a method for producing a metal component such as a metal turbomachine blade reinforcement, comprising, in succession: a step of producing a three-dimensional metal structure (310) consisting of an insert ...
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WO/2012/117009 |
A method of operating actuators simultaneously for moving at least two aircraft movable aerodynamic surfaces, the method comprising the steps of: • controlling the actuators to move the aerodynamic surfaces towards a predetermined posi...
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WO/2012/117209 |
A fibrous structure (100) for reinforcing a component made of composite material is obtained by the multi-layer weaving of a plurality of layers of warp threads (101) and a plurality of layers of weft threads (102). The fibrous structure...
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WO/2012/117202 |
The present invention relates to a method for producing a metal component such as a metal turbomachine blade reinforcement, comprising, in succession, a step of producing a plurality of three-dimensional metal structures (350) by securin...
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WO/2012/117628 |
Provided is a machine tool, which is capable of highly accurately performing machining with respect to a bent surface of a subject to be machined. The machine tool fixes work (W), which has an upper flat surface (Wa) and a lower bent sur...
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WO/2012/117201 |
The present invention relates to a method for producing a metal component (30) such as a metal turbomachine blade reinforcement, comprising, in succession, a step (230) of positioning a plurality of metal clips (301') in a forming tool (...
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WO/2012/119044 |
A replaceable thrust generating structure for an air vehicle, which includes one or more mounts, which are attachable to the air vehicle, and a thrust generating structure attached to each of the one or more mounts, and wherein the thrus...
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WO/2012/113287 |
Disclosed is a reciprocal flapping wing fluid energy transformation device, which comprises frameworks (1), wing racks (2) and a wing rack linkage device (3), wherein the wing racks (2) are assembled to the frameworks (1), on each of the...
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WO/2012/113158 |
A helicopter includes a fuselage (1) and propellers (3). The propellers (3) are provided under the fuselage (1). The helicopter solves the problem of prior art that the low carrier capacity is caused by the low lifting capacity and impro...
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WO/2012/115633 |
An external airbag for an aircraft includes an inflatable bladder having a top portion and a bottom portion, the top portion being generally adjacent to an exterior of the aircraft. A widthwise panel divides the inflatable bladder into a...
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WO/2012/113521 |
A waste water system for a commercial aircraft, with a waste water line (13) and a valve (5) arranged in the waste water line (13), wherein the grey water, upon drainage, after flowing through the valve (5), is either forwarded for outpu...
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WO/2012/113499 |
The invention relates to a modular on-board galley, in particular an aircraft galley (11), and to a method for assembling a galley of this kind which comprises, as areas of use, a main element and at least one add-on element divided into...
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WO/2012/113742 |
The present invention provides a method for producing a connector (100), in particular for repair, in particular in the field of aviation and aerospace, comprising the steps of: providing a base layer (102); attaching a first layer (200)...
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WO/2012/113576 |
The invention relates to an ultra-lightweight airplane (100) for transporting loads, comprising a hull (110), at least three individually controllable rotors (130), and at least one first airfoil (120a) arranged on the hull. Axes of the ...
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WO/2012/114047 |
The invention relates to an aircraft with reduced environmental impact including two turboprop engines (10) mounted on the back of the aircraft at the rear thereof, and one acoustic masking device per turboprop engine. The acoustic maski...
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WO/2012/114022 |
The invention relates to an aircraft including at least one wall (66) defining a first area (I) of the aircraft that is thermally insulated from the outside of the aircraft, and a second area (E) of the aircraft that is not thermally ins...
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WO/2012/113038 |
The present invention provides an aircraft buoyancy system (14) for providing positive buoyancy to an aircraft (15) to keep it afloat at the surface of a body of water (16) after crashing, ditching or landing into a body of water (16). T...
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WO/2012/116366 |
An opto-mechanical deployable telescope includes a hub, at least one deployable multiple petal primary mirror mounted to the hub, a deployment assembly, and a deployment engine assembly. The deployment assembly is operable to move the at...
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WO/2012/112939 |
Multi-wing hovering and gliding flapping Micro Air Vehicles ("MAV") are disclosed. The MAV can have independent wing control to provide enhance energy efficiency and high maneuverability. Power to each wing can be controlled separately b...
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WO/2012/110221 |
The invention relates to a table device of a vehicle seat, in particular an aircraft passenger seat (12; 30), which has at least one storage surface (16) and a mounting unit (20), which is provided to guide the at least one storage surfa...
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