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WO/2010/078295 |
A parachute seat includes a saddle formed by an ergonomically shaped saddle base member with a cushioning layer thereon that covers and conforms with the shape of the upper surface of the saddle base member. The saddle is preferably rece...
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WO/2010/074595 |
The invention relates to aviation. The aircraft comprises a fuselage, horizontal front and tail empennages and take-off and landing wings, which wings are jointed to the fuselage by means of attachment joints, the axes of which are situa...
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WO/2010/074653 |
A landing pad with an inbuilt fire suppressor that includes at least one first interlocking unit. The interlocking unit includes a landing surface, wherein the landing surface includes openings distributed thereon; and at least one inter...
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WO/2010/072996 |
A system for monitoring the path of an aircraft approaching to land on an aircraft carrier (1) or similar moving platform, particularly in the case of failure or non-availability of other landing aids, utilises a camera (3) which is stab...
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WO/2010/075034 |
The present invention relates to articles and methods for producing non-latex balloons with low surface electrical conductivities and an extended product life. In a preferred embodiment, a multilayer composite film (1) having an exposed ...
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WO/2010/072911 |
The invention relates to propulsion equipment for an aircraft, including a first rotary body (6) referred to as a driving body, a second rotary body (1) referred to as a driven body, and a reduction gear transmission device (19) disposed...
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WO/2010/072916 |
The invention relates to a method for making a structural part comprising a tubular portion (30) from which a structural member made of a composite material protrudes, said method comprising the steps of: shaping a planar preform (59) in...
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WO/2010/074942 |
An anti-icing system (200) includes a component surface (202) having a composite structure including a composite layer (214), aid at least one heating element (220) formed within the composite layer (214), wherein the heating element (22...
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WO/2010/073396 |
An operation control device (300) includes: a database (331) which holds a heat release value condition of an artificial satellite and a temperature environment condition based on an orbit position and a posture of the artificial satelli...
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WO/2010/072952 |
The invention relates to an L-shaped fitting obtained after moulding a composite material, including two portions (20, 21) defining an angle therebetween and having holes (22, 23) formed therein for connecting the two portions using an a...
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WO/2010/072681 |
The invention relates to a propulsion module for launching a vehicle into space comprising a reusable module (14), as well as an expendable portion (16) rigidly connected to the reusable module (16) during the launch, said reusable modul...
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WO/2010/070173 |
A lifting or stabilising component (11) for an aircraft comprising in the area of its trailing edge a rotary control element (13) rotating around an axis (61) with at least one slot (21) between the tip (15) of the component (11) and the...
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WO/2010/069944 |
The invention relates to a part (1) comprising a structural portion made of an electrically insulating or low-conductive composite material (2), such that a piece containing glass fibres or carbon fibres is protected against the accumula...
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WO/2010/070185 |
The invention relates to the trailing edge (3) of an aircraft stabiliser (1) which is made from a composite material and includes an outer skin (40) and an inner skin (41) which are joined to the trailing edge (3) by means of clip-type c...
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WO/2010/069506 |
The invention relates to a door mechanism (10), particularly suitable for use in an aircraft galley, comprising a joint mechanism (18) pivotally connected about a first pivot point (20a, 22a) to a housing (16), and pivotally connected ab...
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WO/2010/070631 |
The present invention relates to an unmanned air vehicle (105), comprising a body having front (121) and rear (122) sections with at least one pair of end plates (110) connected to said body, wherein one end plate within said at least on...
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WO/2010/070184 |
The invention relates to the structure of the load-introduction area in the fuselage rear section of an aircraft, including elements (3, 4) for receiving loads from the horizontal and vertical tailplanes connected to structural elements ...
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WO/2010/069032 |
A foldable ramp for evacuation of a vehicle, the ramp including hingedly connected primary and secondary side members, a primary fixed panel fixedly attached the primary side members, a primary flipping panel extending between the primar...
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WO/2010/069831 |
The present invention relates to a multilayer board for sound insulation and to a method for the production thereof. In order to reduce the sound emission and at the same time to improve the stability, a multilayer board (40) for sound i...
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WO/2010/071782 |
A data monitoring and analysis system suitable for performing real-time monitoring of vehicle information systems installed aboard a passenger vehicle fleet and methods for manufacturing and using same. The data monitoring and analysis s...
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WO/2010/071734 |
A transparent polycrystalline ceramic having scattering and absorption loss less than 0 2 /cm over a region compπsing more than 95% of the originally densified shape and a process for fabrication by hot pressing The ceramic can be any s...
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WO/2010/070071 |
An aircraft cabin panel (40) is provided for sound reduction in an interior space, which has in at least one region a sandwich construction comprising a core layer (50), a first outer layer (52) and a second outer layer (54). The core la...
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WO/2010/071643 |
A method and apparatus are present for managing forces on a refueling boom (500). Force information is received from a force sensor (326) associated with the refueling boom (500). Forces on the refueling boom without a number of air load...
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WO/2010/070273 |
In a first aspect the invention relates to a sensor system (10) for determining a proximity to icing conditions of an environment. The system includes a sensor having a sensor surface (12) for exposure to the environment, an electrically...
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WO/2010/070181 |
The invention relates to a rib fitting forming a component (9) of a torsion box (1, 3) of an aircraft airfoil, said component being made from a composite material in the form of a single piece and having a configuration comprising: a sub...
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WO/2010/069921 |
The invention relates to a part (11) made of a composite formed from a thermosetting resin, which includes lightning protection means comprising, on an upper surface (12) of the part (11) liable to be exposed to lightning strikes, a cont...
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WO/2010/069922 |
The invention relates to a part for an aircraft structure consisting of a structural portion made of a carbon fibre composite, said part comprising, on a surface of said structural portion, at least on a side of the part likely to be sub...
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WO/2010/070070 |
A maintenance system for generating maintenance instructions for at least one system comprising a plurality of system components is set up to receive operating data for a system from a central control unit (12) of the system (2, 24), to ...
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WO/2010/069923 |
The invention relates to a central pedestal for a flight deck of an aircraft, to which to attach aircraft instrumentation and control members, which comprises a three-dimensional shell (8) made of composite material containing inorganic ...
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WO/2010/070182 |
The invention relates to a horizontal stabilising surface (8) of an aircraft, in which the sweep angle (40) of said surface (8) is less than 90 degrees, whereby said angle (40) is that formed by the projection of the point reference line...
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WO/2010/067001 |
The floor section for a vehicle cabin consists of a juxtaposition of profiled elements (9) all of identical cross section and each comprising: a chiefly planar elongate cross member (10), positioned in a transverse vertical plane, said c...
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WO/2010/068942 |
A rotary blade rotating hub mounted rotating assembly vibration control system (20) including a first imbalance mass concentration rotor (28), a second imbalance mass concentration rotor (44), a third imbalance mass concentration rotor (...
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WO/2010/068426 |
An apparatus for use with a flight control actuator and method for assembling the same is provided. The apparatus includes a motor drive system (100) and a control unit. The motor drive system (100) includes a capacitor-based energy stor...
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WO/2010/067325 |
A ducted fan for a VTOL vehicle includes a substantially cylindrical duct having an inlet at an upper end and an outlet at a lower end, a propulsion unit inside the duct, between the inlet and the outlet, and at least one group of contro...
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WO/2010/066985 |
The invention relates to a system for attaching two components together, such as an aircraft engine and the mounting pylon thereof. According to the invention, at least two of the front (10) or rear (11) trunnions of the attaching system...
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WO/2010/066958 |
The invention relates to an overpressure hatch (21) intended to be mounted on a wall (23) of a nacelle (1) for a turbojet engine (5), the overpressure hatch (21) comprising a support (22) intended to be fixed to the wall (23), and at lea...
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WO/2010/068174 |
A microsatellite comprising a propulsion module for moving and/or pointing said microsatellite and an imaging device (100) mounted to said propulsion module. Furthermore there is a fuel supply (210) located within said imaging device (100).
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WO/2010/067096 |
The invention relates to an aircraft transparency protector (10). The protector (10) comprises a lobed blank cut from a sheet of resilient material, which is bendable, such that adjacent lobes abut, thereby to conform to the shape of the...
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WO/2010/068194 |
A rotor system includes a lead stop mounted to a spindle and a lead stop plate mounted to a rotor hub arm, the lead stop operable to contact the lead stop plate over a lead angle range.
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WO/2010/067132 |
A baggage tracking system (200) uses an array of cameras (212) to image a bag tag (128) and thereby route a bag (132) with a sort allocation computer (114) in the event that a barcode on the tag (128) is unreadable. The system can also i...
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WO/2010/068225 |
An electric linear actuator is disposed to pitch a blade of a hingeless, swashplateless rotor in rotary motion. This actuator can be equipped with an electric motor advantageously made fault tolerant by winding the motor for at least 4, ...
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WO/2010/066791 |
The invention relates to a fan (1) for an aircraft turbine engine, including an inlet cone provided with a balancing system having a plurality of holes for housing bodies (42), and also including at least one balancing body (44) mounted ...
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WO/2010/065999 |
The present system provides a buoyancy system for moving an object (401) in a body of water. The system comprises at least one inflatable body (17) which, when inflated, increases the buoyancy of the object (401), and an inflation appara...
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WO/2010/067051 |
Apparatus for use in delivering goods comprises a protective housing (1) for containing the goods, a transportation base (5) serving to facilitate delivery of the housing (1) and the goods therein, a releasable strap connection (6) betwe...
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WO/2010/066440 |
The invention relates to an emergency power system for an aircraft, comprising at least one fuel cell unit for generating electricity. Said fuel cell unit is cooled using at least one cooling cycle encompassing at least one heat exchange...
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WO/2010/067858 |
A desired search range is efficiently monitored. Provided is a monitoring device which is mounted in the body of an airplane flying in the sky and monitors the state of the sea from the sky, the monitoring device being provided with a ...
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WO/2010/068209 |
The invention relates to a backing plate used for an elastomeric bearing system, the backing plate comprising a plate which defines an at least partial annulus about an axis, a motion limiter and a redundant pivot which extend from the p...
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WO/2010/063927 |
The invention relates to an aircraft engine assembly (1) including: a mounting pylon that comprises a rigid structure (16) provided with a central box-type structure (24), as well as a front extension (26) and a rear extension (28), ea...
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WO/2010/064886 |
The present invention relates to an improved encased square aerodynamic wing, the structure of which incorporates the vertical stabilizers and aerodynamic brake, offering the special feature of reducing wing resistance and providing bett...
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WO/2010/064548 |
The unmanned aircraft is equipped with a camera, a laser ranging system, and a drive unit. The laser ranging system measures the distance to an object in the camera field of view. The drive unit rotates the field of view. Information on ...
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