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WO/2011/135605 |
A reduced dimensions platform (1) for the landing of an aircraft on an access facility (B) comprising a support base (2), suitable to be fixed on a reference surface (P) belonging to said access facility (B), and a landing footboard (3),...
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WO/2011/135230 |
The invention relates to a satellite having a structure that includes a circular launching interface ring (1) and at least two main planar apparatus-holding walls (5) that are substantially parallel to the axis (A) of the ring (1) and ri...
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WO/2011/134503 |
A drive unit (16) for an aircraft running gear (2) having at least a first wheel (4) and a second wheel (6) on a common wheel axis (A) is characterized in that the drive unit (16) is drivingly coupleable to the first and second wheels (4...
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WO/2011/134640 |
The invention relates to a rail system (10) which can be used for mounting a component in an aircraft. Said rail system comprises a first rail element (12) provided with a securing device (22) in order to detachably secure the first rail...
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WO/2011/135213 |
The present invention relates to a support half structure for a nacelle of an aircraft engine, which half structure includes at least one longitudinal beam (1 b) and a front half frame (3b). Said half structure is characterized in that s...
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WO/2011/137417 |
A rotary wing aircraft vehicle vibration control system includes a hub mounted vibration control system mounted to the rotary wing hub with the hub mounted vibration control system rotating with the rotary wing hub driven to rotate about...
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WO/2011/135217 |
This nacelle for an aircraft engine comprises: a fixed front frame (19), a thrust reverser cowling (11) mounted to slide with respect to said front frame (19) between a direct-jet position and reverse-jet position, a variable-geometry no...
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WO/2011/135245 |
The aim of the invention is to reduce the multiple costs of manufacture, assembly, use, and upkeep connected with the assembly of window coaming on aircraft fuselages. To this end, the invention provides a particular shape for the coamin...
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WO/2011/137417 |
A rotary wing aircraft vehicle vibration control system includes a hub mounted vibration control system. The system includes a sensor for outputting data correlating to relative rotation of the hub rotating about the Z axis relative to t...
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WO/2011/134799 |
A device (13) for detecting the breakage of a primary path in a flight control actuator, said actuator having a primary path (1) comprising a rotary hollow screw (2), a secondary path (10) comprising a safety rod (3) that reacts the load...
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WO/2011/135363 |
A vacuum anchor for securing a fall protection system to a surface has a gas inlet to receive pressurised gas from a gas container and generates a vacuum to secure the anchor to a surface. An attachment enables a fall protection system t...
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WO/2011/134945 |
A water system (2) for a vehicle has at least one water supply source (4, 32), at least one water-conducting device, at least one shut-off valve (36, 38) and at least one germ reduction connection (34), wherein the germ reduction connect...
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WO/2011/134615 |
The invention relates to a support structure (10) for use in an air supply arrangement for air conditioning passenger compartments in aircraft. Said air supply arrangement comprises at least one centrally controlled cabin ventilator and ...
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WO/2011/135236 |
The invention relates to an actuation device (1) of an adjustable member supported by a rotor of a propulsion engine, said actuation device including: at least one electrical source (2, 2'); an electric actuator (3) for adjusting said ad...
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WO/2011/135134 |
Internal structure for aircraft, comprising a skin (1) of composite material, stringers (2) of composite material integrated into the interior of the aforementioned skin (1), and frames (3) of composite material, the skin (1) comprising ...
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WO/2011/133273 |
The different advantageous embodiments provide a system and method for transmitting messages. In one advantageous embodiment, a system comprising a number of transceiver units, a first computer system, and a second computer system is pro...
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WO/2011/133598 |
An aircraft ceiling module includes a ceiling panel (12) with integrated lighting, valences (16) and wiring. LED lighting units (14) are mounted directly to the ceiling panel, and one or more valence panels (16) are connected to the ceil...
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WO/2011/132291 |
A prediction means predicts the risk of collision of a flying object using at least the altitude, body speed, and body position as parameters. In cases in which the prediction means has determined the risk of collision as being high, a f...
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WO/2011/131873 |
This nacelle for an aircraft engine comprises a thrust reverser cowling (11) slidably mounted between a direct-jet position and reverse-jet position, an outlet jet pipe nozzle (13) of variable cross section positioned in the downstream c...
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WO/2011/133598 |
An aircraft ceiling module includes a ceiling panel with integrated lighting, valences and wiring. LED lighting units are mounted directly to the ceiling panel, and one or more valence panels are connected to the ceiling panel to shield ...
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WO/2011/133702 |
A bin assembly that includes a bin housing and a bin that is pivotal between an open and a closed position within the bin housing. The bin housing includes a forward bulkhead panel, aft bulkhead panel and an aft housing panel that includ...
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WO/2011/133969 |
Described are tray table stop assemblies comprising a housing comprising at least one deployment track, a force-receiving mechanism comprising at least one protuberance, wherein the at least one protuberance is slidingly coupled to the a...
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WO/2011/131599 |
The invention relates to an illuminating device for an airport runway, comprising a base support (1, 21) on which at least one lighting unit is fixed. The lighting unit comprises a light source (5), a reflector (6), and a covering lens (...
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WO/2011/133601 |
A lift assist mechanism is provided for assisting lifting of a movable component that can move between lowered and raised positions relative to a fixed structure. The lift assist mechanism includes a lift assist spring connected to a spr...
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WO/2011/133944 |
Unmanned Aerial Vehicle and Method of Operation A method of unmanned aerial vehicle (UAV) flight includes providing horizontal thrust in-line with the direction of forward flight of the UAV (110) using at least one electric motor (120), ...
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WO/2011/131651 |
The invention relates to an exhaust gas diffuser 10 for a gas turbine, comprising a flow duct 22 which expands toward the diffuser outlet 20 and at the center of which an axially extending conducting body 14 is provided. In order to prov...
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WO/2011/133603 |
An interior ceiling panel system (10) includes a ceiling panel (38) mounted in a ceiling area (14), a first airflow directing panel (44) in a first side of the ceiling area defining an airflow passage, and a second airflow directing pane...
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WO/2011/131382 |
A single wing for an unmanned aircraft (400) adapted for image acquisition, surveillance or other applications consists of a ribbed frame (100) and a foam (200) wherein the ribbed frame (100) is integrated during molding for stiffness an...
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WO/2011/133591 |
An electrically activated latch for aircraft stowage bins includes an overhead stowage bin module having a stationary support structure and a movable stowage bin portion. An electrically operated stowage bin latch mechanism latches the m...
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WO/2011/133601 |
A lift assist mechanism is provided for assisting lifting of a movable component that can move between lowered and raised positions relative to a fixed structure. The lift assist mechanism includes a lift assist spring connected to a spr...
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WO/2011/132202 |
The present invention discloses a tray cart for serving refreshments in an airplane. The tray cart having: a load bearing railing coupled with a fuselage portion of the airplane, the railing stretching from a first end of the airplane to...
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WO/2011/133260 |
A method and apparatus comprise a first number of layers of a flexible material (803, 804), a second number of layers of a dielectric material (805, 806), a first electrode (808) attached to a surface layer in the first number of layers ...
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WO/2011/131733 |
The invention relates to a vertical take-off and landing gyropendular craft or drone device (FIG. 18) able to move around in the following different physical environments: in the air, on land, at sea, underwater or in space, comprising u...
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WO/2011/131874 |
In this arrangement of at least one thrust reverser flap (13) link rod (15) on the internal fixed structure of a turbo jet engine nacelle, said link rod (15) is connected to the internal fixed structure by elastic means (17).
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WO/2011/133586 |
An aircraft overhead luggage bin module includes a stowage bin assembly, an integral light assembly providing structural stiffness to an upper portion of the stowage bin assembly. The stowage bin assembly includes an air distribution ple...
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WO/2011/131733 |
The invention relates to a vertical take-off and landing gyropendular craft or drone device able to move around in the following different physical environments: in the air, on land, at sea, underwater or in space, comprising upper and l...
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WO/2011/131492 |
The invention relates to sound absorption in cabins of aircraft. The invention relates in particular to an aircraft cabin panel absorber for sound absorption, to a device for sound absorption in an aircraft cabin, and to an aircraft comp...
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WO/2011/131570 |
A support apparatus for the positioning of objects (12, 14) which can be moved on one axis, has a distance sensor (40, 52), an activatable position mark (36, 38) for fitting to the object (12, 14) the distance of which from the distance ...
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WO/2011/131691 |
The subject of the invention is a thermal protection material for a surface, which material is made from a mixture comprising a resin, granules of cork and refractory fibres, characterized in that the proportion of granules of cork in th...
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WO/2011/131694 |
The subject of the invention is a thermal protection material for a surface, which material is made from a mixture comprising a resin, granules of cork and refractory fibres, the proportion of granules of cork in the mixture correspondin...
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WO/2011/133576 |
A lavatory for an aircraft cabin includes a wall having a forward wall portion disposed immediately aft of and substantially conforming to an exterior aft surface of an aircraft cabin structure, such as a passenger seat, that is substant...
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WO/2011/132349 |
Disclosed are an aircraft, and an aircraft cockpit window onto which an electromagnetic shield film for preventing electromagnetic noise can be installed reliably, easily, and at a low cost. An electromagnetic shield film (27) is install...
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WO/2011/131692 |
The subject of the invention is a thermal protection material for a surface, which material is made from a mixture comprising granules of cork and a resin forming a binder which furthermore comprises short fibres of a heat resistant mate...
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WO/2011/133603 |
An interior ceiling panel system includes a ceiling panel mounted in a ceiling area, a first airflow directing panel in a first side of the ceiling area defining an airflow passage, and a second airflow directing panel in a second side o...
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WO/2011/127899 |
An aircraft fuselage with an integrated energy-absorbing deformation structure, wherein the fuselage (1) has annular frames (10; 110; 210) and the frames (10; 110; 210) have interconnecting longitudinal fuselage beams (12) and a casing (...
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WO/2011/128667 |
A structure comprising a plurality of plies of fibre-reinforced composite material, each ply having a ply orientation defined by a principal stiffness direction of the ply. The structure has a first region and a second region, each regio...
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WO/2011/128441 |
The present invention relates to an electromagnetic actuator comprising an electric motor (11) to rotate an output shaft (4) via a reduction gear (20) and passive regulation means (30) for controlling the rotation speed of the output sha...
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WO/2011/128211 |
The invention relates to a high-lift system for an aircraft, having at least one lift flap (34), which lies on an airfoil, for forming a gap between a front edge of the airfoil (2) and a rear edge (40) of the lift flap (34) in an extende...
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WO/2011/127996 |
The present invention describes a blade (100) for a wind turbine. The blade (100) comprises a heating mat (101) for generating heat by resistive heating, wherein the heating mat (101) is mounted to the blade (100). The heating mat (101) ...
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WO/2011/130352 |
A method and apparatus for a transmission system selectively positioning sets of planet gear support bearings (50, 55, 80, 90) to achieve an optimized load distribution among a set of drive planet pinions (22) and a set of idler planet p...
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