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WO/2011/089180 |
The invention relates to a flexible oxygen supply system that can be easily adaptable to different seating layouts and significantly improved with respect to opportunities for testing and maintenance. An oxygen module according to the in...
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WO/2011/089413 |
An aircraft wing cover (10) comprising an integrally stiffened sandwich panel including first and second skins (11, 12) sandwiching a core layer (13), wherein at least one of the skins has a plurality of spanwise extending integral regio...
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WO/2011/089580 |
A seating arrangement comprising at least three or more seats arranged in a row and adjacent each other in a side by side relationship to present two outer ends of said row, said seating arrangement further including a deployable side su...
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WO/2011/089566 |
A class divider in an aircraft between a first seating arrangement that comprises of seats of a first kind and a second seating arrangement that comprises of seats of a second kind. The divider comprises a primary partition wall member t...
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WO/2011/089558 |
A tray table arrangement for use by a passenger sitting in an aircraft seat, the tray table arrangement supported by a support structure to allow it to be presented for use by the passenger, and comprising a bi-fold table comprising at l...
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WO/2011/089463 |
A breathing assembly (1) for aircraft comprising: - a breathing mask (2) to be connected to a source of breathing gas, - a stowage box (10) forming a receptacle for receiving the breathing mask (2) in a stowage position, and - a valve as...
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WO/2011/089426 |
A landing gear (70) for an aircraft, the landing gear including an axle (14) pivotally connected to a bogie beam (12) and a locking device (11c), the locking device being arranged to couple the axle to the bogie beam, the locking device ...
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WO/2011/089277 |
The invention relates to a blade with a variable profile and shape, having a section (11) made of a flexible material, the inside of which has two parallel recesses (13) that run the entire length of the blade (1) and contain rods (2), 5...
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WO/2011/088991 |
The invention relates to an aircraft landing gear of the deformable-parallelogram type that comprises: a leg comprising a casing (1) having a lower end on which a rocker arm (3) carrying at least one wheel is hinged, a shock absorber bei...
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WO/2011/089580 |
A seating arrangement comprising at least three or more seats arranged in a row and adjacent each other in a side by side relationship to present two outer ends of said row, said seating arrangement further including a deployable side su...
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WO/2011/089458 |
General purpose airplane with a swept back wing provided with a sharp leading edge as to cause flow separation and stall of the wing in cases where the limits of the regular flight envelope are exceeded in terms of angle of attack, and a...
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WO/2011/089016 |
The invention relates to a self-sufficient monument in an aircraft pressure cabin which is supplied with required operating resources in a decentralized manner such that said resources are entrained in operating resource stores in the mo...
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WO/2011/089180 |
The invention relates to a flexible oxygen supply system that can be easily adaptable to different seating layouts and significantly improved with respect to opportunities for testing and maintenance. An oxygen module according to the in...
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WO/2011/089196 |
The invention relates to a device and method for regulating the humidity in a fuel cell that detect a step response of the output voltage of a fuel cell when the supply to electric consumers is interrupted, determine parameters of the dy...
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WO/2011/089567 |
A stowage system enabling selective positioning of a display rack that holds or can hold util ity items between an elevated stowed position and a lowered display position on a guide rail in a linear sliding manner wherein in the elevated...
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WO/2011/089481 |
The proposed method can be used in any sector of industry for the three-dimensional controlled movement of technical means in spaces above ground, in the air, underwater and in near-Earth space as well as in other centrally symmetric gra...
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WO/2011/088999 |
The invention relates to a seat device, in particular an air passenger seat, comprising a seat structure (28) which can be fastened to a floor (10), a seat shell (18) which comprises a front seat section (20) and a rear seat section (22)...
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WO/2011/088534 |
The present invention provides a seat with a reduced thickness for passenger transport vehicles, comprising in at least part of the user contact zones, deformable materials with a reduced thickness and able to return to their original sh...
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WO/2011/087375 |
This invention relates to arresting beds for decelerating vehicles, especially passenger air-crafts unable to stop on available run-way wherein the system comprises a vehicle arresting area (A) comprising a bed filled with foamed glass a...
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WO/2011/086221 |
Support pylon (19) for aircraft engines joined to a section of the fuselage (17) that has a curved closed cross-section including a skin (31) and a plurality of frames (33); its structural configuration comprising a central box (41) insi...
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WO/2011/086160 |
The invention relates to a device (1) for providing radio frequency signal connections for users on an airplane, wherein the device (1) comprises a plurality of WLAN access points (9 - i), which transmit or receive radio frequency signal...
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WO/2011/087389 |
The invention relates to a device for modifying a counter-acting force and provided in an area of force transfer from one object to another, e.g. on a load-lifting cable or on a thrust transmission line from a thruster to a body, such as...
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WO/2011/086258 |
The invention relates to the mutualization of the electrical converter for starting an aircraft and moving the latter on the ground. According to the invention, a single electrical converter (14) is capable of being coupled to the electr...
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WO/2011/087475 |
A method of providing an aircraft having a fuselage and a wing configured for extensive laminar flow at design cruise conditions, the method characterized by a) providing wing biconvex-type airfoils having values of thickness, chord and ...
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WO/2011/086502 |
A commercial passenger aircraft with a lavatory that includes an interior surface to which an image is applied visible to a lavatory occupier, the image being incongruous with an occupier's usual expectations.
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WO/2011/087479 |
A fluid turbine comprising a rotor, having an axis of rotation, comprising at least two rotor blades disposed at a radius from the axis of rotation, each rotor blade having a pitch axis and a variable pitch angle. The fluid turbine compr...
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WO/2011/087413 |
The present invention regards a structural article comprising an outer surface (5), which serves as an aerodynamic surface when the structural article (1) is subjected for an air stream, the structural article (1 ) comprises a resin matr...
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WO/2011/087412 |
The invention regards a de-icing/anti-icing system comprising at least two conductive structures (3', 3") embedded in an article (2), which includes an outer surface (5) being designed as an aerodynamic surface, at least one of the condu...
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WO/2011/087475 |
A method of providing an aircraft having a fuselage and a wing configured for extensive laminar flow at design cruise conditions, the method characterized by a) providing wing biconvex-type airfoils having values of thickness, chord and ...
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WO/2011/087541 |
A power generation apparatus and method comprises at least one gyroglider rotary wing flying at an altitude above the nap of the earth. A strong and flexible tether, connected to the gyroglider frame is pulled with a force generated by t...
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WO/2011/086273 |
The invention relates to an aircraft nacelle comprising an air inlet (110) with a lip (114) extended to the back by a passage (116) that makes it possible to channel an air flow to a drive (112), said passage (116) comprising at least on...
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WO/2011/087189 |
Disclosed are a door control device for a flight vehicle and a flight vehicle having the same, the door control device including, an opening formed at a main body of the flight vehicle and allowing a corresponding wing to be deployed fro...
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WO/2011/087785 |
A system i s provided for the force decay triggered release of a device, the system compris ing: a base; a plural ity of retention rods extend ing from the base; a rotationa l ly movabl e actuator, to wh ich a l i n ear force is confi gu...
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WO/2011/087475 |
A method of providing an aircraft having a fuselage and a wing configured for extensive laminar flow at design cruise conditions, the method characterized by a) providing wing biconvex-type airfoils having values of thickness, chord and ...
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WO/2011/086222 |
Aircraft component with panels (11) stiffened with stringers (15) configured with a web (17) and several feet (19) in which there are zones of potential intersection or interference of said stringers (15) with spars (25) and ribs (27), i...
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WO/2011/088426 |
A cooling system for a wind tunnel (100) is disclosed. The heat exchanger (200) of the present disclosure is formed as a turning vane assembly in an airflow duct of a re- circulating wind tunnels. The individual vanes (201) are formed fr...
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WO/2011/087541 |
A power generation apparatus and method comprises at least one gyroglider rotary wing flying at an altitude above the nap of the earth. A strong and flexible tether, connected to the gyroglider frame is pulled with a force generated by t...
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WO/2011/087724 |
The present invention provides novel inflatable and rigidizable support elements, and methods of manufacture and use thereof. In particular, the present invention provides inflatable and rigidizable support elements which find use in rap...
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WO/2011/086281 |
The invention relates to an aircraft nacelle including a first subassembly consisting of a pipe (112) channeling an airflow in the direction of an engine having a covering or panel (118) for acoustic treatment, including, from the inside...
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WO/2011/086304 |
The invention relates to an aircraft comprising at least one net for reducing aerodynamic noise from a structural element of said aircraft. According to the invention, the flexible net (5A) associated with the structural element (2) is r...
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WO/2011/087411 |
The invention regards an article comprising an outer surface (11), which serves as an aerodynamic surface when the article (3, 3', 16, 27, 53) is subjected for an air stream (a), the article (3, 3', 16, 27, 53) comprises a resin matrix m...
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WO/2011/084358 |
A piezoresistive sensor assembly is provided that has a flex circuit having at least one air flow aperture formed therein. A sensor die is coupled to an absolute support and the flex circuit. The sensor die has a diaphragm that deflects ...
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WO/2011/082775 |
The invention relates to a parachute composed of a plurality of individual textile strips (11) separated from one another, at least two groups of individual strips in each case comprising a plurality of individual strips running parallel...
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WO/2011/084358 |
A piezoresistive sensor assembly is provided that has a flex circuit having at least one air flow aperture formed therein. A sensor die is coupled to an absolute support and the flex circuit. The sensor die has a diaphragm that deflects ...
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WO/2011/084114 |
The invention is the vertical wind tunnel comprising air flow channels (10) having rectangular shaped structure, high power fan mechanisms for providing air flow inside the said air channels (10), flying field (12) having the capacity to...
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WO/2011/082983 |
The present invention relates to sound damping of air conditioning systems in an aircraft. The invention in particular relates to an air conditioning air duct for an aircraft, and to an aircraft having air conditioning air ducts. In orde...
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WO/2011/082983 |
The present invention relates to sound damping of air conditioning systems in an aircraft. The invention in particular relates to an air conditioning air duct for an aircraft, and to an aircraft having air conditioning air ducts. In orde...
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WO/2011/084081 |
The invention relates to aircraft on an air cushion. The aircraft comprises a disc-like body with a central tunnel, within which a streamlined body is mounted with a lifting propeller on the upper part thereof, said streamlined body bein...
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WO/2011/083250 |
The invention relates to an aircraft propeller blade (10) which includes a structure having an aerodynamic profile (20), characterised in that the structure having an aerodynamic profile includes at least one fibrous reinforcement obtain...
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WO/2011/082998 |
The invention relates to a supply module for a passenger transport vehicle, comprising a first supply unit for supplying passengers with a first supply medium in a first supply area, and a second supply unit for supplying a second supply...
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