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WO/2011/083137 |
The invention relates to a contra-rotating propeller system for an aircraft turbine engine, including a free power turbine including a first rotor and a second rotor contra-rotating relative to said first rotor, a first contra-rotating p...
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WO/2011/084246 |
A method and apparatus for controlling a propeller of a contra-rotation open fan (CROF) engine of an aircraft. A diameter of the propeller is set to be at a first diameter during at least a portion of a first flight condition of the airc...
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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/2011/080320 |
The invention relates to an aircraft or spacecraft casing, comprising a composite shell (1) made of first rod elements (111, 112) or sandwich core elements and first skin elements (12), which are connected to the first rod elements or sa...
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WO/2011/081695 |
A torque production vehicle includes a plenum body having a wall with a central port and a radial port formed within the wall, an impeller disposed within the plenum body to move air through the central port, an engine coupled to the imp...
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WO/2011/079924 |
The invention relates to a device (10) for stabilizing the guidance of a vehicle (1), wherein the vehicle (1) has at least one or two wheels, which are rotatably arranged relative to the longitudinal axis of the vehicle (1), and steering...
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WO/2011/081695 |
A torque production vehicle (100) includes a plenum body (110) having a wall (112) with a central port (120) and a radial port (130) formed within the wall, an impeller (140) disposed within the plenum body to move air through the centra...
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WO/2011/082239 |
One embodiment of the present invention is a unique composite gas turbine engine component. In one form, the composite component is an airfoil. Another embodiment is a unique method for manufacturing a composite gas turbine engine compon...
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WO/2011/082299 |
A fan containment system for a gas turbine engine, and a method of making the same, is disclosed that in one embodiment includes casing that surrounds at least a portion of a plurality of fan blades. In one form, a pair of standoff rings...
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WO/2011/081579 |
The invention relates to a weapons bay in an aircraft (4), comprising an aperture (6) in an aircraft fuselage (8); a platform (2) movable between a first position in which the platform (2) is retracted from the aperture (6) and a second ...
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WO/2011/080414 |
The device according to the invention comprises: a first compartment (22) suitable for receiving carts (10) lined up side by side, a second compartment (24) suitable for receiving carts (10) lined up side by side, having an aperture allo...
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WO/2011/080286 |
The invention relates to a fuselage (2) for an aircraft, which fuselage is produced of a fiber-reinforced composite material and comprises a skin (4) and a plurality of peripheral reinforcements (12) and only a small number of longitudin...
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WO/2011/079906 |
A system component module (100) to be mounted in an aircraft cabin (22) comprises a support (34), to which a PSU duct (34) as well as an individual air supply system (72) are attached. A fastening device (112) is designed to fasten the s...
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WO/2011/081854 |
An aircraft crew rest station includes an overhead crew rest portion including a central deck portion, forward and aft bunk portions, and a central entry vestibule connected between a passenger seating area and the central deck portion. ...
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WO/2011/081830 |
A fireproof, bi-directional decompression panel includes a frame member and a pressure relief panel member that is releasably retained to the frame member to removably cover a decompression vent opening of an aircraft partition, such as ...
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WO/2011/082237 |
A turbomachinery blade for a gas turbine engine is provided and includes an airfoil extending between a leading edge and a trailing edge. In one embodiment the turbomachinery blade is a compressor blade. The blade can include a platform ...
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WO/2011/079519 |
A hydrodynamic method is disclosed. Work is done on a quantity of fluid and the motion range of the fluid is limited, so that the fluid is moved only on a dynamic surface of a dynamic mechanism or the fluid is moved in a back and forth m...
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WO/2011/081854 |
An aircraft crew rest station includes an overhead crew rest portion including a central deck portion, forward and aft bunk portions, and a central entry vestibule connected between a passenger seating area and the central deck portion. ...
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WO/2011/081289 |
Provided is a convenient airplane seat system having a modified seat arrangement to reduce contact and interference between adjacent passengers. In the airplane seat system, a plurality of seats, each having a seat part, a backrest part,...
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WO/2011/081683 |
An aerial vehicle adapted for vertical takeoff and landing using the same set of engines for takeoff and landing as well as for forward flight. An aerial vehicle which is adapted to takeoff with the wings in a vertical as opposed to hori...
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WO/2011/081289 |
Provided is a convenient airplane seat system having a modified seat arrangement to reduce contact and interference between adjacent passengers. In the airplane seat system, a plurality of seats, each having a seat part, a backrest part,...
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WO/2011/079923 |
The invention relates to a control device for aircraft (1), comprising at least one aircraft landing gear (4a, 4b, 4c), which is arranged on an aircraft (1) and has one or more landing gear wheels (3), and a control mechanism (5), which ...
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WO/2011/081635 |
A multi-wing, airfoil fuselage aircraft (1) that is capable of flying in a ground- effect mode includes a main airfoil fuselage wing (2), a fin (8) that extends vertically from this wing, a pivot mount (26) that is affixed to the fin, an...
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WO/2011/080320 |
The invention relates to an aircraft or spacecraft casing, comprising a composite shell made of first rod elements or sandwich core elements and first skin elements, which are connected to the first rod elements or sandwich core elements...
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WO/2011/080286 |
The invention relates to a fuselage (2) for an aircraft, which fuselage is produced of a fiber-reinforced composite material and comprises a skin (4) and a plurality of peripheral reinforcements (12) and only a small number of longitudin...
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WO/2011/081683 |
An aerial vehicle adapted for vertical takeoff and landing using the same set of engines for takeoff and landing as well as for forward flight. An aerial vehicle which is adapted to takeoff with the wings in a vertical as opposed to hori...
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WO/2011/081577 |
The invention concerns an air propeller arrangement (10, 30, 50) for propulsion of a fixed-wing aircraft (8), said arrangement comprising a first air propeller (11, 31, 51) that comprises a first hub member (15, 35, 55) and at least a fi...
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WO/2011/080410 |
The invention relates to a system for carrying and dropping ammunition for a transport airplane. The system (1) includes a container (4) which contains at least one load (3), in particular ammunition, which is capable of being brought in...
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WO/2011/081830 |
A fireproof, bi-directional decompression panel includes a frame member and a pressure relief panel member that is releasably retained to the frame member to removably cover a decompression vent opening of an aircraft partition, such as ...
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WO/2011/079906 |
A system component module (100) to be mounted in an aircraft cabin (22) comprises a support (34), to which a PSU duct (34) as well as an individual air supply system (72) are attached. A fastening device (112) is designed to fasten the s...
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WO/2011/077700 |
Disclosed is a technique that can easily and efficiently disassemble a mandrel with a roughly cylindrical structure that is dividable into a plurality of segments. A rotating process for rotating a pair of support rings in a manner such ...
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WO/2011/076428 |
A high lift system with a main wing and regulating flaps, also bearing devices for the mounting of the regulating flaps, and positioning devices for the positioning of the regulating flaps, wherein the respective bearing device and/or po...
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WO/2011/077698 |
Provided is a die for manufacturing a composite material structure. A single cylindrical die is supported by affixing the end surfaces of slab-shaped first and second segments to a support ring, one at a time with the convex top surfaces...
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WO/2011/077454 |
A rotor blade for a fluid turbine is disclosed. The rotor blade includes a flange section configured to connect the rotor blade to a rotor hub; and an airfoil section extending outward from the flange section. The flange section is compr...
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WO/2011/077366 |
A seating arrangement for a passenger vehicle, the arrangement comprising at least two juxtaposed seats that face the same direction wherein the distal end seats have a bias in a direction towards each other. The distal end seats also ha...
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WO/2011/076427 |
An aircraft (F) with aerofoils (1a, 1b) comprising a main wing (M) and at least one control flap (S) that is arranged so as to be adjustable relative to the aforesaid, and comprising at least one adjustment flap (K), with the aircraft co...
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WO/2011/077363 |
A vehicle seat comprising a seat base including a seat pan defining two opposite edges ("seat ends"), forming the base of the vehicle seat ("seat base"), a reversible backrest, the back rest including a back side and a front side and ada...
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WO/2011/077364 |
A seating arrangement suitable for a passenger vehicle cabin, the seating arrangement comprising a pair of seats aligned with each other, a movable (preferably horizontally aligned) upper bed assembly disposed vertically above at least p...
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WO/2011/076706 |
The invention relates to an ultra-rapid air vehicle and to a method for aerial locomotion provided by an ultra-rapid air vehicle. The air vehicle is propelled by an engine system consisting of jet engines (TB1, TB2), ramjet engines (ST1,...
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WO/2011/077365 |
A vehicle seat configuration, comprising or including, at least two columns of least, where all seats are facing in a direction parallel to each other, each seat in a first of the at least two parallel columns is offset in the seat facin...
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WO/2011/077699 |
Disclosed is a technique that can easily assemble, with high positional accuracy, a mandrel that is used, for example, in the production of an aircraft body, or the like, and has a roughly cylindrical structure that is dividable into a p...
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WO/2011/077424 |
An oscillatory vorticity generator device for controlling the flow on an aero- or hydrodynamic surface (104) of an element (110), the oscillatory vorticity generator device (130) comprising: two main walls, positioned opposite to each ot...
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WO/2011/076202 |
The invention relates to a component (12) designed to be load-adaptive comprising at least one trapezoidal, elastically movable four-bar hinge (10) incorporated integrally into said component in order to generate a shape change behaviour...
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WO/2011/076427 |
An aircraft (F) with aerofoils (1a, 1b) comprising a main wing (M) and at least one control flap (S) that is arranged so as to be adjustable relative to the aforesaid, and comprising at least one adjustment flap (K), with the aircraft co...
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WO/2011/077152 |
Disclosed is air vehicle mounted or mountable transmitting and/or receiving equipment (1) including a transmitting and/or receiving turret (7) allowing at least a forward field of view, said device being mounted or mountable on a fuselag...
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WO/2011/077468 |
Disclosed herein is a method for determining a trajectory for a transfer of a spacecraft from a starting space body to a target space body with respect to a given central space body, wherein the determined trajectory is optimal with resp...
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WO/2011/076425 |
A high-lift system with a main wing and adjustable flaps as well as guiding devices for holding the adjustable flaps and adjustment devices for adjusting the adjustable flaps, wherein the respective guiding device and/or adjustment devic...
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WO/2011/077363 |
A vehicle seat comprising a seat base including a seat pan defining two opposite edges ("seat ends"), forming the base of the vehicle seat ("seat base"), a reversible backrest, the back rest including a back side and a front side and ada...
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WO/2011/076427 |
An aircraft (F) with aerofoils (1a, 1b) comprising a main wing (M) and at least one control flap (S) that is arranged so as to be adjustable relative to the aforesaid, and comprising at least one adjustment flap (K), with the aircraft co...
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WO/2011/078684 |
The present invention provides a rotor assembly for helicopter vehicles for providing an easy way of controlling pitch, roll and lift of the aircraft by respective servo actuators (8a, 8b, 8c). The rotor assembly has a rotor shaft (5a) a...
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