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WO/2011/079138 |
An electrospray thruster and methods of manufacturing such thrusters are provided. The micro-electrospray thruster increases the thrust density of conventional electrospray thrusters by miniaturizing the individual components of the thru...
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WO/2011/077030 |
The device intended for double glazing comprising at least one outer glazing (1) and one inner glazing (2), which glazings are separated by a gas-filled intermediate space (3), used for insulating an interior environment against an exter...
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WO/2011/076762 |
A wing assembly (2) with an adjustable flap (6, 6'), which can be adjusted between a retracted position and at least one extended position, has at least one casing element (10) for encasing a flap adjusting mechanism, and at least one co...
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WO/2011/076425 |
A high-lift system (100) with a main wing (112) and adjustable flaps (110) as well as guiding devices (130) for holding the adjustable flaps (110) and adjustment devices (120) for adjusting the adjustable flaps (110), wherein the respect...
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WO/2011/077025 |
The invention relates to a method for repairing aircraft primary structures. In particular, the invention relates to a method for repairing damage to the coating (1) of an aircraft fuselage, said coating comprising a fiber-reinforced com...
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WO/2011/076428 |
A high lift system (100) with a main wing (112) and regulating flaps (110), also bearing devices (130) for the mounting of the regulating flaps (110), and positioning devices (120) for the positioning of the regulating flaps (110), where...
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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/2011/073827 |
A rotor for a rotary wing aircraft is provided, which includes a hub and a number of rotor blades (10). Each rotor blade (10) includes an elongate central body (14) that has a leading edge (16) and a flap (20) along the leading edge (16)...
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WO/2011/073079 |
The present invention relates to a method for measuring the angular position of a contrasting edge of an object having a luminance transition zone which is substantially rectilinear in a given direction and separates two regions of diffe...
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WO/2011/073590 |
The invention relates to a system for motorising a wheel (2), said system including an engine block (4), a driving member (6) secured to the wheel (2) and a clutch device (7) connecting the output shaft (8) of the engine block (4) to the...
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WO/2011/073565 |
The subject of the invention is an aircraft nacelle air intake comprising a duct extending around the circumference of said air intake and means (24) for the localized injection of hot air into said duct to make the hot air circulate in ...
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WO/2011/075251 |
Position determining systems and methods are provided. A particular portable device includes a calibration component to communicate with a local positioning system to determine an initial position and orientation of the portable device w...
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WO/2011/073493 |
A telescoping tube (42) for fuel transfer operations, this tube (42) comprising a fixed part (41 ) and a moving part (40), such that this moving part (40) comprises in turn means for dynamic sealing (21 ) which guarantee the sealing of t...
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WO/2011/073846 |
An optical device (1) for indicating the glide angle of aircraft comprises at least one light source (2) of predetermined colour, at least one unit (4) for creating a light image, coinciding with the light source (2), and at least one un...
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WO/2011/073573 |
The invention relates to a method for producing a structural composite trailing edge panel (1) for an aircraft element having: an upper surface (3), a lower surface (5), and a trailing edge (7) connecting said upper (3) and lower (5) sur...
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WO/2011/073561 |
The invention relates to an air inlet of an aircraft nacelle including a pipe, extending over the circumference of said air inlet and defined in the back by a front frame, and a means for the localized injection of hot air into said pipe...
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WO/2011/074978 |
There is described a system for a landing site (1) for a helicopter or a load suspended from a helicopter, where landing positioning references are visualised as a luminous pattern (2) on the landing site (1), and where the landing posit...
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WO/2011/073099 |
The invention relates to a force transmission fitting (2) for lightweight components (18), comprising two radial force transmission surfaces (6, 8), at least one axial force transmission surface (4) and at least one receiving means (10) ...
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WO/2011/073063 |
The present invention provides a system (1), in particular, for an aircraft or spacecraft (2), having: a first vehicle component (3) which has one or more primary windings (P1-PN); a second vehicle component (6) which has one or more sec...
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WO/2011/073650 |
The invention relates to an apparatus for transporting and dispersing solid particles into the earth's stratosphere, comprising a conduit connecting a substantially ground level location to an elevated location, a particle transport mean...
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WO/2011/073659 |
A resonance engine is disclosed comprising: a driver plate (12), to which is coupled at least one oscillatory transducer (14); a drive signal generator connected to the oscillatory transducer for excitation thereof; a first spring-mass r...
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WO/2011/073587 |
The invention relates to a system for motorising a wheel (5) connected to a suspension, the system including an engine block (3) and a driving member (4) secured to the wheel (5). According to the invention, the engine block is secured t...
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WO/2011/073573 |
The invention relates to a structural composite trailing edge panel (1) for an aircraft element having: an upper surface (3), a lower surface (5), and a trailing edge (7) connecting said upper (3) and lower (5) surfaces, the upper surfac...
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WO/2011/073493 |
A telescoping tube (42) for fuel transfer operations, this tube (42) comprising a fixed part (41 ) and a moving part (40), such that this moving part (40) comprises in turn means for dynamic sealing (21 ) which guarantee the sealing of t...
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WO/2011/072362 |
Frequency multiplexed command signaling that permits a single pilot command interface (e.g. control stick) to serve as a multiple response mode interface for piloting a craft conforms with natural interface operation of most pilots. High...
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WO/2011/074350 |
Provided are an aviation air bag which inflates across a plurality of seats; an air bag device provided with this air bag; and an aircraft wherein this air bag device is installed. The air bag (1) comprises a bag body (2) which is locate...
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WO/2011/072366 |
Disclosed is an electric accumulator for selectively operating at least one aircraft device. The electric accumulator includes an ultra-capacitor array for storing electrical energy, which can later be used to power an aircraft device. T...
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WO/2011/075344 |
Embodiments of the invention are directed to metal- or metal alloy-coated sheet materials (hereinafter, "metal-coated sheet material") including, but not limited to, fabrics and veils which have a metal content of between one (1) and fif...
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WO/2011/073477 |
The invention relates to a device for protecting sensitive areas against the impact of foreign objects. The device includes a flexible, laminar, impact-resistant body (1) disposed at a distance from the body (4) to be protected and on th...
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WO/2011/074245 |
Provided is an electronic system mounted on an aircraft, wherein it is possible to reduce the number of wires and electronic devices needed by integrating the control system. Specifically, the airframe (80) of an aircraft (100) is divide...
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WO/2011/073566 |
The invention relates to a method for designing repair kits for a predefined area of the external/internal structure of an aircraft, said repair kits each including an external/internal structural part having predefined shape and size, s...
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WO/2011/073565 |
The subject of the invention is an aircraft nacelle air intake comprising a duct extending around the circumference of said air intake and means (24) for the localized injection of hot air into said duct to make the hot air circulate in ...
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WO/2011/073315 |
The invention relates to a structural element (2) capable of recovering static compressive forces along an axis Z. Said structural element comprises two profile members (21, 22) made of fibrous composite material that extend along the ax...
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WO/2011/073551 |
The present invention relates to a supporting structure (200) for a nacelle of a jet engine, in particular provided with a thrust reverser device, including at least one base body (201) made of a composite material, characterised in that...
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WO/2011/069655 |
The invention relates to a line replaceable unit (LRU) (2) for an aircraft (1). According to the invention, the line replaceable unit comprises: a) a first main memory (7), which contains the software needed for certification of the LRU ...
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WO/2011/069875 |
The invention relates to a lock for a luggage box installed overhead in the cabin of an aircraft, comprising a stationary housing and a cover that can move about a rotary axis. The lock comprises a locking pin device that can be mounted ...
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WO/2011/070349 |
The invention relates to the protection of spacecraft (501) from debris (701) and to de-orbiting devices of the atmospheric drag type, and to debris sweeping apparatus for the removal of debris from the space environment. The debris shie...
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WO/2011/070340 |
An aircraft landing gear including a fairing (12) arranged to be moveable between first and second configurations, wherein in the first configuration the fairing shields an element of the landing gear from an incident airflow, the fairin...
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WO/2011/069641 |
The invention relates to a seat device of a passenger seat (10), which comprises a backrest (14), which in a normal adjustment range can be adjusted by a movement in a forward direction (16) from at least one stable comfort position (20)...
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WO/2011/070515 |
A seat that includes a backrest with a back side defined at least in part by a shell that includes a recess in which a visual display screen is mounted and in which a receptacle is disposed below the visual display screen, for use by a p...
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WO/2011/069981 |
The invention relates to a polygonal ring (17) for supporting the blades of the propeller, which consists of two annular end sides (20, 21) spaced apart parallel to one another and between which rings (23) having radial cylindrical reces...
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WO/2011/070347 |
An aerodynamic control surface assembly comprising: an aerodynamic control surface (4); an actuator (10) for controlling deployment of the control surface; and a locking mechanism (30) moveable from a locked to an unlocked position. When...
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WO/2011/070345 |
A slat support assembly is disclosed. It comprises a slat support arm having a toothed rack (10), the slat support arm being movable to deploy a slat attached to one end of said slat support arm from a leading edge of an aircraft wing an...
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WO/2011/070260 |
The invention relates to an assembly for holding the interface of a stationary outer structure (15) of a nacelle (3) and housing (27) of a jet engine (5), said assembly including: - a first raised element belonging to the upstream end of...
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WO/2011/070260 |
The invention relates to an assembly for holding the interface of a stationary outer structure (15) of a nacelle (3) and housing (27) of a jet engine (5), said assembly including: - a first raised element belonging to the upstream end of...
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WO/2011/069899 |
The invention relates to a method for connecting a fiber composite component (2) to a structural component (3) of an air and spacecraft, wherein a metal foil (4) is provided between the fiber composite component (2) and the structural co...
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WO/2011/071602 |
A device for producing electrical power. A thermoelectric device is coupled to an aircraft bleed system for generating electrical power using temperature differentials between ram air and bleed air.
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WO/2011/069650 |
An aircraft (F), which has a respective arrangement (20) of flow-influencing devices (16; 16K) in at least one surface segment (10; 11 a, 12a; 11 b, 12b) of each wing (M; 1 a, 1 b) extending in the wingspan direction in order to influenc...
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WO/2011/070532 |
This invention discloses a wingtip (10) arrangement for an aircraft wing comprising at least one winglet (12) movably mountable to an extremity (16) of the wing (14); and actuating means (18) connected to the winglet for actuating in use...
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WO/2011/070516 |
A cup holder comprising, a housing, a carrier member slidably engaged to the housing and movable between a condition where it is housed within the housing and condition where it at least partially extends from the housing, a cup receptac...
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