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WO/2008/029048 |
The invention relates to a panel assembly in which the joint between two adjacent panels is closed by a seal (20), said assembly being characterized in that the seal comprises a central part (21) housed in a gap (19) formed between the t...
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WO/2008/028474 |
The invention relates to a method for actuating an aircraft landing gear, according to which a controlled speed profile for actuating the aircraft landing gear between the end positions thereof is used without monitoring the position of ...
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WO/2008/030175 |
A nozzle arrangement for use in a gas thruster is presented. At least one heater micro structure (20) is arranged in a stagnation chamber (12) of the gas thruster. The heater microstructure (20) comprises a core of silicon or a silicon c...
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WO/2008/029095 |
A flow control actuator (10) for a body exposed to fluid flow comprises first and second flow surfaces (14, 16) spaced to define an elongate gap (20) therebetween. An elongate control element is disposed in or adjacent the gap and has an...
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WO/2008/030097 |
The invention pertains to use of a low-temperature ozone conversion means containing an ozone catalyst composition supported on a honeycomb structure in cabin conditioning and/or inerting fuel tanks. The ozone conversion means preferably...
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WO/2008/028473 |
The invention relates to a method for actuating aircraft landing gear, whereby the displacement speed of the aircraft landing gear over the entire duration of displacement or over most of said duration is selected in such a way that the ...
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WO/2008/029049 |
The invention relates to a panel assembly (100) in which two panels (101, 102) are connected together, in which assembly a surface of each of the two panels comprises a step (105, 106), in such a way as to form an upper level (112, 114) ...
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WO/2008/025940 |
A mobile aeroengine washing cart (50) , and a method of their operation, comprises a platform (52) having two lateral walls (64) , a front wall (62) and a drip tray (58) for capturing washing medium during an engine washing operation. Th...
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WO/2008/025128 |
The present invention is a device that allows the pressure inside an aircraft landing gear shock strut to be measured. A charging valve is modified by integrating a small pressure sensing device into the stem of the part such that the ac...
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WO/2008/025860 |
The invention relates to a tubular component (19) for a fuselage, which is made from composite materials and comprises a cylindrical or truncated-cone-shaped seamless outer casing (1), a plurality of stiffening elements (2) disposed long...
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WO/2008/025139 |
A hybrid lift air vehicle for lifting and transporting a payload to a delivery location, which comprises a helium or other lighter-than-air gas filled envelope mounted on an airframe. Variable and reversible vertical thrusters are positi...
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WO/2008/025890 |
The present invention relates to a locking system (20) for a movable lateral cowl (8) of a turbine engine nacelle intended to be connected to a pylon (4) of an aircraft, comprising, on the one hand, a clevis (21) intended to be connected...
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WO/2008/022641 |
The present invention concerns a mounting device for fastening a chair or seat to a groove (41), said groove comprising engagement means (45), where the mounting device comprises locking means (20) prepared for entering the groove and fo...
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WO/2008/022773 |
A frame element (10; 10') for use in an aircraft component assembly system (46) is attachable to an aircraft structure (36) and comprises at least one fastening device for fastening at least one aircraft interior component (34) or at lea...
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WO/2008/024178 |
An improved powered hinge (20) with an automatic locking feature proximate the ends of permissible relative angular displacement of its two hinge sections broadly includes: a stationary member (23) having a pivotal axis (x-x), and having...
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WO/2008/022977 |
The invention relates to the loading and unloading of items of flight luggage in an airport.
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WO/2008/022752 |
A frame element (10; 10') for use in an aircraft air-conditioning system is attachable to an aircraft structure (36) and includes at least one strut (12, 14, 16, 18; 12', 14', 16') which is formed at least in sections as a hollow cylinde...
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WO/2008/022965 |
The present invention essentially relates to an aircraft comprising a fuselage (2) with a cockpit (4) for receiving passengers and/or a load and a propulsion system, said propulsion system comprising at least a tank (6) and/or a combusti...
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WO/2008/022688 |
A frame element (10) for use in an aircraft component installation system (46) is attachable to an aircraft structure (36) and comprises a storage bin fastening device which is designed to fasten a storage bin (26) at various positions o...
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WO/2008/022428 |
A transferable modified leading edge for a wing is detachably mountable to a parent wing. The parent wing may use a NACA 23000-series airfoil. A modified wing tip may be used in conjunction with the modified leading edge. The modified le...
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WO/2008/023198 |
An jam-tolerant actuator (2), comprises a housing (4), a first prime mover (6) for producing rotary motion, a first gearbox (10) arranged to convert in use the rotary motion from the first prime mover (6) into rotary motion. The first ge...
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WO/2008/019858 |
The invention is based on a seat arrangement, in particular for an aircraft seat (10), with a back rest unit (12). It is proposed that the back rest unit (12) has at least one stiffening means (16) in a seat region (14).
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WO/2008/019561 |
A Cable conveying apparatus for passenger bridge particularly for three-tunnel bridge is provided. The first chain conduit is provided beneath the first tunnel and includes a first chain bracket (4) and a first chain. The first chain bra...
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WO/2008/020683 |
The present invention provides a main rotor assembly for a helicopter that can easily generate lift forces and improve output and flight stability. The main rotor assembly for a helicopter includes a mast that is provided to stand in a h...
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WO/2008/020848 |
A torque coupling for a rotor head of a rotary-wing aircraft is configured for rotation with a mast and for causing rotation of an attached yoke. The coupling has trunnions that rotate with the mast and extend generally radially. Pad-bea...
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WO/2008/020248 |
A rib bay platform (1) for use in an aircraft rib bay, is adjustable in length (for example it comprises two telescopically mounted sections (3, 5). The platform (1) comprises a first end (7) configured for mounting on a stringer of the ...
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WO/2008/019700 |
The invention relates to an aerodynamic profiled element for generating power by means of a tractive force, especially for driving watercraft. Said profiled element comprises a flexible top layer that extends in a transversal direction a...
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WO/2008/020084 |
A cart (100) for storage of items, such as air passenger luggage, and transport thereof between, e.g., airport sorting apparatus and aircrafts, comprises a chassis (104) and a storage sect ion (102). The storage section comprises one or ...
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WO/2008/019812 |
The invention relates to an aerostat (1) which can be tethered by cables but can move in the direction in which the cables extend, with the aerostat (1) having a drive and, via its drive (14), a friction connection to at least one of the...
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WO/2008/020419 |
This invention relates to a collector rotor (10) and to a related airplane tyre (116.1). The collector rotor (10) is for harvesting energy from fluid flow, e.g. airflow or water flow. The rotor includes an arrangement of fluid flow barri...
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WO/2008/019692 |
The invention is a leg-rest for the lower legs and feet formed as a hammock with a bottom, 2 sides and a backside, the bottom mainly being a wooden/plastic shell lined with a soft material, as a horizontal support sheet for the lower leg...
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WO/2008/019697 |
Suspending a body in air or reducing its weights by a balloon filled of light nonflammable gas which is charged by a compressed gas in a tank during any emergency. Regaining the gas in the tank happens by an engine and a valve that allow...
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WO/2008/017567 |
An air inlet (2, 3) for a jet engine (1) is disclosed. The air inlet (2, 3) has a housing (5) with an inlet lip (51) which is mounted on the surface (6) of the aircraft. The flow upstream of the air inlet (2, 3) has a boundary layer (9)....
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WO/2008/017763 |
The invention relates to an aircraft sub-assembly comprising at least one seat (28, 39) and/or rest (40) for a passenger, characterised in that it also includes a separation panel (38) extending along one of the two opposed sides of said...
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WO/2008/017606 |
A sensor for sweat or other aqueous discharge onto skin comprises a plastic optical fibre comprising a core and cladding, said core being in intimate contact at a first end with a light emitter and at a second end with a light detector, ...
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WO/2008/017134 |
It is described a non-movable aerodynamic device of fence type (F) installed on the leading edge of a wing (W) of an aircraft, close to a slat (S), however said fence is not fastened to said slat, so that when the slat (S) is extended or...
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WO/2008/017901 |
The invention relates to a storage box (13) in which is received a protective mask (4) adapted to be applied on the face of an aircraft crewmember, said storage box further comprising signaling means (19) activable upon occurrence in the...
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WO/2008/015082 |
The invention provides a method for producing a component (37) for aerospace, with the following method steps: supplying a lay-up arrangement (1) to be laid by means of a tape-laying machine (25), with a glass-fibre lay-up (8), which is ...
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WO/2008/016928 |
Embodiments of the subject invention relate to a Wingless Hovering Micro Air Vehicle (WHOMAV) and its Power Source Unit (PSU). Embodiments can operate at reasonable power levels for hovering and withstanding expected wind gusts. Embodime...
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WO/2008/014912 |
An aircraft air-conditioning unit (10) includes a compressor (18) and a motor (20) driving the compressor (18). A fuel cell system (24) is connected directly to a control unit (22) for controlling the motor (20) driving the compressor (1...
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WO/2008/015663 |
A system for landing UAV's comprising a slingshot structure (25) that includes a central arm (26) and an axis means (45) installed along the central arm of the structure and wherein it enables the central arm to move around it in additio...
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WO/2008/015356 |
The invention concerns a device for detecting and eliminating a layer of ice formed on the surface of an aircraft structure (6) or a liquid that has infiltrated inside of a structure and/or into the material of the structure. According t...
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WO/2008/015360 |
The invention concerns a doorway (1) in an aircraft fuselage (2) comprising a door frame in which a door is mounted, this frame comprising an outer framework (60), an inner framework (50) and a core (40) placed between the inner framewor...
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WO/2008/015362 |
The invention concerns a rear frame of an air intake of a nacelle of an aircraft, characterized in that it is partly made of fiber-reinforced geopolymer resin-based composite material and comprises at least one part (56) that surrounds a...
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WO/2008/014973 |
The invention relates to a pressure suit (01) for a person, having a substantially fluid-tight outer skin (02) which envelops the body of the person at least in regions, wherein the pressure suit (01) has at least one partial zone (03) w...
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WO/2008/012427 |
A rack comprises a compartment which has an open face for inserting and removing luggage, a lower face (8) and an end wall (10) opposite the open face. This compartment is mounted such that it can pivot about a fixed pivot axis (4) betwe...
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WO/2008/010226 |
A deployable wing arrangement or kit is provided for use with a longitudinally extending fuselage (20) having an upper portion and a lower portion. The kit includes a first pair of wings (100) pivotably mountable with respect to said upp...
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WO/2008/010728 |
An aerial delivery device which includes a carrier configured to carry an item for delivery, and one or more wings attached to the carrier and arranged to extend therefrom; wherein said aerial delivery device is configured to provide a c...
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WO/2008/009921 |
A heated leading edge component for an aircraft and a method of manufacture thereof. The leading edge component includes an outer skin, a supporting rib for the outer skin, and a cavity located substantially in-between the outer skin and...
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WO/2008/006823 |
The invention relates to an engine assembly for an aircraft, comprising an engine, an engine mounting device (4) and a cowling enclosing the engine provided with fan shrouds (34), the mounting device (4) having a rigid structure (8) and ...
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