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WO/2011/071939 |
A wing spar joint is provided for coupling the inboard ends of a right wing spar and a left wing spar. The wing spar joint comprises a forward fitting ( 62 ), an aft fitting ( 50, 52 ), a spar cap a lower chord fitting ( 64 ) and a strap...
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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/2011/070266 |
The present invention relates to a nacelle rear assembly (1) including a pod-shaped internal structure (11), said internal structure comprising at least one downstream portion (15) and one upstream portion (13) that are each movably moun...
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WO/2011/070536 |
The application provides a component flight-hour updating module (10) of an aircraft. The module comprises at least one Radio Frequency Identifier (RFID) tag (16; 54) being attached to at least one component (15) and a component flight-h...
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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/2011/070536 |
The application provides a component flight-hour updating module (10) of an aircraft. The module comprises at least one Radio Frequency Identifier (RFID) tag (16; 54) being attached to at least one component (15) and a component flight-h...
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WO/2011/071939 |
A wing spar joint is provided for coupling the inboard ends of a right wing spar and a left wing spar. The wing spar joint comprises a forward fitting, an aft fitting, a spar cap a lower chord fitting and a strap member. A first pluralit...
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WO/2011/070072 |
Disclosed are a locking mechanism (100) and a lock (110). The locking mechanism (100) comprises a push-button (148) connected to a freewheel (154) via a traction cable, said freewheel being connected to a drive device (160) of the lock (...
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WO/2011/070531 |
In one embodiment now described, and according to one aspect of the invention. There is provided a leg rest mechanism 100. The leg rest mechanism is suitable for use with a seat pad 200of a seat arrangement 300 in a passenger vehicle (no...
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WO/2011/069887 |
The invention relates to a high-lift system for an aircraft, comprising a lift flap (4) disposed on an airfoil (2), said lift flap being coupled to the airfoil (2) and designed to be displaceable relative to the airfoil (2) between a ret...
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WO/2011/067286 |
The invention relates to a seat that can be converted into a sleeping-berth. The invention comprises a block (2) of adjacent seats (3) that can be converted individually from an armchair configuration to a horizontal sleeping configurati...
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WO/2011/068536 |
Embodiments of a free-floating connector engagement and retention system are provided. In some embodiments, the system includes a slotted mounting surface, a connector carrier guide, and a connector carrier to receive a connector. The co...
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WO/2011/067108 |
The invention relates to a lighting apparatus (1) for a beacon system having at least one VIS-LED (4) as a first light source and a second light source (6) emitting substantially infrared radiation.
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WO/2011/068659 |
An active winglet includes a body portion substantially parallel to a wing of an aircraft, as if it were an extension of the wing, and an angled portion that projects at an upward angle from the body portion. The body portion is attachab...
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WO/2011/066891 |
The invention relates to an aircraft tractor (4) for moving aircrafts (1) coupled thereto on airfields, comprising a drive assembly (5) for driving at least one wheel set (6, 6', 6") of the tractor (4) and at least one coupling unit (7) ...
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WO/2011/068445 |
The invention relates to an unmanned aerial vehicle (UAV) helicopter comprising a dismountable tail section including a torque compensating rotor, wherein power transmission from the motor to the torque compensating rotor is accomplished...
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WO/2011/066950 |
The invention relates to an aircraft fuselage component (4) having an exterior wall (5) with reinforcing elements and having an opening (3, 9) in the exterior wall (5). The aircraft fuselage component (4) is designed as an integral fibre...
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WO/2011/066708 |
An aerobat toy, which includes propellers (30), a fuselage (50) and an undercarriage (70), is provided. The propellers (30) have a first propeller (310) set on the top of the fuselage (50) and a second propeller (320) set between the fus...
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WO/2011/067286 |
The invention relates to a seat that can be converted into a sleeping-berth. The invention comprises a block (2) of adjacent seats (3) that can be converted individually from an armchair configuration to a horizontal sleeping configurati...
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WO/2011/067248 |
The present invention relates to an airfoil shaped body with a leading edge and a trailing edge extending along the longitudinal extension of the body and defining a profile chord, the airfoil shaped body comprising an airfoil shaped fac...
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WO/2011/067334 |
The invention relates to a safety system (S) for an aircraft (1) for storing flight (FD) and voice data (SD) relevant for reconstructing crashes, having a data collection device (6) connected to sensors (4, 5) of the aircraft (1) and by ...
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WO/2011/068659 |
An active winglet includes a body portion substantially parallel to a wing of an aircraft, as if it were an extension of the wing, and an angled portion that projects at an upward angle from the body portion. The body portion is attachab...
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WO/2011/067527 |
The invention relates to a device suitable for vertical and horizontal transport of loads, in particular heavy loads, in good weather conditions, using the load-bearing capacity obtained by means of blowing a stream of air, produced by a...
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WO/2011/068443 |
The invention relates to helicopters with removable fuel tanks, wherein all fuel tanks of the helicopter are removable fuel tanks. Helicopters all fuel tanks of which are removable can safely be stored on ships and aircraft carriers.
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WO/2011/068828 |
Embodiments of the present invention include a seat back pivotally coupled to a seat frame via a pivot shaft, wherein a lower end of the seat back does not extend below the pivot shaft, a seat pan fixedly coupled to the seat frame, at le...
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WO/2011/068828 |
Embodiments of the present invention include a seat back pivotally coupled to a seat frame via a pivot shaft, wherein a lower end of the seat back does not extend below the pivot shaft, a seat pan fixedly coupled to the seat frame, at le...
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WO/2011/068193 |
Disclosed is a method for clearing space debris in earth orbit, wherein, in earth orbit, a spatial region is provided having a greater resistive force than the atmosphere in said earth orbit, and space debris passing through said spatial...
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WO/2011/064715 |
Solar collector (1) comprising: a deformable tubular body (2) including a transparent portion (4) and an internally reflecting portion (6), said tubular body (2) being deformable from a contracted position to at least one deployed positi...
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WO/2011/066233 |
Disclosed herein, in certain embodiments, is a method of altering the stability of unstable space debris. In some embodiments, the method further comprises changing the orbit of the unstable space debris.
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WO/2011/064519 |
The invention relates to an aircraft comprising a structural element, such as a fuselage, a wing or a tail unit, including: a wall separating the inside and the outside of the element and including portions jointly defining an inner volu...
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WO/2011/066031 |
A system comprising an aerial vehicle or an unmanned aerial vehicle (UAV) (100,400,1000,1500) configured to control pitch, roll, and/or yaw via airfoils (141,142,1345,1346) having resiliently mounted trailing edges opposed by fuselage-ho...
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WO/2011/064356 |
The invention relates to a cargo hold floor for a cargo hold of an aircraft. The cargo hold floor comprises a plurality of panels for forming the cargo hold floor, wherein the panels have rail segments for forming rails extending over a ...
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WO/2011/064808 |
A machine (1) for. extending and retracting an extendable corrugated hose (3) comprises a tubular housing (4) for storing the extendable corrugated hose (3) in a retracted condition, tubular housing (4) having a rear end (5), which is co...
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WO/2011/063978 |
The invention relates to an aircraft seat assembly (10) for aircraft passengers having restricted mobility comprising a seat base assembly (14) that can be mounted in an aircraft cabin (12) and comprises a first carrier device (22) and a...
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WO/2011/064520 |
The invention relates to a method for creating a sealed joint (118) between elongate parts (14, 116) of an aircraft extending locally in main directions that are not mutually parallel; a plurality of parts of a mould are assembled on the...
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WO/2011/064263 |
The invention relates to a structural element made of a layered composite material in the form of an elongate profile section and comprising, in a thickness of the layering, three cores consisting of an electrically conductive material c...
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WO/2011/063483 |
The present invention relates to a force modulating apparatus, more specifically to an apparatus for minimising and/or cancelling forces such as the Coriolis, gravitational and centrifugal forces, thus simulating outer space conditions. ...
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WO/2011/064531 |
The present invention relates to an improved sensor arrangement, a system and method for determining the rate of ice formation and how close conditions are to those at which ice will form on a surface, and to an improved sensor arrangeme...
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WO/2011/066004 |
A convertible combined road, water, and aircraft vehicle (2) has a road form, a water form, and an aircraft form. The vehicle includes a vehicle body having a passenger compartment (16) and wheels (10,12) supporting the vehicle body on t...
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WO/2011/066233 |
Disclosed herein, in certain embodiments, is a method of altering the stability of unstable space debris. In some embodiments, the method further comprises changing the orbit of the unstable space debris.
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WO/2011/064261 |
The invention relates to a structural stiffener made of a layered composite material comprising a head (11) held at a distance from a sole plate by means of which said stiffener is intended to be attached to a panel. The head (11) compri...
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WO/2011/064456 |
The invention relates to the wing of a flying apparatus and a flying apparatus, the leading edge of which wing is at least partly at a sweep, on which leading edge part at a sweep are arranged means (2, 2') which, when activated, raise c...
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WO/2011/064419 |
Concave blade for wind turbine, formed by a body (1) determined by a surface that defines a concavity (3), with a flattened part (2) at one extremity, to be attached, using said flattened part (2), in a radial position to a supporting disk.
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WO/2011/066030 |
An unmanned aerial vehicle (UAV) launch tube (100) that comprises at least one inner layer of prepreg substrate (370) disposed about a right parallelepiped aperture (305), at least one outer layer of prepreg substrate (380) disposed abou...
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WO/2011/064519 |
The invention relates to an aircraft comprising a structural element, such as a fuselage, a wing or a tail unit, including: a wall separating the inside and the outside of the element and including portions jointly defining an inner volu...
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WO/2011/064356 |
The invention relates to a cargo hold floor for a cargo hold of an aircraft. The cargo hold floor comprises a plurality of panels (110a, 110b) for forming the cargo hold floor, wherein the panels have rail segments for forming rails (120...
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WO/2011/066031 |
A system comprising an aerial vehicle or an unmanned aerial vehicle (UAV) (100,400,1000,1500) configured to control pitch, roll, and/or yaw via airfoils (141,142,1345,1346) having resiliently mounted trailing edges opposed by fuselage-ho...
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WO/2011/064531 |
The present invention relates to an improved sensor arrangement, a system and method for determining the rate of ice formation and how close conditions are to those at which ice will form on a surface, and to an improved sensor arrangeme...
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WO/2011/064565 |
There is herein described an unmanned aerial vehicle capable of inspecting, identifying, and/or categorising defects on objects to be inspected using visible and/or non-visible wavelengths from infra-red to ultraviolet. More particularly...
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WO/2011/066410 |
Embodiments include an assembly comprising: (a) a camera support structure comprising: a masthead (320) disposed on the distal end of a mast (210) wherein the masthead (320) is configured to receive an imaging element (1110); where a pro...
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