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WO/2012/004820 |
The present invention concerns a method for emergency landing of a vehicle, such as an helicopter (1) or like, said vehicle (1) comprising at least one airbag (2, 3) provided with a respective opening valve for allowing the outflow of th...
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WO/2012/006337 |
An optical element for a side emitting light that emits light from a light source at side directions relative to the horizon is disclosed. The optical element has an internal recess adapted to fit over a light source. The internal recess...
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WO/2012/006158 |
In one possible embodiment, a UAV payload module retraction mechanism is provided including a payload pivotally attached to a housing. A biasing member is mounted to bias the payload out of the housing and a winch is attached to the payl...
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WO/2012/003973 |
An aircraft (F) with wings (1; 1a, 1b) and a system for minimizing the influence of unsteady flow states, wherein the wing consists of a respective main wing (M) and at least one control flap (S) adjustably arranged relative thereto, a a...
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WO/2012/004260 |
The invention relates to a method for locating the wiring in an aircraft provided with a harness database (11) containing data relating to the aircraft wiring, said method comprising the following steps: placing a set of radio frequency ...
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WO/2012/003964 |
The invention relates to an interior component carrier system (22) for use in the assembly of aircraft interior components (12, 14, 16, 68, 78) in an aircraft, said system comprising a retaining system (24) with at least one retaining el...
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WO/2012/004594 |
A linkage for guiding a flexible cable between two structures. The linkage comprises a proximal arm with a proximal pivot joint for coupling the proximal arm to a first one of the two structures; and a distal arm which is coupled to the ...
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WO/2012/004490 |
The subject of the invention is a method for producing a central wing box comprising an upper panel (32), a lower panel (34), a front spar (36) and a rear spar (38), the upper edges of said spars (36, 38), which are approximately paralle...
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WO/2012/005634 |
The present invention relates to a device (100) and method for measuring ice thickness on a first surface (110) of a construction element (120). The device comprises a sensor arrangement (130) arranged in connection with said constructio...
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WO/2012/001334 |
The invention relates to a device for protecting against the overspeed of a free turbine (6) of a turbine engine which comprises a gas generator including at least one compressor (1), a combustion chamber (3), at least one linked turbine...
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WO/2012/001205 |
Aircraft component which comprises at least one panel (11) of composite material, formed by a skin (13) and a plurality of stiffening stringers (15) which are configured with a core (17) and a base (19) of width (A), said stiffening stri...
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WO/2012/001207 |
Aircraft fuselage made out with composite material and manufacturing processes. The structure of the fuselage (1 1 ) comprises a skin (13), a plurality of frames (17) positioned transversely to the longitudinal axis (9) of the fuselage (...
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WO/2012/001459 |
A method and apparatus for producing a linear thrust force, comprising an array of phase-shifted electric oscillations having frequency greater than or equal to ratio of the speed of electromagnetic waves in free space to length of the a...
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WO/2012/001259 |
The present invention relates to a turbojet engine nacelle including an air inlet (3) arranged upstream from the turbojet engine, a middle section for surrounding a turbojet engine fan and the housing (6) thereof, and a downstream sectio...
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WO/2012/000908 |
A conveyor apparatus for loading and unloading aircraft (1), said apparatus comprising a first conveyor (14) for conveying articles from an area outside of an aircraft (1) to an entrance to a cargo compartment (2) of the aircraft and a s...
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WO/2012/000664 |
An adjustment system of an aeroplane, having: at least one adjustable flap (A1, A2; B1, B2) on each of the wing of an aeroplane, adjustable with an adjustment device (A11, A12, B11, B12, A21, A22, B21, B22), a drive device (PA1, PA2, PB1...
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WO/2012/001302 |
Apparatus comprising a fixed part, a rotary support able to be rotated with respect to said fixed part, at least one item of electrical equipment (23) carried by said rotary support, and a power supply device able to provide electrical e...
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WO/2012/003512 |
An aircraft hover system for enabling an aircraft to hover at a target spatial location represented by GPS location coordinates. The hover system includes a display screen rendering a display including live video feed of the terrain belo...
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WO/2012/001206 |
Reinforcement structure (1) for an opening (10) in the primary structure of an aircraft, said structure comprising a skin (2), frame members (3) which are transverse with respect to the flying direction of the aircraft, and stringers (4)...
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WO/2012/002276 |
An FPM (30) and a target air attitude angle indication (32) are displayed on a PFD (10) which is an integrated instrument. The target air attitude angle indication (32) is an index showing a target angle of attack and a target air attitu...
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WO/2012/003285 |
Disclosed is a system for the airborne deployment and delivery of palletized cargo. The system includes a cargo pallet, one or more risers connected to the pallet, and an associated rigging. The risers are used in both stabilizing the ca...
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WO/2012/001279 |
A blade (10) comprising: - a structure (20) having an aerodynamic profile comprising two facing skins (21, 22) obtained by three-dimensional weaving of fibre reinforcement densified by a matrix, - a spar (30) consisting of a fibre reinfo...
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WO/2011/163316 |
A system for monitoring for pushrod faults in an aircraft includes a pushrod; a sensor (36) mounted on the pushrod (34), the sensor (36) wirelessly transmitting measured pushrod load data; a receiver (44) receiving the measured pushrod l...
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WO/2011/160172 |
An enclosure (10) for transporting people (1000) to and from high-altitudes, comprising a body (20) adapted for housing the people (1000) having a top portion (30); and a drag inducing structure (60) extending upwardly from the top porti...
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WO/2011/162876 |
There is provided a method for mitigating static discharge in a fuel container. The method provides a static dissipative coating having a volume resistivity of 1.0x109 Ω-m (ohm-meter) or less when measured at 40 V (volts) or less, havin...
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WO/2011/163453 |
A door apparatus (100) includes a door (102), actuating mechanism (104), and tie rod mechanism (126,128), the actuating mechanism actuating the tie rod mechanism to impart a substantially translating motion to the door. The actuating mec...
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WO/2011/163440 |
Described are seat back assemblies including a seat back with a recess and a bezel assembly having a bezel pivotally coupled to the recess and configured to substantially fit within the recess. Other examples may include a tray table ass...
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WO/2011/161359 |
The disclosed system (SYS1) comprises a digital computer (FAD1), the inputs of which a selection module (MSEL1) directs to a sensor (CAPi) or to a substitute digital bus (BSU1) on which substitute digital data (DSUi) generated by a real-...
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WO/2011/161377 |
The invention relates to a method of detecting a fault with the means for de-icing a probe for measuring a physical parameter on an aircraft engine, comprising the successive steps consisting in: - measuring a first value (T1) of the phy...
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WO/2011/161061 |
A device for acquiring mechanical loads on mechanically loaded bodies exhibits a resonance-capable micro-bridge structure (16), an alternating voltage source (22) with a variable frequency, an impedance measuring device (18) for acquirin...
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WO/2011/162844 |
A Combination Ground Vehicle and Helicopter and Fixed Wing Aircraft. A sideways translating tailsitter aircraft.
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WO/2011/159671 |
Method of mounting an engine (50) in a rotary wing aircraft. The method includes providing a rotary wing aircraft having an aircraft body (54) supported in flight through an exterior air space by a rotary wing system rotating with an ope...
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WO/2011/157875 |
The invention relates to a night vision system for viewing selected objects, in order to provide improved night viewing of an object such as the refuelling device (21, 41) used in aerial refuelling operations between an aircraft tanker (...
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WO/2011/159345 |
An Airborne Elevator Apparatus capable of deploying at the same time multiple service loads at different altitudes in the Earth's atmosphere by physically separating tether weight carrier function from the service load weight carrier fun...
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WO/2011/157931 |
The invention relates to a suspension system including a front suspension plane located at an intermediate turboshaft engine casing and connecting same to the pylon, a rear suspension plane located at the exhaust casing of the turboshaft...
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WO/2011/157808 |
The invention relates to a landing gear of an aircraft, characterised in that it comprises two walking beams (1, 2) carrying wheels and mounted in such a way as to pivot on at least one pivot (3, 4) of the landing gear, the landing gear ...
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WO/2011/157834 |
The invention relates to a power supply and control device (20) for a plurality of electrical actuators (7, 8, 9, 10, 11) comprising a control circuit (250) and a power circuit (200), wherein the power circuit comprises an inverter modul...
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WO/2011/157924 |
The invention relates to an aircraft engine (1) including a stator (2), a main shaft (3), a first rotor (4), a second rotor (5), a transmission mechanism (6), a first electrical apparatus supported by the first rotor and a second electri...
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WO/2011/158015 |
An aircraft wing box spanwise joint (2), comprising a rib having a web, and a pair of rib fittings joined together, each rib fitting forming a closed loop around the periphery of the rib, wherein the rib is integrally formed with one of ...
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WO/2011/157879 |
Pin bearing arrangement (10) for measuring loads in an aircraft landing gear (1 ), comprising a trailing arm (2), connected to at least one of the aircraft wheels (3), and a shock absorber (4), connected to the aircraft, whereby load (1 ...
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WO/2011/157926 |
The invention relates to a turbojet engine nacelle, comprising at least one nacelle element (31) having a wall (33) defining a main flow channel (34), said channel (34) having a variable cross-sectional flow area, wherein the cross-secti...
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WO/2011/160032 |
A seat back tray for being pivotally mounted an aircraft seat, and including a frame mounted on the aircraft seat and movable between a stowed position against a seat back of the aircraft seat and a deployed, generally horizontal positio...
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WO/2011/157807 |
The invention relates to a landing gear of an aircraft, comprising two walking beams (1, 2) carrying wheels and mounted in such a way as to pivot on a common pivot (Y1), the landing gear comprising a damping device having two rods (5, 6)...
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WO/2011/157953 |
The invention relates to an air inlet duct (11) for a turbojet nacelle, comprising an upstream annular lip (13) and a downstream outer annular structure (14Ex). The invention is characterised in that the upstream annular lip (13) and the...
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WO/2011/157066 |
A safety belt device for an aero seat on airplane comprises a locking device and a belt (1). The locking device comprises a plug (2) and a locker (3) that are embedded mutually, where the locker (3) is fixed on one side of the aero seat,...
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WO/2011/157965 |
Aircraft turbo jet engine fan casing, notable in that it is in the form of a box section (6), the radially interior wall (6a) of which is able to form the internal skin of the cold air flow duct (17) of a nacelle in which said turbo jet ...
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WO/2011/157962 |
This airflow-straightening structure for an aircraft engine (15) comprises: a hoop (31) inside which there are arranged a plurality of flow-straightening vanes (23) bearing a hub (21) of a fan (19), and a clevis (33) for connecting to a ...
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WO/2011/157265 |
The invention relates to an ejection device for a flight data recorder, comprising an ejection spindle (8), which can be detachably connected to the flight data recorder by means of a bayonet coupling (1), wherein the bayonet coupling (1...
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WO/2011/159281 |
A foldable rotor system for a rotorcraft, the foldable rotor system comprising a rotor assembly operably associated with a driveshaft, the driveshaft being operable associated with an engine, the rotor assembly comprising a rotor blade c...
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WO/2011/157641 |
Recoverable module for propulsion module intended to launch a craft into space, said recoverable module of longitudinal axis (X1), said recoverable module (14) comprising a central body, a propulsive system (8) intended for launching the...
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