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WO/2011/157943 |
The invention relates to a turbine engine (100) for a helicopter (200), said helicopter comprising a main gearbox, a rotor (204), and a speed-reducing device (206) that is placed entirely within the main gearbox (202) of the helicopter w...
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WO/2011/156347 |
An aircraft control system is presented. The system includes a wing including a flap track, and a shuttle connected to the flap track and configured to slide along a length of the flap track. The system includes a flap panel pivotally at...
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WO/2011/154249 |
The invention relates to a method and device for protecting an aircraft during the flight phase, the aircraft having a plurality of slat and flap configurations. The method comprises the following steps: determining (201), for at least o...
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WO/2011/154797 |
The invention relates to a super-rigid hybrid airship having a modular structure, which comprises a central tube (1) having a diameter of between 5 to 10% of the diameter of the airship, structural rings (2) surrounding and preferably co...
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WO/2011/155485 |
A trochoid drive system (1) is equipped with: wheels (153) disposed in three locations on the periphery of an outer wheel (10) that revolves around a drive shaft (22a); and steering links (16) that revolve with the wheel, and that are ab...
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WO/2011/154645 |
The invention relates to an aircraft electrical power supply circuit including: an power distribution network (17), onboard the aircraft, for electrical devices (5b) located in an engine of the aircraft or near said engine; and a power s...
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WO/2011/155850 |
An inflatable wing for a traction kite, the wing including: a flexible envelope having a first sheet and a second sheet, the first and second sheets joined together at a leading edge, a trailing edge and two spaced apart wing tips; and a...
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WO/2011/155020 |
Disclosed is a flight control support device such that a flight restricted area (W) is set along a terrain, and that thereby the degree of freedom of course selection by a pilot can be sufficiently secured while improving the safety of a...
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WO/2011/156370 |
A ground impact cargo parachute release mechanism includes a pair of interlocking release elements, one for connection to the parachute the other the cargo; each release element has a pawl and a notch for engaging the pawl of the other r...
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WO/2011/154684 |
The present invention describes a flight recorder for an aircraft with an instrument display panel for displaying aircraft status data to a pilot. The flight recorder comprises one or more sensors that monitor one or more flight conditio...
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WO/2011/155866 |
The invention relates to systems for controlling the aerodynamic surfaces (rudder, aileron, etc.) of an aircraft. The electromechanical actuator device for an aerodynamic surface of an aircraft has: a controllable aerodynamic surface tha...
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WO/2011/154340 |
A safety seat for land vehicles, aircraft and watercraft having a seat part frame and a backrest frame, which is suspended on a restraint strap which is attached firmly to the vehicle, wherein the backrest frame has a lateral strut and a...
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WO/2011/154582 |
Procedure for the manufacture of large parts of composite material, controlling the thickness of the edges thereof. It relates to the manufacture of a part (11) possessing edge zone (11) in an aeronautical structure through a join with j...
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WO/2011/153902 |
A safety seat capsule includes a safety capsule (2) and a seat (1) which has a backrest (11) and a cushion (12). The seat (1) is installed in the safety capsule (2) and is detachable from it. A door (21) which can be opened and closed an...
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WO/2011/156062 |
Apparatus for the recovery of an aircraft includes a capture device and first and second pole pairs. Each first and second pole pair includes top and bottom poles. First pole pair is configured to move from a first position, in which the...
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WO/2011/154952 |
A vehicle for towing an airplane by receiving thereupon a nose landing gear of the airplane having an airplane longitudinal axis. The vehicle having a vehicle longitudinal axis and is configured to tow the airplane along a straight or cu...
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WO/2011/155892 |
The invention concerns a lifesaving vehicle (10) designed as a hollow body with the form of a sphere or disk essentially flattened along a vertical axis (16) that demonstrates its greatest width in a horizontal plane (15) and which body,...
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WO/2011/154325 |
Fire fighting device (1) designed to be fixed under a helicopter (50), said helicopter having landing gear (51) and an external load hook (58), said fire fighting device comprising a frame (2), a fluid reservoir (4), an adjustable fluid ...
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WO/2011/150967 |
The aircraft refuelling equipment (20) of an aircraft comprises a pipework (22) in which a fuel supply line (13) is connected to a plurality of tank supply lines, fuel tanks connected to tank supply lines of the pipework, first valves (2...
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WO/2011/152614 |
The present invention relates to a flying object having small bottom blades, which is one type of unmanned rotor craft. A conventional bottom blade type flying object needs an apparatus having a complex configuration constituted by the c...
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WO/2011/151577 |
The invention relates to a nacelle (1) for an aircraft turbojet engine, comprising: a fan casing secured to a supporting pylon and surrounded by an outer fan cowl; an internal structure; a thrust reverser (50) comprising two removable ha...
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WO/2011/151893 |
A path search device (1) for searching for a path for a flight vehicle is provided with a wind information acquisition unit (12) for acquiring wind information as disturbance information, a flying ability information acquisition unit (14...
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WO/2011/151816 |
A primary controller disclosed. The primary controller is configured for controlling operation of a drive system comprising a prime mover, a generator, and a motor, wherein the prime mover is configured to provide energy to the generator...
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WO/2011/151160 |
The invention relates to a power supply unit for an aircraft, such as a helicopter or a fixed-wing aircraft. The power supply unit according to the invention comprises at least one power provision component for providing electrical energ...
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WO/2011/152702 |
A remotely controlled flying apparatus (200) utilized for crop-spraying and crop monitoring purposes is disclosed. The present indention comprises a microcontroller (110) electronically coupled to an inertia measuring means(120). A contr...
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WO/2011/148373 |
A controllable buoyant system (10) includes a support structure having a sealed hollow enclosure (12) containing a first gas and surrounded by a second gas, either the first gas or the second gas being lighter than ambient air. The hollo...
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WO/2011/148085 |
The invention relates to a positioning device for assembling parts on a structure. Specifically, the invention relates to a positioning device intended for assembling stationary brackets on an aircraft structure. A laser projector is att...
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WO/2011/148167 |
A method of sealing a gap between first (1) and second (2) aerodynamic surfaces. The width of the gap between the two surfaces is measured to obtain a gap measurement. The width of a seal member (43) is pre -formed in accordance with the...
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WO/2011/148090 |
Such a mould comprises: a central core (11) having a side wall (17) with a plane external surface (19); an internal mould element (24) having an internal surface (28) facing said external surface (19) of the central core, with said surfa...
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WO/2011/148419 |
The disclosed jet bridge (20) is provided with: an ambulation passage (31); a lift deck (35) that is provided in the plane of the ambulation passage (31) in a planar view and is used to connect to a boarding/deboarding section (11A) of a...
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WO/2011/148187 |
A rotor blade for a rotorcraft includes an actuator assembly (11) comprising a prime mover assembly which is drivable by the prime mover to change the separation of a first connection point (17) of the assembly from a second connection p...
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WO/2011/148158 |
A landing gear (10), including: a bogie beam (12); an axle (14) pivotally connected to the bogie beam (12); a locking member (40) coupled to the axle (14) such that movement of the axle (14) invokes movement of the locking member (40), s...
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WO/2011/149440 |
The new Deturbulator could be is a really significant drag-reducing aerodynamic invention since the development of the now-common laminar-flow airfoils that were developed some 65 years ago. Its small size and lightweight make it easy to...
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WO/2011/149544 |
A quadrotor UAV including ruggedized, integral-battery, load- bearing body, two arms on the load-bearing body, each arm having two rotors, a control module mounted on the load-bearing body, a payload module mounted on the control module,...
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WO/2011/147571 |
The invention concerns a device for a adjustable flap adjustably mounted on a main wing surface of an aeroplane wing, in particular, a landing flap, with at least one adjustment unit for purposes of adjustment of the adjustable flap, whi...
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WO/2011/149440 |
The new Deturbulator could be is a really significant drag-reducing aerodynamic invention since the development of the now-common laminar-flow airfoils that were developed some 65 years ago. Its small size and lightweight make it easy to...
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WO/2011/148199 |
A method of simulating a terrain view from the point of view of an airborne object and a terrain view simulation system which obtain a geo-referenced terrain to the airborne object, correlate in a computer the position and orientation in...
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WO/2011/148186 |
A rotor blade includes an actuator (1) comprising an electric motor (30) having a rotary drive shaft (31), a bearing (32) for mounting the rotary drive shaft along an axis extending along the length of the rotor blade, and a lubrication ...
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WO/2011/145972 |
The invention relates to the field of aircraft construction. The aircraft fuselage comprises consecutive frames (1) with an outer skin (2) secured thereto, stringers (3) connected to the skin (2) and the frames (1), passenger floor cross...
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WO/2011/144236 |
The present invention provides a light for the interior of an aircraft, in particular wash light for an aircraft, comprising a first group of white LEDs (18) each having an InGaN semiconductor material chip, and a second group of amber c...
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WO/2011/144688 |
The rotors of a helicopter are directly connected to electric high-torque machines and are driven by the same. The energy generation and rotor drive are separate from each other. The high-torque machine of the main rotor is mounted on th...
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WO/2011/144298 |
The invention relates to a wing with an extension in the wingspan direction (SWR), in the wing chord direction and in the wing thickness direction (FDR) for use in an aircraft, with a retractable wing end piece (42). A mechanical lever s...
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WO/2011/145291 |
Provided is an occluding member for an opening with which a lightning protection function can be reliably maintained. The occluding member is provided with a first insulator (63) and a second insulator (65) between a door body (30) and a...
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WO/2011/144210 |
Heating and cleaning apparatus for the cleaning and heat-treatment of surfaces, items, joints, cracks and similar by the use of a hot blast jet produced by the exhaust jet of a jet engine where aggregate injectors have been added in the ...
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WO/2011/144692 |
The invention relates to a hybrid drive system for aircraft, in particular helicopters, comprising at least one energy generating module having an internal combustion engine and a generator that can be driven by the same for generating e...
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WO/2011/144690 |
The rotors of a helicopter are driven by electric machines. The electrical energy required therefor is generated by a motor-generator unit (101, 103) which comprises one or several combustion engines (100). The motor-generator unit may b...
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WO/2011/146021 |
The present invention relates to a yaw control and anti-spin device for fixed wing aircraft which is self -powered by means of recuperating the energy from the wingtip or wing's trailing edge vortices, which occur during flight. The same...
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WO/2011/144836 |
The nacelle (1) comprises a stationary shroud (9) and an intake lip (8) that can move axially in relation to the shroud (9) between a rear operating position and a front maintenance position. The aerodynamic element (15) is flexible and ...
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WO/2011/146194 |
A stringer (2) having a stringer end trim (7) that reduces pull-off forces in a stringer connection structure, including a stringer body (9); a stringer free edge (8) provided on said stringer body (9); and a stringer end trim (7) having...
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WO/2011/143680 |
The invention relates to a supporting assembly (5, 6) for a seat, especially a vehicle seat or aircraft seat, comprising a support structure (13), a damping and resetting unit (14) and a top layer (15). The damping and resetting unit (14...
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