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WO/2011/056285 |
An aircraft system for improved cooling efficiency comprises at least one air conditioning pack (44), coupled to an aircraft, having at least one air compression device (50) powered by at least one power source (62) and having an air com...
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WO/2011/055062 |
The invention relates to a method for manufacturing an engine pylon (7) to be mounted between an engine (1) and an aircraft wing (6), said method comprising: mounting a pylon box (8) around a main structure (9), the box having a substant...
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WO/2011/055061 |
The flying vehicle comprises a means (4) that is capable of moving the jet nozzle (1) in the absence of propulsion so as to generate inertial forces for stabilizing the vehicle.
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WO/2011/056791 |
The present invention enhances the optical features of acrostats. The invention utilizes a barrier film having at least one layer containing optically enhancing elements. Aerostats formed from the barrier film possess unique aesthetic fe...
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WO/2011/056082 |
The object of the invention is an aircraft provided with a device for creating a constant moment in relation to the axis of rotation of an additional control surface placed at the front of the aircraft at an as large as possible distance...
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WO/2011/054683 |
The present invention relates to an aircraft or spacecraft, comprising a cargo space (8) for receiving cargo and at least one wall element (10) disposed between the cargo space (8) and an area (2, 16) adjacent thereto and comprising at l...
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WO/2011/055524 |
Provided is a bladder type of jig for manufacture of a composite material structure. The jig is particularly useful for manufacture of a stiffened panel structure employing a hat-type stringer and is sufficiently durable to withstand rep...
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WO/2011/054532 |
A wing (10a) of an aircraft provided with a main wing (10) and an arrangement of leading edge lifting bodies (13a), which as seen with reference to the incident flow direction (F) are arranged on the leading edge, which are adjustably ar...
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WO/2011/054907 |
The invention relates to a method for operating a loading system for loading luggage (90, 90a-90f) at an airport. The loading system used for this purpose comprises a transport system (10) having at least one feed section (14a-14b, 16a-1...
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WO/2011/055097 |
The invention relates to a front section (1) of the fuselage of an aircraft comprising secure access between the cockpit (2) and the passenger cabin (3) while being compact. For this purpose, the front section (1) comprises a separation ...
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WO/2011/054683 |
The present invention relates to an aircraft or spacecraft, comprising a cargo space (8) for receiving cargo and at least one wall element (10) disposed between the cargo space (8) and an area (2, 16) adjacent thereto and comprising at l...
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WO/2011/056082 |
The object of the invention is an aircraft provided with a device for creating a constant moment in relation to the axis of rotation of an additional control surface placed at the front of the aircraft at an as large as possible distance...
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WO/2011/056795 |
Examples of the present invention may include a low visibility landing system for guiding aircraft on landing approaches. The low visibility landing system may aid a pilot during landing in low visibility conditions such that an aircraft...
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WO/2011/056257 |
An electromagnetic inertial actuator includes a support base (3) and a parallel arrangement (5) of a first flexure part (7), a voice coil motor part (9), and a second flexure part (11). The parallel arrangement (5) is cantilevered from t...
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WO/2011/056795 |
Examples of the present invention may include a low visibility landing system for guiding aircraft on landing approaches. The low visibility landing system may aid a pilot during landing in low visibility conditions such that an aircraft...
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WO/2011/054084 |
A helicopter settling protector and method of manufacturing same, the settling protector being made of a thermoformed thermoplastic, preferably a polycarbonate resin thermoplastic, and adapted to be connected to a skid tube of a helicopt...
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WO/2011/054532 |
A wing (10a) of an aircraft provided with a main wing (10) and an arrangement of leading edge lifting bodies (13a), which as seen with reference to the incident flow direction (F) are arranged on the leading edge, which are adjustably ar...
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WO/2011/056791 |
The present invention enhances the optical features of acrostats. The invention utilizes a barrier film having at least one layer containing optically enhancing elements. Aerostats formed from the barrier film possess unique aesthetic fe...
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WO/2011/054047 |
A compound motion structure (3) for connection between two surfaces comprising a first arm (5) and a second arm (7) swingable coupled together through a first hinge connection ( 13), a first surface (35) coupled to an opposite end of the...
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WO/2011/056763 |
Embodiments of the present invention provide steam oven drain valve systems (22) and methods for draining steam ovens and associated water lines (18) on aircraft and other passenger transport vehicles.
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WO/2011/055097 |
The invention relates to a front section (1) of the fuselage of an aircraft comprising secure access between the cockpit (2) and the passenger cabin (3) while being compact. For this purpose, the front section (1) comprises a separation ...
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WO/2011/052714 |
Provided are a joint structure for a composite member and a metal member adhered to the composite member by way of an adhesive surface. The metal member has a slit extending along the adhesive surface in such a way that a thin portion is...
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WO/2011/050452 |
A vertical axis turbine includes a modified darrieus type rotor having at least three circumferentially spaced apart blades, each having an airfoil shape in cross section such that the blades generate a torque in a direction of rotation ...
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WO/2011/053805 |
A Real-time Allocation Flight Management System and method, which defines specific roles functions for crew during the implementation of the flight plan. The flight control system requires crew input during pre-programmed way points duri...
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WO/2011/051148 |
A storage compartment module having an integrated supply channel for optimized installation comprises a housing (100) having a storage compartment receiving space (180) and a passenger supply channel (160), a storage compartment (200) wi...
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WO/2011/051699 |
There is provided an aerofoil comprising an inboard section, a tip section moveable between a flying configuration and a parked configuration, a hinge shaft mounted at a compound angle in the inboard section, a fixed gear mounted concent...
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WO/2011/051698 |
A curable flexible electromagnetic hazard resistance laminate, comprising a layer of electrically conductive metal material and thermosetting resin, wherein a first external face of the laminate comprises a releasable backing sheet in co...
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WO/2011/051149 |
A storage compartment module having a mobile storage compartment comprises a housing (100) having a storage compartment receiving space, a storage compartment with lateral guide elements (231, 233) and optionally at least one passenger s...
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WO/2011/051149 |
A storage compartment module having a mobile storage compartment comprises a housing having a storage compartment receiving space, a storage compartment with lateral guide elements and optionally at least one passenger supply element, a ...
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WO/2011/051210 |
The invention relates to a fuel cell system having a device for drying gases, comprising at least one cooling body having at least one first surface and at least one removal device. The cooling body is designed to be thermally connected ...
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WO/2011/051501 |
A training simulation system for a drone system comprises a trainer station (10) having a first output means (101, 102, 103), which is equipped to generate and show at least one current exterior view of the drone, a second output means (...
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WO/2011/051308 |
The invention relates to a fastening arrangement (4, 72, 76, 84) for fastening components on a fuselage of an aircraft, comprising at least one base element (6), at least one mounting rail (8, 74, 78) and connecting elements (10), wherei...
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WO/2011/052822 |
The present invention relates to a portable unmanned airship for magnetic-force surveying and to a magnetic-force surveying system employing the same, comprising: a main airship body propelled under its own power using the buoyancy of a ...
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WO/2011/051778 |
A system for determining the relative and absolute blade angle settings of variable pitch wind turbine blades (12, 14, 16). The system uses a wire frame digital file and physical reference apparatus (15, 17, 19, 21) applied to the rotor ...
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WO/2011/051526 |
Aerial system for transmitting video and images via satellite in real time, composed of two main parts: the shipped part (30) which has sensors (1) and (2) for capturing video and images, an electronic switch (3), several coders (4), (5)...
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WO/2011/051699 |
There is provided an aerofoil comprising an inboard section, a tip section moveable between a flying configuration and a parked configuration, a hinge shaft mounted at a compound angle in the inboard section, a fixed gear mounted concent...
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WO/2011/051533 |
Control post that comprises: a seat (10) for the operator of said control post, the seat (10) comprising at least one armrest (30), and a control and command assembly, said assembly comprising a command lever (1) with controls, mechanica...
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WO/2011/051308 |
The invention relates to a fastening arrangement (4, 72, 76, 84) for fastening components on a fuselage of an aircraft, comprising at least one base element (6), at least one mounting rail (8, 74, 78) and connecting elements (10), wherei...
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WO/2011/051526 |
Aerial system for transmitting video and images via satellite in real time, composed of two main parts: the shipped part (30) which has sensors (1) and (2) for capturing video and images, an electronic switch (3), several coders (4), (5)...
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WO/2011/051533 |
Control post that comprises: a seat (10) for the operator of said control post, the seat (10) comprising at least one armrest (30), and a control and command assembly, said assembly comprising a command lever (1) with controls, mechanica...
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WO/2011/050594 |
A magnetic suspension electric rotor flying saucer comprises: a saucer shell (1), a saucer cabin (2), a rotor system (3), and a control system (4). The rotor wing system is a magnetic suspension electric rotor wing system (3) composed of...
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WO/2011/051697 |
A curable flexible electromagnetic hazard resistance laminate, comprising a layer of electrically conductive metal material and thermosetting resin, wherein an external face of the laminate comprises a releasable backing sheet in contact...
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WO/2011/051148 |
A storage compartment module having an integrated supply channel for optimized installation comprises a housing having a storage compartment receiving space and a passenger supply channel, a storage compartment with lateral guide element...
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WO/2011/048081 |
The present invention relates to a system for varying the angle of attack of the blades of an aircraft turbine engine propeller, including a brushless axial flow engine (10) comprising a stator (10a) provided with windings (12), as well ...
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WO/2011/048591 |
A system is provided for guarding a perimeter, including a control center, a launch system, a controller and a communication system. The control center is configured for generating a control signal responsive to receiving infiltration in...
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WO/2011/047998 |
The present invention relates to a control device (10) for a cabin of an aircraft or spacecraft, comprising a first control means (11) for actuating at least one camera (21-23) by means of at least one first control signal (51), set up f...
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WO/2011/048394 |
An aircraft landing gear assembly including a bogie beam, a landing gear strut (1) having a first end arranged to be pivotally coupled to an aircraft and a second end pivotally coupled to the bogie beam (3), and a stop (13) arranged to l...
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WO/2011/048064 |
An adjustable, or all -moving, horizontal stabiliser (4) for an aircraft, the stabiliser having a leading edge, a trailing edge, a root and a tip, and a strake (7) fixed with respect to the stabiliser (4) and attached to, or integrally f...
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WO/2011/047998 |
The present invention relates to a control device for a cabin of an aircraft or spacecraft, comprising a first control means for actuating at least one camera by means of at least one first control signal, set up for providing the first ...
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WO/2011/047864 |
The invention relates to a system (100) for storage in an aircraft galley (10) comprising a plurality of receiving devices (16) provided to be received in a main body (12) of the aircraft galley (10), wherein said receiving devices are e...
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