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WO/2012/135250 |
Describes are passenger seats including a seat pan (14) assembly with a reclining mechanism (60), a seat back (12) pivotally coupled to the aft end of the seat pan assembly, and a lumbar mechanism (18) coupled to the seat back (12) and/o...
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WO/2012/135371 |
An aircraft galley includes a beverage center including one or more hot beverage makers, and one or more combination oven-chiller units for multiple replaceable meal carrier rotables. The beverage center may also include an espresso make...
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WO/2012/130876 |
The present invention relates to a system comprising a check-in module (1) having a baggage drop-off panel (2) and a check-in execution panel (3), a first controller (4) associated with said check-in module, responsible for the operation...
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WO/2012/133066 |
An actuator monitoring system (1) is provided with: an electrical actuator (10) that is provided with an electrical motor (11); and a control device (20), which outputs to the electrical motor (11) a control command (CMD) that controls o...
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WO/2012/135245 |
Described are passenger seats having a seat back support and a head rest assembly coupled to the seat back support. The head rest assembly includes a head support and a lower head support with a rest bar and a pair of extensions, wherein...
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WO/2012/134945 |
Systems and methods for electromagnetic thrusting are disclosed. An electromagnetic thrusting system includes an axially-asymmetric resonant cavity including a conductive inner surface, the resonant cavity adapted to support a standing e...
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WO/2012/131101 |
The invention relates to an aircraft (11) comprising an enclosure and a system for surveilling areas of interest inside the enclosure. The enclosure includes a transverse aisle (13) and a longitudinal aisle (15) that intersect at an inte...
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WO/2012/135300 |
An aircraft having a cooling system is disclosed. The cooling system can he used to cool a heat emitting component In one form the cooling system is a refrigerant system and includes a relatively high temperature device such as, but not ...
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WO/2012/131105 |
The invention relates to an aircraft (11) comprising a system for observing part of the external environment of the aircraft. The environment observation system comprises a camera, known as a panoramic camera (21, 22, 23), including a st...
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WO/2012/130809 |
The seat according to the invention makes it possible to absorb, in the event of a frontal impact of an airplane, the rocking to which a passenger in a seat located behind the seat according to the invention is subjected. The backrest (2...
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WO/2012/132690 |
The present invention provides technology making it possible to reduce the cost of a spacecraft equipped with an on-board solar cell. The spacecraft is provided with a collector and a solar cell. The collector is disposed on the surface ...
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WO/2012/131233 |
The invention relates to a suspension device of a turbine engine casing, comprising a stepped shaft (26) that extends through aligned holes in two lugs (52, 54) of a clevis that is solidly connected to the casing. In addition, a wear-pro...
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WO/2012/135552 |
A wheel design is provided for an aircraft landing gear wheel that is configured to maximize the space available within a landing gear wheel well to support a motor driver assembly that drives the aircraft wheel when the aircraft is on t...
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WO/2012/134365 |
The present invention regards an aerial vehicle harpoon device for securing an aerial vehicle (31, 55) to a grid (9) of a landing site, the aerial vehicle (31, 55) comprises an undercarriage (11) having a supporting surface (13) for supp...
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WO/2012/131211 |
The present invention relates to a method for inspecting impacts (Ii) present on an internal face (104) of a fan casing (100), said method being characterized in that it comprises the following steps consisting in: - spotting (201) a fir...
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WO/2012/131209 |
The present invention relates to a seal assembly (300) for a turbojet nacelle comprising a first end (301) equipped with means for fastening to at least a first structure (100), and a second end (302) designed to come into contact agains...
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WO/2012/131271 |
The invention relates to a system (25), comprising: a linear actuator (26) axially arranged in the first propeller (9) and rotatably secured thereto, a first linking mechanism (27) connecting the rod of said linear actuator (26) to the s...
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WO/2012/130458 |
The present invention relates to an aircraft fuel cell system (1) comprising a fuel tank (2), a reactor (3) for generating hydrogen gas from a fuel, heating apparatus (4) and a fuel cell (5), wherein the reactor can process a synthetic f...
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WO/2012/131384 |
An aircraft seat arrangement comprises first and second seats (10, 20) and first and second consoles (12, 22), the first console (12) being in front of the first seat (10) and adjacent to the second seat (20), such that the first and sec...
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WO/2012/130856 |
The invention relates to a microscale radio-controlled aerial vehicle, having a fixed wing (as opposed to a rotary wing) comprising propulsion means (23, 24), said vehicle comprising a means for traveling on the ground, which are attache...
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WO/2012/131373 |
A method of and apparatus for operating a propeller (10), the propeller (10) moving through a fluid, the method comprising: measuring a value of a property of the fluid (e.g. a parameter related to the density of the fluid); measuring a ...
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WO/2012/132420 |
A high-lift device (3) for an aircraft comprises: a flap main body (11) provided at the trailing edge portion of the main wing (2) of the aircraft so as to be able to be expanded and housed and extending along the wing span direction of ...
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WO/2012/135117 |
An airship (25) is provided. The airship includes a hull (12) configured to contain a gas, at least one propulsion assembly (31) coupled to the hull and including a propulsion device (45), and at least one aerodynamic component (2000) in...
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WO/2012/129569 |
Restoration methods for effectively restoring the light transmission and optical clarity properties to polymeric aircraft windows or other high optical polymeric surfaces. The methods restore optical polymeric surfaces damaged by scratch...
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WO/2012/127038 |
The invention relates to a method for producing a structural component (6), which has at least two component parts (11, 12) connected to each other by means of a thermoplastic plastic material (13) and can be used in particular in the fi...
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WO/2012/129223 |
An aircraft wing (12) includes a wing structure (12a), a slat panel (16) mounted on a track (18), and an actuator mechanism (26) on the wing structure coupled to the track for moving the slat panel between a deployed position and a retra...
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WO/2012/129116 |
An in-flight entertainment (IFE) system that integrates a touch screen display device with a tray table (e.g., an airplane tray table or a train tray table) to provide a superior media experience for users in a highly efficient manner. T...
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WO/2012/128778 |
An aircraft engine generates engine power by burning hydrocarbon fuel such as Jet-A. A minute quantity of the fuel is burned in such a manner as to generate no engine power, and the heat generated by the burning fuel is used to protect r...
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WO/2012/127108 |
Flying device, in which there is a fuselage (2, 2'), wings (8, 9), which are connected to each other to form an essentially looped structure, means (4, 5) for creating a flying force, and the desired means (e.g., 7, 7') for controlling t...
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WO/2012/127038 |
The invention relates to a method for producing a structural component (6), which has at least two component parts (11, 12) connected to each other by means of a thermoplastic plastic material (13) and can be used in particular in the fi...
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WO/2012/129116 |
An in-flight entertainment (IFE) system that integrates a touch screen display device with a tray table (e.g., an airplane tray table or a train tray table) to provide a superior media experience for users in a highly efficient manner. T...
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WO/2012/128851 |
A method comprises removing space debris (110) having a relatively low ballistic coefficient by hastening orbital decay of the debris. A transient gaseous cloud (120) is created at an altitude of at least 100 km above Earth (E). The clou...
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WO/2012/129569 |
Restoration methods for effectively restoring the light transmission and optical clarity properties to polymeric aircraft windows or other high optical polymeric surfaces. The methods restore optical polymeric surfaces damaged by scratch...
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WO/2012/126953 |
A load introduction element (10) for a movable surface (2) of an aircraft comprises a load introduction body (12) that is connectable with the surface (2). A fitting (14) connected with the load introduction body (12) with a first sectio...
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WO/2012/126914 |
The invention essentially concerns an aircraft seat (1), comprising control units (17.2, 22.2, 27), at least one node (11-15) to execute a particular action or function, and a display (22.1) for viewing video data. Said node (11-15) and ...
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WO/2012/126731 |
The invention relates to an improved seat assembling method for assembling at least one seat (124) into an airplane (146), having the following steps: a) positioning a seat installing device (10) at a specified assembling position in the...
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WO/2012/125919 |
In a composite component having a laminate body, a conductive layer and a connector can be joined to one another using an intermediate flexible circuit. Among other things, this flexible circuit places the conductive layer and the connec...
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WO/2012/123681 |
Turbomachine with fan(s) for aircraft, with mobile jet nozzle. The turbomachine comprises at least one turbine (5) driving the rotation of the fan (3, 4), and a jet nozzle (8) coaxially extending said turbine and creating, with an outlet...
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WO/2012/125895 |
An aircraft engine includes a precooler disposed within a nacelle. The precooler defines an ambient air passage and a bleed air passage. Air passes through the precooler from an ambient air inlet to an ambient air outlet. Bleed air passe...
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WO/2012/125052 |
The invention pertains to aeronautical engineering and consists of an airborne platform that can be built to large sizes without requiring a rigid structure of comparable dimensions and which uses both buoyancy and the aerodynamic Magnus...
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WO/2012/125127 |
An invention concerns a method achieved to provide fully lying for seats groups of public transport vehicles in the space to be allocated for them and a seats group which uses this method.
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WO/2012/123757 |
The present invention provides a method and system of determining the ground-to-tyre friction coefficient for an aircraft landing event, the method comprising: providing a plurality of aircraft data parameters including aircraft vertical...
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WO/2012/123074 |
The invention relates to a flapping wing device comprising a main body (2), a drive device (3) and a flapping wing (4), wherein the flapping wing (4) comprises a first and a second wing portion (8, 9) and also an articulating device (42)...
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WO/2012/125233 |
The disclosure provides in one embodiment a method of insulating a structural frame member of a transport vehicle. The method comprises providing at least one flexible insulation member (118,166). The method further comprises providing a...
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WO/2012/123725 |
An aircraft assembly comprising a plurality of structural components (4) and an electrically conductive bonding network, wherein at least one of the structural components (4) is formed of material of low electrical conductivity, and the ...
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WO/2012/125597 |
A spacecraft reaction control system comprising: a spacecraft having a center of mass; a length of free tether extending from said spacecraft and offset from said spacecraft's center of mass, such that a force exerted upon said spacecraf...
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WO/2012/122925 |
An aircraft wingtip device, comprising a transition part (1) and a wingtip part (2); the inner end of the transition part (1) is connected to the far end of an aircraft wing, and the outer end of the transition part is connected to the w...
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WO/2012/123487 |
The invention relates to a control device (32) for controlling an actuator (26, 28, 30) for moving a mobile element (12, 16, 18) of a seat (10) in a vehicle. The control device comprises: a measuring device (38, 40) for determining a ref...
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WO/2012/125639 |
In one example, a long endurance airship system includes a payload airship and a first logistics airship mechanically joined to the payload airship to form a first combined airship, the payload airship and the logistics airship having de...
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WO/2012/125692 |
A seat mounting assembly ( 20 ) including a swingarm ( 32 ) configured for attachment to spaced-apart floor tracks, and a plinth ( 22 ) having a seat ( 24 ) mounted thereon mounted on the swingarm such that the swingarm is configured def...
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