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WO/2013/033585 |
A console for aircraft that is located between two seats which face each other. The console includes an open ledge with a cup holder arrangement. The cup holder arrangement includes two removable holder dividers which can be flipped up o...
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WO/2013/029591 |
The invention relates to a lifting apparatus (16) for an aircraft (1), comprising: at least one cushion (19) which can be blown up and has at least two chambers (20, 21); at least one compressor; and at least one pressure control device,...
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WO/2013/030489 |
The invention relates to a rotary- or fixed-wing aircraft comprising one or more rotors and/or one or more propellers, in which the rotor(s) and/or propeller(s) are rotated at a variable or constant speed by at least one shaft and the ai...
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WO/2013/032369 |
The technical problem solved by the claimed solutions of an aircraft fuselage compartment joint assembly and the pressure bulkhead thereof is the design of low-mass constructions in conjunction with increased service life of the joint as...
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WO/2013/032078 |
The present invention relates to a method and system for unmanned airborne collection and transmission of information during flight, and to technology for performing an unmanned flight using an air-collecting body, descending from a pred...
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WO/2013/032369 |
The technical problem solved by the claimed solutions of an aircraft fuselage compartment joint assembly and the pressure bulkhead thereof is the design of low-mass constructions in conjunction with increased service life of the joint as...
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WO/2013/030498 |
In an assembly comprising a dual-flow turbine engine and a system for attaching the turbine engine to an aircraft structure, the attachment system includes a pylon, at least two rear fasteners connecting the pylon to two rear attachment ...
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WO/2013/030527 |
The present invention provides an aircraft structure comprising a structural component (130, 230) and a set of reinforcing straps (140, 240) for reinforcing the structural component, wherein the set comprises a first reinforcing strap (1...
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WO/2013/030030 |
The invention relates to an anti-lofting deflector for landing gear bearing two wheels on an axle, and comprising: - a fixed support (5) intended in service to be fixed on a part of the landing gear bearing the axle so that it extends be...
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WO/2013/030797 |
Embodiments of the invention provide premium seats for aircraft and other passenger transport vehicles that provide extra seat room by providing an improved tray table configuration, which also enhances privacy for each passenger. Certai...
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WO/2013/032490 |
A method and apparatus comprising a first wall (122) and a plurality of longitudinal members (120). The first wall is for an inlet (110) of an aircraft engine (108). The plurality of longitudinal members connects the first wall to a stru...
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WO/2013/027032 |
An aircraft landing gear (10) comprising: a strut (12) having an upper portion (12a) arranged to be mechanically coupled to an aircraft and a lower portion (12b) movably mounted with respect to the upper portion; a bogie beam (14) pivota...
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WO/2013/027388 |
The purpose of the present invention is to provide a moving blade such as a slat capable of maintaining and fulfilling a minimum necessary function even when suffering damage due to a collision with a bird or the like, and a wing using t...
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WO/2013/026582 |
The invention relates to a device for the multi-axis adjustment of a plurality of elements relative to each other, wherein the elements can be rotated against each other via open-center large diameter anti-friction bearings having differ...
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WO/2013/026746 |
A kite for a system for extracting energy from the wind, the kite comprising: a body having a wing for providing lift; means for connecting the wing to a tether; and means for controlling the flight of the kite in the wind, wherein the w...
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WO/2013/026975 |
The present invention relates to a locking device (10) comprising a locking pair (11) comprising a bolt (112) capable of engaging with a retaining means (111), the bolt being movably mounted against an elastic return means (113) that ten...
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WO/2013/026963 |
The invention relates to a helicopter rotor system and to a helicopter including such a rotor system. Said rotor system has a rotor shaft (8) extending along a main axis, a rotor head (4) for supporting variable-pitch blades (6), the rot...
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WO/2013/023771 |
Water disinfection system comprising a water disinfection device (10), having a UV light generator (13, 14) for the UV treatment of water, and a water pipe (82, 81), having a first pipe portion (81) and a second pipe portion (82) and a t...
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WO/2013/023649 |
The invention relates to a device for conditioning of cabin air from a cabin space of an aircraft that has at least one lithium air battery (106), having a first feed line (101) by means of which ambient air can be delivered to the batte...
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WO/2013/025133 |
The invention aims at pressurising a volume (2) that needs to have a relative air pressure, in comparison with an ambient pressure, where the ambient air pressure can change rapidly and with large amplitude and where the access to pressu...
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WO/2013/025877 |
An aircraft interior panel (10) for supporting high-weight loads including a core panel (14) sandwiched between structural plies (16), a panel insert (12) embedded in the panel (10) and passing through and interrupting the core panel (14...
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WO/2013/025971 |
An aircraft interior door assembly (10), such as for a lavatory, including a door panel (12) configured to simultaneously pivot and translate within its opening, a first pair of linear door guides (14, 14') running parallel to the door o...
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WO/2013/024405 |
A method of delivering over the air, shelled portions (110) of fluids or granular substances (120) containing effective ingredients, to a target, is provided herein. The method includes the following stages: selecting (630) a type and a ...
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WO/2013/020803 |
A pressure supply system (1) for a fresh water system of an aircraft, comprising a water reservoir (10) having a bleed air inlet (11) and a water outlet (12), and comprising a water pump (30) so as to load water, which is loaded with ble...
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WO/2013/021141 |
The invention relates to a method for producing a protective reinforcement (30) of the leading edge (16) of a vane (12), in which the reinforcement (30) is produced by depositing a metallic coating by thermal spraying under compression o...
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WO/2013/020955 |
The invention relates to a method for manufacturing a rocker arm for the landing gear of an aircraft, including a body that is provided with a double yoke (24) comprising two flanges (19, 21) arranged parallel to a radial direction with ...
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WO/2013/022368 |
1. The utility model relates to air and water transport and can be used for producing propellers for propelling vehicles in continuous fluid media. 2. The technical result of the proposed utility model consists in an increase in reliabil...
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WO/2013/023123 |
An aircraft with a control system having joint control for a throttle and a propeller of an aircraft may be modified to decouple the joint control of a throttle and a propeller. Control of the throttle and propeller may be independent of...
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WO/2013/022414 |
A spacecraft defends an object in space against space junk, by altering the trajectory of the space junk, away from the threatened object, using one or more of the following methods: 1) magnetic, 2) vaporization, 3) physical fusion, or 4...
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WO/2013/020708 |
The invention relates to a service module (10) for supplying passengers in a passenger space of a means of transport, in particular of an aircraft, and to a service system having a service channel and a plurality of such service modules ...
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WO/2013/021127 |
Hydraulic control system for controlling the orientation of fan blades of a turbomachine comprising at least one set of variable-pitch fan blades operated by actuators (10, 12) connected to a hydraulic pump (18), a small pitches protecti...
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WO/2013/022955 |
A flight-operable, truly modular aircraft has an aircraft core to which one or more of outer wings members, fuselage, cockpit, leading and trailing edge couplings, and empennage and tail sections can be removably coupled and/or replaced ...
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WO/2013/022970 |
An aircraft wing is equipped with asymmetric wing folding hinges to achieve a highly compact folded footprint. One or more of the hinges is advantageously placed at angle with respect to an aircraft centerplane such that the wing tips ca...
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WO/2013/019301 |
Holonomic-motion ground vehicles (i.e., mobile platforms) that are ca- pable of controlled movement across non-level surfaces, while car- rying one or more nondestructive inspection sensors or other tools. The mobile platform comprises a...
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WO/2013/019898 |
Embodiments of the invention relate to systems and methods for casting hybrid rocket motor fuel grains. In one embodiment, a method for casting a rocket motor fuel grain can be provided. The method can include providing a positive image ...
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WO/2013/017680 |
The object of the invention is a drive system of at least one rotor of an aircraft via electrical energy in addition to or as a replacement of a mechanical system, characterised in that the electrical energy is provided at least in part ...
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WO/2013/019213 |
A skid landing gear assembly is provided. One embodiment of the landing gear assembly may include a first and a second skid member, and a forward and an aft cross member. The forward and aft cross-members may have integrated attachment m...
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WO/2013/019210 |
An unmanned aircraft system has an airframe and a payload pod detachably secured to the unmanned aircraft system under the airframe and a nacelle attached atop the airframe. The UAS is payload agnostic and provides the platform to which ...
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WO/2013/017506 |
A storage compartment for a passenger cabin of an aircraft comprises a storage compartment body (100), a mounting (500), a fixing brace (310, 320)and a pull rod (450, 480). The fixing brace (310, 320) is connected to a frame of the prima...
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WO/2013/017759 |
The present invention relates to a longitudinal beam (500) for a turbojet engine nacelle support structure, said beam being made mainly of composite material and being substantially L-shaped comprising, on the one hand, at least one long...
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WO/2013/017290 |
An aircraft monument (10) for installation in an aircraft cabin comprises a sanitary module (12) having a sanitary fitment (16), and a galley module (14) arranged adjacent to the sanitary module (12). The galley module (14) comprises a t...
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WO/2013/019539 |
An apparatus for moving parked aircraft with an omni-directional tractor via an aircraft lift dolly that is revolvably coupled thereto which includes a hinged gate to entrap the aircraft nose gear. The aircraft lift dolly may be removabl...
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WO/2013/016788 |
The invention relates to an inflatable aerodynamic garment, a winged aircraft propelled by human muscle power and designed as a garment made of flexible materials and filled with gases lighter than air. The invention comprises inflatable...
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WO/2013/017759 |
The present invention relates to a longitudinal beam (500) for a turbojet engine nacelle support structure, said beam being made mainly of composite material and being substantially L-shaped comprising, on the one hand, at least one long...
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WO/2013/017789 |
The invention relates to a device (210) for supplying an aircraft on the ground with electricity, comprising two electric generators (216, 218) driven by an auxiliary power unit (220), characterized in that the first generator is connect...
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WO/2013/017854 |
A method for in-situ cleaning of compressor blades in a gas turbine engine on an aircraft comprises the following sequential steps: Step 1 - washing said compressor blades by spraying a first liquid composition into the engine; and Step ...
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WO/2013/015295 |
The purpose of the present invention is to provide a vertical takeoff and landing aircraft which takes off and lands vertically with the plane of rotation of a rotor facing to the lower side of a main wing and moves forward with the plan...
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WO/2013/015720 |
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WO/2013/016173 |
An aerial refueling system utilizes the full drogue-probe coupling event as a control parameter for hose control. A variety of different types of signal sending and signal receiving devices may be used to indicate a coupling event betwee...
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WO/2013/016173 |
An aerial refueling system utilizes the full drogue-probe coupling event as a control parameter for hose control. A variety of different types of signal sending and signal receiving devices may be used to indicate a coupling event betwee...
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