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Patent Searching and Data


Matches 201 - 250 out of 5,938

Document Document Title
WO/2013/043974A3
An airplane ground support system includes a multi-voltage power supply (20). This system includes an air conditioning module, a control module (22), and a power supply module which has an A.C. power input, at least one power output, wit...  
WO/2013/042114A1
An airplane transfer system (740) for transferring an airplane (700) comprising an airplane control component (707, 709) and an electric control system (704) configured to generate one or more transfer signals responsive to one or more c...  
WO/2013/041099A1
An example of an aim with the disclosed method and system may be seen to provide a method and system which does not require more square meters of footprint than existing solutions or even requires less square meters of footprint, while s...  
WO/2013/039409A1
The present invention relates to an apparatus for moving a large stationery object, the apparatus including a chassis, wherein the chassis is provided with a plurality of ground engaging wheels, and a motor, wherein the motor drives at l...  
WO/2013/038091A1
The invention relates to a method and system for monitoring a measurement chain (3) designed to collect measurements over time regarding an aircraft turbojet engine (13), said system comprising processing means (21) configured to constru...  
WO/2013/039946A1
An air delivery hose assembly (10) for use with aircraft ground support equipment (12) provides conditioned air to an on-ground aircraft (14). The hose assembly (10) includes an impermeable inner liner (22) which forms an air conduit, a ...  
WO/2013/037921A1
The present invention relates to a mobile device for measuring photometric characteristics of airport runway lights, including a measuring rod to be moved over runway lights to be checked in the light beams emitted by said lights, and a ...  
WO/2013/034054A1
An assisted takeoff system for an aircraft, comprising a slope slideway (3) and a sliding carrier (4), wherein one end of the slideway is smoothly connected to a horizontal track (1) and the other end thereof is fixed to the island (2) o...  
WO/2013/029591A1
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,...  
WO/2013/030527A1
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...  
WO/2013/024256A3
Embodiments of the present invention provide a method of manufacturing a complex aircraft landing gear (2) component having a plurality of sub-components (4, 4a, 6, 6a), the method comprising forming first (4, 4a) and second (6, 6a) sub-...  
WO/2013/019301A1
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...  
WO/2013/019539A1
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...  
WO/2013/017854A1
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 ...  
WO/2013/014225A3
Pipe treatment system (1) for a supply unit, the pipe treatment system (1) comprising a fresh water inlet pipe (10), a tap for fresh water (40, 41, 42), a controllable tap valve (30, 31, 32), and a control device for the pipe treatment c...  
WO/2013/013219A1
A vehicle, especially a maritime vessel, is provided with an autogyro drawn by a tether. The tether contains mechanical strengthening components that enable it to securely retain the autogyro to the vehicle. The tether also contains two ...  
WO/2013/011412A1
An apparatus for launching a remotely piloted aircraft (50) from a submarine (100) comprises a tubular body (2) insertable into a mast (103) of the submarine (100), extending along a respective principal direction (C) and defining an eje...  
WO/2013/012321A1
The invention provides a conveying system for pieces of luggage, which may or may not form part of a check-in system. The conveying system comprises a conveyor for conveying pieces of luggage, detection means provided with a camera for m...  
WO/2013/009906A3
A method comprises using a computer to access an engineering definition of a composite part and to apply a set of rules governing material laydown prior to performing the laydown.  
WO/2013/009907A3
A method for creating a layup of reinforcing fibers comprises mounting a face sheet to a spindle of a mandrel tool support, the face sheet having a layup surface for the reinforcing fibers, and counterbalancing the mounted face sheet for...  
WO/2013/007805A1
The invention relates to an intermediate structure for retaining systems intended to be installed on board an aircraft, comprising a plurality of independent modules (M1 - M6) secured separately to a primary structure of a section of air...  
WO/2012/176132A1
The invention relates to a fluid supply bench (1), for example for an aircraft undergoing maintenance, said bench including: a fluid circuit (10) comprising a variable-displacement, constant-pressure pump (12), said circuit (10) being in...  
WO/2012/176223A1
A hooking member (1) for favouring landing of an aircraft on a access surface (G) comprising a support group (2) which protrudes from the support pads (P) of the aircraft to which is firmly coupled, a grip assembly (3), coupled to the su...  
WO/2012/173632A1
The self-sustaining drone aircraft freight and observation system (5) comprises a fleet of jet-powered drone aircraft (10) designed to carry freight (12) only. The drones (10) operate from a separate airfield in outlying areas to decreas...  
WO/2012/172320A1
The invention provides a computer-implemented method and corresponding system for conducting an inspection of an aircraft component, such as an aircraft engine. Reference data relating to the component is stored electronically in a datab...  
WO/2012/171105A1
The test cell comprises a test cell chamber comprising an air intake opening for allowing air to be fed into the test cell chamber. An aircraft engine test stand is mounted within the test cell chamber with the aircraft engine to be test...  
WO/2012/168518A1
The object of the invention is to achieve a universal module that can be fitted to any type of hose, and specifically to the various installations currently used, without making modifications thereto, and which is applicable not only to ...  
WO/2012/170672A1
According to various embodiments, apparatuses and methods for providing a control system for aircraft refueling trucks is provided. The control system is configured for facilitating remote troubleshooting of one or more safety mechanisms...  
WO/2012/165887A3
The present invention pertains to a technique for supplying power to an object in midair, and more specifically, to a ground-level power supply system for a small unmanned aerial robot to continuously supply power as a power source for t...  
WO/2012/165887A2
The present invention pertains to a technique for supplying power to an object in midair, and more specifically, to a ground-level power supply system for a small unmanned aerial robot to continuously supply power as a power source for t...  
WO/2012/155873A1
A movable access or loading device (1) for an aircraft (2) with a scanner (10) arranged on the access or loading device, wherein the position of the aircraft (2) relative to the axis or loading device (1) is determined by the scanner (10...  
WO/2012/156634A1
The invention relates to an air transport apparatus including: pieces of luggage (110, 120, 130, 140), a storage assembly comprising a storage frame (74, 76) and luggage containers (10) that can be inserted into said storage frame, said ...  
WO/2012/153731A1
In the present invention the following are provided: an actuator (81) provided between piping (33) and branch pipes (34) and having a cylinder (83), a piston (84), a rod (85), and a link mechanism (82) linked to the rod (85). When cleani...  
WO/2012/154093A1
A vehicle with a self-supporting chassis (1), which is cast of composite material(2) such as concrete or a comparable material, and being provided with an arrangement(3) for engine and wheels, for towing of aircraft, cargo and for indust...  
WO/2012/149292A3
An apparatus for facilitating fluid bladder removal from a support structure through an access opening includes a frame defining a central opening dimensioned to conform to the access opening, the frame having opposed first and second su...  
WO/2012/149379A2
A method of forming a composite structure (50) can include providing a plurality of composite panels (10) of material, each composite panel (10) having a plurality of holes (26) extending through the panel. An adhesive layer (30) is appl...  
WO/2012/149292A2
An apparatus for facilitating fluid bladder removal from a support structure through an access opening includes a frame defining a central opening dimensioned to conform to the access opening, the frame having opposed first and second su...  
WO/2012/149379A3
A method of forming a composite structure (50) can include providing a plurality of composite panels (10) of material, each composite panel (10) having a plurality of holes (26) extending through the panel. An adhesive layer (30) is appl...  
WO/2012/147823A1
In this method for fastening a composite material component, the first smoothness is measured of a first fastening component disposed in a first countersink-provided hole formed in a first article to be fastened as a plurality of stacked...  
WO/2012/145124A3
A tow vehicle for aircraft comprises a nose gear support assembly that can be raised and lowered relative to the vehicle about a first pivot axis. The support assembly can comprise a base portion and nose gear support portion pivotal abo...  
WO/2012/140247A1
A system for providing pre-conditioned air to an aircraft on the ground comprises: A ground air conditioning unit (30) configured to produce pre-conditioned air; a control module (46) controlling operation of said air conditioning unit (...  
WO/2012/141673A1
Ground-accessing elevator systems and methods are provided for transporting personnel between the ground level and one or more decks of multi-level vehicle such as a fixed-wing aircraft. The vehicle elevator systems and methods may be im...  
WO/2012/139185A2
The present invention relates to a case for packaging and transporting an aircraft brake assembly which comprises two separable pieces which accommodate the brake assembly in its interior, the pieces being assembled to one another by mea...  
WO/2012/139186A1
The present invention relates to a hubcap for protection and transportation of an aircraft wheel/tire assembly comprising a pair of circular parts fixed respectively on each side of the wheel/tire assembly by means of a through-bolt system.  
WO/2012/139185A4
The present invention relates to a case for packaging and transporting an aircraft brake assembly which comprises two separable pieces which accommodate the brake assembly in its interior, the pieces being assembled to one another by mea...  
WO/2012/141770A2
Aircraft configured to operate at Mach numbers from above.80 and up to 1.2 with wing sweep angles defined by the wing outboard leading edge of less than 35 degrees, and incorporating calculated values of the ratio of outboard wing panel ...  
WO/2012/139185A3
The present invention relates to a case for packaging and transporting an aircraft brake assembly which comprises two separable pieces which accommodate the brake assembly in its interior, the pieces being assembled to one another by mea...  
WO/2012/133440A1
In order to increase the safety and work efficiency of a worker loading and unloading cargos into and from a cargo compartment using a belt loader vehicle and to increase the loading capacity of the cargo compartment while ensuring that ...  
WO/2012/132773A1
The purpose is to make it possible to easily perform thin-wall machining such as pocket-forming on the curved inner-surface side of a curved, thin, plate-shaped workpiece, using a simple and inexpensive configuration, and to improve prod...  
WO/2012/130876A1
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...  

Matches 201 - 250 out of 5,938