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Matches 201 - 250 out of 6,069

Document Document Title
WO/2013/079583A1
Provided in a method for landing an airship (20) on a landing device (22) placed on the ground (3) are the following method steps: alignment, in particular horizontal alignment of the airship (20) relative to the landing device (22) with...  
WO/2013/081538A1
Passenger bridge for airports and ships, comprising one or several walking tunnels (1,2) for passengers, where, in case the passenger bridge comprises two or more walking tunnels, these are arranged to be telescopic relative one another....  
WO/2013/077742A1
Anchoring device (1) in a helicopter deck (2), where a housing (11) that is provided with an open top (111) and lowered into the helicopter deck (2), contains a fastener (12) which is vertically displaceable between a withdrawn, inactive...  
WO/2013/075180A2  
WO/2013/076349A1
The present invention improves the efficiency of the loading cell while maintaining and improving the flexibility of the baggage handling system of an airport such that bags may be received early with minimal labor-intensityby virtue of ...  
WO/2013/075731A1
The invention pertains to a de-icer for airplanes, which comprises a self-propelled vehicle (32) which is provided with a lifting device (34, 36) for lifting and positioning a spraying nozzle (38) in the vicinity of an outer surface of a...  
WO/2013/076633A1
Method for manufacturing a support pylon for avionics made of composite materials, adapted to allow the transport of external loads that cannot be directly supported at the primary or secondary structure of the aircraft. Said loads are r...  
WO/2013/076708A1
A test apparatus for avionic sensors including a helicopter (2), an avionic sensor test pod (3) equipped with at least one avionic sensor (18, 20) and a cable suspension system (4) connecting the test pod (3) to the helicopter (2).  
WO/2013/077223A1
The purpose of the present invention is to provide a very versatile cargo carrying vehicle capable of smooth cargo carrying processing by fine-tuning the position of and the length between a pair of right and left guide rails on a platfo...  
WO/2013/068575A2
The invention relates to a cleaning machine for windows (F) façade elements, solar modules, and smooth-surfaced surface elements of that kind, in particular at great height, which cleaning machine enables quick and efficient cleaning in...  
WO/2013/068575A3
The invention relates to a cleaning machine for windows (F) façade elements, solar modules, and smooth-surfaced surface elements of that kind, in particular at great height, which cleaning machine enables quick and efficient cleaning in...  
WO/2013/070102A3
The invention solves a problem of a carriage (1) assembly for an airplane transporting system on an airport apron, from a parking location to a runway and from a landing to the parking location with an airplane's engine off. The carriage...  
WO/2013/068496A1
The invention relates to an anchoring harpoon that includes a bistable actuator (34) comprising a rod (56) for actuating the finger (32) that is movable between a retracted rest position and an extended deployment position of the finger ...  
WO/2013/056806A1
The invention relates to an operating method for a positioning system 1, in particular for the structural assembly of aircraft. The positioning system 1 comprises multiple positioners 2a, 2b, 2c, each of which has at least one manipulato...  
WO/2013/057706A1
The application provides a multi-storey storage device. The device includes an upper storey and a motor with a torsional supporting structure. The upper storey includes a rotatable upper disc, a plurality of supporting elements, and an u...  
WO/2013/053047A3
Herein is disclosed a multifunctional tool with replaceable tool tips. The disclosed multifunctional tool may be used as an end-effector on a robotic arm in space. Each tool tip, when in the tool holder, is driven by a common motor. The ...  
WO/2013/053632A1
A method for driving a LED-airfield light by a controller 18, being at least connected two LED-modules 20, 30, wherein the LED-modules 20, 30 each comprise a memory 28, 38, permits to drive the LEDs at equal luminosity if the method comp...  
WO/2013/055265A1
The present invention relates to a system and method for automatic launch and landing UAVs (Unmanned Aerial Vehicles). The system comprises a ground station adapted for automatic UAV launching and landing. The ground station comprises: m...  
WO/2013/055227A1
A device for a helicopter deck (1) comprising a supporting, fluid-tight floor (3) is described, the helicopter deck (1) comprising an overlying, draining top cover (2) formed out of at least two top-cover sections (20) arranged side by s...  
WO/2013/053633A1
A light for airfield lighting comprising at least a housing having at least one light exit for light emitted by at least one LED, at least one heating element for heating at least the light exit, and a controlling unit configured for bei...  
WO/2013/052193A1
A peel-resistant mechanism includes a body (130) and a plurality of arms (140) extending from the body (130) such that a recess is defined between each pair of adjacent arms (140). At least one of the arms (140) is positionable to facili...  
WO/2013/050839A1
The seal comprises a bellows (1) arranged on a passing platform (2), with a proximal end connected to a gantry frame (3) and a distal end connected to a flexible frame (4) provided for resting on an outer surface of said aircraft when th...  
WO/2013/050444A1
The invention relates to a method for optimizing the tolerancing of a set of flexible parts, said parts being particularly subjected to forces. The method that is the subject of the invention enables the definition, at the design phase, ...  
WO/2013/050850A1
The invention relates to a method for transporting containers (30), in which a group of containers comprises a sub-group M assigned to the transportation of goods and a sub-group V assigned to the transportation of a vehicle (10) that ca...  
WO/2013/047038A1
An airplane design device performs a repetitive process whereby the following operations are repeated: airframe specifications, which are the specifications for the airplane, are calculated on the basis of multiple design variables neces...  
WO/2013/049516A1
A method for repairing an aircraft component (100) includes removing a portion of the aircraft component (100) to create an opening (106) within the aircraft component (100). The method also includes creating a patch (102), inserting the...  
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...  

Matches 201 - 250 out of 6,069