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Patent Searching and Data


Matches 551 - 600 out of 6,061

Document Document Title
WO/2010/046605A3
The invention relates to a method for controlling at least one appliance (12) for moving aircrafts (10): at least one appliance (12) connected to an aircraft is driven to a position (80) that is closer to an entry corridor (74) of a take...  
WO/2010/046603A2
The invention relates to a method according to which an aircraft (10) is moved along the ground by means of at least two separate appliances (12) connected to the aircraft independently from each other or other appliances. A control elem...  
WO/2010/043815A1
The invention relates to a system for guiding a drone during the approach phase to a platform, in particular a naval platform, with a view to landing same, characterised in that the platform is provided with equipment indicating the angl...  
WO/2010/037964A2
The invention relates to a panel assembly for an aircraft fuselage, in which a first panel (10) and a second panel (20) respectively have a first end portion (11) and a second end portion (21) overlapping one another and connected to one...  
WO/2010/031591A2
The invention relates to a method for covering light aircraft and/or parts thereof with a polyester covering fabric, and to a dispersion hot-melt adhesive and to the use thereof for covering. The invention further relates to a light airc...  
WO/2010/031241A1
A cold-launch method and apparatus are provided. The present invention follows the formula of “accumulated energy quick releasing + effective transmission = launching movement”. A gas-liquid combined cylinder (1) is used as the catap...  
WO/2010/031384A2
The method for launching a drone (10) is carried out by means of a launch catapult (9) which applies the launch energy, such that the launch catapult (9) is first of all aligned, before launch. In this case, the launch catapult (9) is co...  
WO/2010/031384A3
The method for launching a drone (10) is carried out by means of a launch catapult (9) which applies the launch energy, such that the launch catapult (9) is first of all aligned, before launch. In this case, the launch catapult (9) is co...  
WO/2010/031591A3
The invention relates to a method for covering light aircraft and/or parts thereof with a polyester covering fabric (17, 18, 19, 29), and to a dispersion hot-melt adhesive and to the use thereof for covering. The invention further relate...  
WO/2010/028360A1
A method for analyzing tolerances for features for an object. A framework may be created from the plurality of features for the object. The framework may be fitted to a plurality of manufactured features for the object based on the plura...  
WO/2010/025910A1
The invention relates to a method for measuring the interior of an elongated body (1, 2), which has a longitudinal axis x in a global xyz coordinate system, a laser profile scan being carried out, during which a laser scanner (6) carryin...  
WO/2010/023371A1
The invention relates to a method for steadying an aircraft using jack props (1), in which: - the number and location of the props to be used is determined as a function of the area of operation, on the basis of a prop map, - strain gaug...  
WO/2010/025376A1
A large scale composite structure is fabricated by forming a plurality of composite laminate modules (208d, 208e) and joining the modules together along their edges (210) using scarf joints.  
WO/2010/020049A1
This invention concerns an aircraft cargo loader for lifting cargo and freight onto and off an aircraft or plane by the loader comprises a longitudinal deck platform; a supporting assembly extending under the platform for supporting and ...  
WO/2010/020050A1
This invention concerns an aircraft cargo loader comprising a deck platform; a front and a rear wheel assembly units; and a scissor assembly extending under the platform for supporting it and move it between an open and close position. T...  
WO/2010/020751A3
A visual aid for the pilot of an aircraft approaching to land on an aircraft carrier comprises a series of lights (9) embedded along the landing deck and controlled in response to pitch and heave of the vessel so that the light(s) illumi...  
WO/2010/020751A2
A visual aid for the pilot of an aircraft approaching to land on an aircraft carrier comprises a series of lights (9) embedded along the landing deck and controlled in response to pitch and heave of the vessel so that the light(s) illumi...  
WO/2010/018292A1
Protection for elements (1) made from composite material that are protected where the geometry thereof is complex, e.g. borders, ridges, edges and corners, against electrical discharges to which those elements are potentially exposed, sa...  
WO/2010/018090A2
According to one exemplary embodiment of the invention, preassembly and integration of a part of an aircraft cabin are carried out outside the aircraft structure with the aid of an assembly apparatus. After the preassembly, the part of t...  
WO/2010/018090A4
According to one exemplary embodiment of the invention, preassembly and integration of a part (2, 3) of an aircraft cabin are carried out outside the aircraft structure (7) with the aid of an assembly apparatus (8). After the preassembly...  
WO/2010/018090A3
According to one exemplary embodiment of the invention, preassembly and integration of a part (2, 3) of an aircraft cabin are carried out outside the aircraft structure (7) with the aid of an assembly apparatus (8). After the preassembly...  
WO/2010/012261A2
The invention relates to an automatic system for manoeuvring aircraft on the ground, based on driverless towing vehicles, (hereafter AGTV's), which can independently hold the undercarriage of the aircraft. In said system the AGTVs pull t...  
WO/2010/012261A4
The invention relates to an automatic system (1) for manoeuvring aircraft (2) on the ground, based on driverless towing vehicles, (hereafter AGTV's) (1), which can independently hold the undercarriage of the aircraft (2). In said system ...  
WO/2010/012261A3
The invention relates to an automatic system (1) for manoeuvring aircraft (2) on the ground, based on driverless towing vehicles, (hereafter AGTV's) (1), which can independently hold the undercarriage of the aircraft (2). In said system ...  
WO/2010/014333A1
A method and apparatus are used to fit a metallic or composite doubler on an uneven surface. A three dimensional digital map of the gap between the doubler and the uneven surface is generated by digitally scanning the uneven surface. The...  
WO/2010/010382A2
A method of stiffening a rib during the assembly of an aircraft wing is described. A stiffener panel is attached to a face of the rib. The rib is aligned with one or more wing components with the stiffener panel attached. An assembly ope...  
WO/2010/010279A1
The invention relates to a harpoon head (6) for a system for anchoring an aircraft on a grating (4) and is characterized in that a distal end of the harpoon head has an interchangeable insert (20).  
WO/2010/011783A3
The invention disclosed and claimed herein relates to treatment of water contaminated with glycol to be recycled for further effective use of the cleaned water resulting therefrom, especially at airports. More specifically, this inventio...  
WO/2010/010382A3
A method of stiffening a rib (19, 20) during the assembly of an aircraft wing is described. A stiffener panel (40, 41) is attached to a face of the rib (19, 20). The rib is aligned with one or more wing components with the stiffener pane...  
WO/2010/009899A3
The invention relates to a loading system for loading a cargo hold (2) of an aircraft (1), containers, pallets or the like ULDs (20) for accommodating freight being introduced into the cargo hold through an access opening, being transpor...  
WO/2010/009899A2
The invention relates to a loading system for loading a cargo hold of an aircraft, containers, pallets or the like ULDs for accommodating freight being introduced into the cargo hold through an access opening, being transported by means ...  
WO/2010/008323A1
The invention relates to a laser beacon for a landing glide slope system and a laser emitter for said laser beacon. Moreover said laser emitter may be used separately. The inventive laser beacon is characterised by the block-modular desi...  
WO/2010/006946A1
The invention relates to a device (20) and a method for avoiding ice-buildup on a surface area (22) of an aircraft (10) and/or for de-icing the surface area (22). In the process, a laser (1) is used, said laser being adapted to emit onto...  
WO/2010/004172A2
A section of aircraft fuselage comprises a cockpit structure (2) and a floor (4) connected to said cockpit structure. The cockpit structure (2) has an external skin (21) and a framework (22) comprising frames (23) positioned in fuselage ...  
WO/2010/003818A3
The invention relates to a method for installing an especially dome-shaped pressure bulkhead 5,25 on a one-piece, substantially conical rear section 1,13,18 of an aircraft, wherein said rear section comprises a connection area 3,35 and a...  
WO/2010/003686A1
A sealant made of expanded polytetrafluoroethylene having a coating of an active hydraulic fluid repellent component and an indicator, the sealant having a first uncompressed state and a second compressed state, wherein the sealant is re...  
WO/2010/003818A2
The invention relates to a method for installing an especially dome-shaped pressure bulkhead 5,25 on a one-piece, substantially conical rear section 1,13,18 of an aircraft, wherein said rear section comprises a connection area 3,35 and a...  
WO/2010/003640A3
A system (10) for cooling an aircraft zone comprises an air-conditioning unit (12a, 12b) for supplying cool air, a device (20a, 20b) conducting circulating air, and a mixing chamber (18) which is connected to the air-conditioning unit (1...  
WO/2010/001009A2
The subject of the invention is an aircraft nacelle comprising an air intake (40) able to channel an airstream (42) towards a drive unit (44), the said air intake (40) comprising an interior duct (48) forming an aerodynamic surface (52) ...  
WO/2010/001009A3
The subject of the invention is an aircraft nacelle comprising an air intake (40) able to channel an airstream (42) towards a drive unit (44), the said air intake (40) comprising an interior duct (48) forming an aerodynamic surface (52) ...  
WO/2010/003051A1
Air filtration devices and systems are provided to filter conditioned air after air exits an air conditioner module located on a ground support equipment unit but prior to entering a grounded aircraft. Disclosed embodiments include a sys...  
WO/2010/000575A1
The invention relates to an attachment support (1) for temporarily installing equipment (13) on a wheel (8) of an aircraft or of a vehicle, characterized in that it comprises: - two bearing elements (2) connected by a spindle (4) forming...  
WO/2009/156637A2
The invention relates to a method for assembling two structural elements, at least one of the two being tube-shaped and including a skin made of a fiber-reinforced composite material. The ability of said element to adapt to the shape and...  
WO/2009/156140A4
An auxiliary cooling device (100) is designed to be operated outside an aircraft (2) and comprises a source of cold adapted to cool a refrigerant to a desired low temperature, an auxiliary cooling device outlet (104), connected to the so...  
WO/2009/156140A3
An auxiliary cooling device (100) is designed to be operated outside an aircraft (2) and comprises a source of cold adapted to cool a refrigerant to a desired low temperature, an auxiliary cooling device outlet (104), connected to the so...  
WO/2009/156140A2
An auxiliary cooling device (100) is designed to be operated outside an aircraft (2) and comprises a source of cold adapted to cool a refrigerant to a desired low temperature, an auxiliary cooling device outlet (104), connected to the so...  
WO/2009/149491A1
A device (10) for arranging a plurality of individuals into a desired order. The device includes a floor plan (14) having a plurality of separately identifiable markings (16) thereon indicating an intended location for each individual on...  
WO/2009/151423A1
This invention provides an improvement in a no-back device (20) having a ball screw (21 ) connected to a variable load of reversible polarity (± L) and having a portion penetrating a housing (24). The device includes a braking mechanism...  
WO/2009/148307A2
An electricity distribution system, arranged to provide low voltage to end users, for instance vehicles (P), located at end user locations, comprising: - a first medium voltage line (Kl) for providing medium voltage, wherein the first me...  
WO/2009/148307A9
An electricity distribution system, arranged to provide low voltage to end users, for instance transport means (P), located at end user locations, comprising: - a first medium voltage line (K1) for providing medium voltage, wherein the f...  

Matches 551 - 600 out of 6,061