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Patent Searching and Data


Matches 701 - 750 out of 6,395

Document Document Title
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/2010/025376A1
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/2010/023371A1
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/2010/020050A1
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/2010/020049A1
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/2010/020751A2
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/2010/018090A3
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/2010/018090A4
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/2010/018090A2
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/2010/012261A4
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/2010/012261A2
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/2010/012261A3
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/2010/010279A1
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/2010/010382A2
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/2010/009899A3
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/2010/010382A3
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/2010/011783A3
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/2010/009899A2
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/2010/003686A1
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/2010/004172A2
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/2010/003640A3
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/2010/003818A2
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/2010/001009A2
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/2010/000575A1
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/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/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/2009/156140A4
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/2009/156140A2
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/2009/156637A2
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/2009/151423A1
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/2009/149491A1
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/2009/148307A9
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...  
WO/2009/147494A2
A support platform (100) for workers dealing with maintenance and construction of a means of transport (NT). The platform (100) comprises: - a motorised carriage (1); - a horizontal walkway (PDN) supported by the motorised carriage (1); ...  
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/2009/148307A3
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/2009/143798A1
A catapult for launching an aircraft comprises a carriage (14) for supporting the aircraft, said carriage being movable on a guide rail (2), and at least one cable (10), which can be tensioned and is configured to be elastic at least in ...  
WO/2009/141475A1
The invention relates to a method and accessory tooling for mounting aeronautical structures such as torsion boxes. The method basically comprises mounting the longitudinal members (2, 2') and the ribs (3) with reference to the liner (4)...  
WO/2009/138593A2
The present invention relates to the fitting‑out of an aircraft by the laying of a floor, particularly in the cockpit of an aircraft. The invention relates more particularly to a method of fitting out an aircraft and to such an aircraf...  
WO/2009/140453A1
A system and method for the analysis of composite materials in aircraft components. Structured light measurements are used to determine the 3-dimensional shape of an object, which is then analyzed to minimize the number of scans when per...  
WO/2009/138593A4
The present invention relates to the fitting‑out of an aircraft by the laying of a floor, particularly in the cockpit of an aircraft. The invention relates more particularly to a method of fitting out an aircraft and to such an aircraf...  
WO/2009/138593A3
The present invention relates to the fitting‑out of an aircraft by the laying of a floor, particularly in the cockpit of an aircraft. The invention relates more particularly to a method of fitting out an aircraft and to such an aircraf...  
WO/2009/135472A2
The invention relates to a device in the form of a ground-bound device for take off, landing and taxiing aircrafts or flying objects without a landing gear or with a retracted landing gear. Said device consists of three main components, ...  
WO/2009/135472A8
The invention relates to a device in the form of a ground-bound device for take off, landing and taxiing aircraft or flying objects without a landing gear or with a retracted landing gear. Said device consists of three main components, a...  

Matches 701 - 750 out of 6,395