Login| Sign Up| Help| Contact|

Patent Searching and Data


Matches 501 - 550 out of 5,886

Document Document Title
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...  
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/2009/148307A3
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/2009/140453A1
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/2009/138593A3
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/2009/138593A4
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/2009/138593A2
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/2009/135975A3
The invention relates to a modular device for removing and installing aircraft components comprising a modular frame (41) as main system of the device, common for every aircraft component which is to be installed or removed, this modular...  
WO/2009/136040A3
The invention relates to a method and system for automatically depositing objects (306) for the purpose of their transportation. A first electromagnetic identification label (304) is attached by the user to the object to be transported (...  
WO/2009/135472A3
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...  
WO/2009/136040A2
The invention relates to a method and system for automatically depositing objects (306) for the purpose of their transportation. A first electromagnetic identification label (304) is attached by the user to the object to be transported (...  
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/2009/135975A2
The invention relates to a modular device for removing and installing aircraft components comprising a modular frame (41) as main system of the device, common for every aircraft component which is to be installed or removed, this modular...  
WO/2009/136152A1
A PAPI light (fig.1) is operable to emit a beam of light comprising red light in a first sector of the beam and white light in a second sector of the beam. The white light has a colour temperature greater than 3500K. The white light may ...  
WO/2009/132527A1
A full-floating steam-powered compression catapult is presented. Its shell comprises a left cylinder (1), a right cylinder (2) and a base (5). A left cylinder cover (11) and a right cylinder cover (12) are respectively arranged on the en...  
WO/2009/132402A2
Aircraft fuselage structures have reinforcement members in the vicinity of the stringer openings formed in frame members and are rigidly lap joined to a surface region of the frame members by a friction stir weld region. Such aircraft fu...  
WO/2009/134928A2
Airship handling devices and associated systems and methods are disclosed herein. An airship handling device in accordance with one embodiment of the disclosure, for example, can include a first support member mountable to a ground vehic...  

Matches 501 - 550 out of 5,886