| Document |
Document Title |
|
WO/2010/020049 |
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/2010/020050 |
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/2010/020751 |
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/2010/020751 |
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/2010/018292 |
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/2010/018090 |
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/2010/018090 |
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/2010/018090 |
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/2010/012261 |
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/2010/012261 |
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/2010/012261 |
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/2010/014333 |
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/2010/010382 |
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/2010/010279 |
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/2010/011783 |
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/2010/010382 |
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/2010/009899 |
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/2010/009899 |
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/2010/008323 |
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/2010/006946 |
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/2010/004172 |
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/2010/003818 |
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/2010/003686 |
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/2010/003818 |
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/2010/003640 |
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/2010/001009 |
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/2010/001009 |
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/2010/003051 |
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/2010/000575 |
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/2009/156637 |
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/2009/156140 |
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/2009/156140 |
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/2009/156140 |
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/2009/149491 |
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/2009/151423 |
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/2009/148307 |
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/2009/148307 |
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/2009/147494 |
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/2009/148307 |
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/2009/143798 |
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/2009/141475 |
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/2009/140453 |
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/2009/138593 |
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/2009/138593 |
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/2009/138593 |
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/2009/135975 |
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/2009/136040 |
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/2009/135472 |
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/2009/135472 |
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/2009/136040 |
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 (...
|
