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Patent Searching and Data


Matches 351 - 400 out of 5,886

Document Document Title
WO/2011/061770A1
A method for detecting physical associations between electronic identifiers and objects to which the electronic identifiers are physically coupled. The method 'includes the steps of: detecting the electronic identifiers in respective det...  
WO/2011/061307A1
The invention relates to an assembly for handling a module (1) especially comprising a carriage (2), a part (5) that pivots at the top of the carriage, equipment (12) for supporting the module, and complementary means (19) for joining th...  
WO/2011/058076A1
The invention relates to an integrated end-to-end maintenance platform (1) for maintenance of an aircraft (8) comprising a customer interface for selecting a customized service package including modular services of different aircraft mai...  
WO/2011/054907A1
The invention relates to a method for operating a loading system for loading luggage (90, 90a-90f) at an airport. The loading system used for this purpose comprises a transport system (10) having at least one feed section (14a-14b, 16a-1...  
WO/2011/048591A1
A system is provided for guarding a perimeter, including a control center, a launch system, a controller and a communication system. The control center is configured for generating a control signal responsive to receiving infiltration in...  
WO/2011/047879A1
The invention relates to a method for introducing bores (58) that are aligned in relation to each other into a body section (28) of a component (20) consisting of a plurality of individual bodies (28, 30), wherein the component (20) is j...  
WO/2011/046482A1
Adjustable bracket in fixtures with a bottom plate (5) for fastening on a supporting structure and a top plate (4) on which a fixture can be mounted. The top plate (4) can be adjusted in the six degrees of freedom in the room. Three adju...  
WO/2011/042286A1
An asset management system comprising a plurality of assets (12), a plurality of sensors for determining one or more operating conditions for each of said assets and one or more processors (14,22) for determining a risk profile (26,28,30...  
WO/2011/039309A1
The invention relates to a lighting unit for lighting airfields on an airport, in particular for delivering signals to an airplane. It comprises a light source, which has at least one light-emitting diode (4) for generating light to be e...  
WO/2011/034992A2
An aircraft fluid application system includes a structure, and nozzles coupled to the structure and able to move in relation to the structure. The structure may be a fixed structure, or may be a movable structure. The nozzles may be moun...  
WO/2011/034992A3
An aircraft fluid application system (10) includes a structure (16), and nozzles (14) coupled to the structure and able to move in relation to the structure. The structure may be a fixed structure, or may be a movable structure. The nozz...  
WO/2011/030140A1
A transport cradle for a skid-supported helicopter having a pair of laterally spaced and generally parallel support skids. The cradle comprises a main frame (2, 102) comprising a pair of laterally spaced elongate support arms (4, 104) ex...  
WO/2011/023698A1
The invention relates to a method for loading ULD containers with flight baggage or similar cargo, relatively large quantities of which can be transported in the ULD container, which forms a transporting unit, in a state in which layerin...  
WO/2011/021206A3
The disclosure relates to Aeronautics, more particularly relating to wing planforms that reduce wing drag substantially in aircraft driven by propellers or other rotors in tractor configuration. An aircraft comprising a wing and propelle...  
WO/2011/017727A2
The invention relates to a method for producing a hollow body (1), in particular an aircraft fuselage (2), designed as a sandwich construction, wherein an inner layer (3) comprises a specifiable number of plies (4) of a specifiable, at l...  
WO/2011/017727A3
The invention relates to a method for producing a hollow body (1), in particular an aircraft fuselage (2), designed as a sandwich construction, wherein an inner layer (3) comprises a specifiable number of plies (4) of a specifiable, at l...  
WO/2011/016936A1
Systems and methods are provided for detecting an anomaly in a hidden portion of a first layer of a multi-layer structure. A monitoring element is provided on at least one exposed end of a fastener that extends through the multi-layer st...  
WO/2011/015291A2
The invention relates to a device for de-icing vehicles, particularly airplanes, comprising flexible, electric heat elements with a control system, which can be connected to a power source, wherein the heat elements are arranged in flexi...  
WO/2011/015679A3
The present system allows conventional, unprepared fixed-wing aircrafts to land safely on unprepared, small zones, enabling an aerodynamic capacitance in which the airplanes can fly in a controlled manner against coherent airflow, assist...  
WO/2011/015291A3
The invention relates to a device for de-icing vehicles, particularly airplanes, comprising flexible, electric heat elements with a control system, which can be connected to a power source, wherein the heat elements are arranged in flexi...  
WO/2011/012996A8
A self-righting aerostat (10) is described comprising at least one blimp- shaped body (12), supported by gas and in which a bow and a stern are defined, a plurality of tailplanes (13) having a stabilizing function, a self-righting system...  
WO/2011/012996A2
A self-righting aerostat (10) is described comprising at least one blimp- shaped body (12), supported by gas and in which a bow and a stern are defined, a plurality of tailplanes (13) having a stabilizing function, a self-righting system...  
WO/2011/012996A3
A self-righting aerostat (10) is described comprising at least one blimp- shaped body (12), supported by gas and in which a bow and a stern are defined, a plurality of tailplanes (13) having a stabilizing function, a self-righting system...  
WO/2011/009916A3
The invention relates to a method for system installation in a fuselage (4), to a device (2) comprising a rail system (14) for carrying out said method, and to a freight loading system (50) that uses the rail system (14) as a guidance sy...  
WO/2011/009983A1
The invention relates to a method including manufacturing the front section (2) and the rear section (3), with the assembly structure built into the rear section, and subsequently assembling the two sections. Manufacturing the front sect...  
WO/2011/007200A1
A method for at least partially de-icing an aircraft by applying a de-icing fluid through a nozzle (10) is disclosed. The method involves the steps of : measuring a distance to an outside surface of the aircraft, applying the distance in...  
WO/2011/004119A1
The invention relates to a device (6) for closing a fuel-dump circuit (48) of an aircraft, including a coupling tip (43). The tip has a seal (31) and a means (34) for changing a dimension (d) of the seal.  
WO/2011/000001A1
The invention relates to a device for cleaning a wastewater line (3) of a vacuum toilet system, in particular in an aircraft (1), train, or bus, comprising at least one toilet (2, 2'), a collection tank (4), the wastewater line (3) conne...  
WO/2011/002479A1
One embodiment includes a launch vessel defining an elongate, linear interior extending from a bottom portion to an exit opening. The embodiment includes a ram slidably disposed in the launch vessel, the ram sealed to the vessel. The emb...  
WO/2010/149303A1
A system and method for tracking the history of modules of a modular apparatus such as a gas turbine engine is provided. Each module (2a -2e) is provided with an associated module tracking device (3a - 3e). In use an interface device (9)...  
WO/2010/146045A1
The invention relates to a drive system for an aircraft, comprising an electric motor. With the aim of allowing aircraft to be driven on the ground more efficiently and also more quietly, the invention provides that the electric motor is...  
WO/2010/145638A1
The disclosed aircraft transfer system is used for transferring an aircraft located in a pick-up zone into a park position, and has at least one rail (6, 8), the parking section of which is arranged near the park position, and the pick-u...  
WO/2010/145666A1
The invention relates to a method for positioning an airship 100 at a wind turbine generator. The method comprises the step of docking the airship 100 at the wind turbine generator with a forwards docking section, a rearwards docking sec...  
WO/2010/145915A1
A system for producing a vehicle cabin comprises at least one first equipment component (2, 4), at least one first surface element (6) and at least one guiding element (16). The first surface element (6) is arranged movably at the first ...  
WO/2010/145637A1
A gripper arrangement is disclosed for coupling an aircraft to an aircraft transfer system, wherein a connecting part (14) which can be connected to a gripper (2) is attached to the aircraft, and wherein the gripper is coupled to a gripp...  
WO/2010/142924A2
The invention relates to a method for treating the drinking water circuit of an aircraft (A), said circuit including at least one storage tank (100), a plurality of pipes providing a plurality of water inlet (210) and outlet (220) points...  
WO/2010/142924A3
The invention relates to a method for treating the drinking water circuit of an aircraft (A), said circuit including at least one storage tank (100), a plurality of pipes providing a plurality of water inlet (210) and outlet (220) points...  
WO/2010/141254A1
A modular air conditioning (AC) system including one or more AC modules is provided. The AC modules may be adapted to function individually or cooperatively as part of a modular system. The AC modules may be further adapted to connect in...  
WO/2010/140994A1
The invention relates to aviation, in particular to aircraft engineering. A method for transporting a "BiCar" coaxial-rotor aircraft, including on public roads, involves transforming the aircraft and then transporting it on an open platf...  
WO/2010/138251A1
A method and apparatus for aligning objects may be present. A locating pin may be positioned relative to secondary holes in a plurality of objects. The locating pin may comprise a segment with a cross section having an elliptical shape, ...  
WO/2010/136102A4
The invention relates to a transport device (10) for use when mounting interior component modules (12) in an aircraft, comprising a frame (18) and an interior component module support unit (30). Said interior component module support uni...  
WO/2010/138250A1
A method and apparatus for aligning a plurality of objects may be present. A locating pin may be positioned relative to secondary holes in a plurality of objects. The locating pin may comprise a segment with a cross section having a numb...  
WO/2010/136630A2
A repair process for a composite material panel (1) that forms part of the fuselage, the wings or the stabilizers of an aircraft, with the panel (1) having large dimensions and having irregular contours in some areas, comprising of edges...  
WO/2010/138265A1
Systems and methods for recovering unmanned aircraft and controlling post-recovery motion of the aircraft are disclosed herein. An aircraft recovery system for handling an unmanned aircraft in accordance with one embodiment of the disclo...  
WO/2010/136451A1
The invention relates to a theft protection during the security check of carry-on luggage and/or other personal objects (5) in passenger terminals of airports or the like, wherein the objects are placed by the passenger (4) in a provided...  
WO/2010/136103A1
The invention relates to a method for mounting interior components in an aircraft, comprising the premounting of a first interior component (14) and the premounting of a second interior component (18). The first and/or the second interio...  
WO/2010/136717A2
The invention relates to a method for producing an aircraft, comprising: passing a mandrel (6, 30) through frames (52) supported by a magazine (46) and, during the passing operation, transferring the frames onto the mandrel.  
WO/2010/136369A1
The invention relates to a nacelle for receiving an aircraft engine (2), comprising a fixed tubular cowl and at least one mobile portion connected to the fixed cowl by a means for moving the mobile portion between a near position and a s...  
WO/2010/136717A3
The invention relates to a method for producing an aircraft, comprising: passing a mandrel (6, 30) through frames (52) supported by a magazine (46) and, during the passing operation, transferring the frames onto the mandrel.  
WO/2010/136630A3
A repair process for a composite material panel (1) that forms part of the fuselage, the wings or the stabilizers of an aircraft, with the panel (1) having large dimensions and having irregular contours in some areas, comprising of edges...  

Matches 351 - 400 out of 5,886