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Matches 301 - 350 out of 3,008

Document Document Title
WO/2011/073428
The invention relates to an assembly (1) for verifying a real model using a virtual model, comprising a real model (24) having a real coordinate system, a virtual model (26) having a virtual coordinate system, a first position determinat...  
WO/2011/068536
Embodiments of a free-floating connector engagement and retention system are provided. In some embodiments, the system includes a slotted mounting surface, a connector carrier guide, and a connector carrier to receive a connector. The co...  
WO/2011/067108
The invention relates to a lighting apparatus (1) for a beacon system having at least one VIS-LED (4) as a first light source and a second light source (6) emitting substantially infrared radiation.  
WO/2011/066891
The invention relates to an aircraft tractor (4) for moving aircrafts (1) coupled thereto on airfields, comprising a drive assembly (5) for driving at least one wheel set (6, 6', 6") of the tractor (4) and at least one coupling unit (7) ...  
WO/2011/068443
The invention relates to helicopters with removable fuel tanks, wherein all fuel tanks of the helicopter are removable fuel tanks. Helicopters all fuel tanks of which are removable can safely be stored on ships and aircraft carriers.  
WO/2011/064808
A machine (1) for. extending and retracting an extendable corrugated hose (3) comprises a tubular housing (4) for storing the extendable corrugated hose (3) in a retracted condition, tubular housing (4) having a rear end (5), which is co...  
WO/2011/066030
An unmanned aerial vehicle (UAV) launch tube (100) that comprises at least one inner layer of prepreg substrate (370) disposed about a right parallelepiped aperture (305), at least one outer layer of prepreg substrate (380) disposed abou...  
WO/2011/064519
The invention relates to an aircraft comprising a structural element, such as a fuselage, a wing or a tail unit, including: a wall separating the inside and the outside of the element and including portions jointly defining an inner volu...  
WO/2011/066030
An unmanned aerial vehicle (UAV) launch tube (100) that comprises at least one inner layer of prepreg substrate (370) disposed about a right parallelepiped aperture (305), at least one outer layer of prepreg substrate (380) disposed abou...  
WO/2011/062905
Embodiments of a modular condenser unit are provided. The modular condenser unit may include a housing and a first condenser coil and a second condenser coil disposed within a volume of the housing. A fan may also be disposed in an end o...  
WO/2011/062696
A method and apparatus may be present for processing parts. A first part may be positioned in a first position. A first number of features may be formed on the first part using a feature forming system at a number of points for attachmen...  
WO/2011/061770
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/2011/061306
The invention relates to a carriage (1) for transporting an aircraft engine module (2) from a preparation station (3) to an assembly station (4), said carriage comprising, on a rolling chassis (8), a framework (10) that can be rendered h...  
WO/2011/062893
Embodiments of a modular air conditioning (AC) unit include a base unit and a blower selected from a group of blowers configured for different cooling capacities. The module AC unit also includes at least one heat exchanger unit selected...  
WO/2011/061770
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/2011/061307
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/2011/058076
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/2011/054907
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/2011/048591
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/2011/047879
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/2011/046482
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/2011/042286
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/2011/039309
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/2011/034992
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/2011/034992
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/2011/030140
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/2011/023698
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/2011/021206
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/2011/017727
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/2011/017727
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/2011/016936
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/2011/015291
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/2011/015679
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/2011/015291
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/2011/012996
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/2011/012996
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/2011/012996
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/2011/009916
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/2011/009983
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/2011/007200
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/2011/004119
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/2011/000001
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/2011/002479
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/2010/149303
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/2010/146045
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/2010/145638
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/2010/145666
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/2010/145915
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/2010/145637
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/2010/142924
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...  

Matches 301 - 350 out of 3,008