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Patent Searching and Data


Matches 351 - 400 out of 3,038

Document Document Title
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...  
WO/2010/136789A1
A baggage handling apparatus has a first, indexing, conveyor (20) which receives items of baggage (18) from a discharge chute (10). The first conveyor (20) conveys the items of baggage (18) to a second, queueing, conveyor (24) which in t...  
WO/2010/136102A1
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/2010/133541A1
The invention relates to a method for controlling an obstruction light (2), wherein a receiver (4) cooperates with a switching device (S) for the obstruction light (3). According to the invention, when receiving a first predefined signal...  
WO/2010/133602A3
The invention relates to a method for protecting a part of a surface of an aircraft against soiling with insect residues and/or against icing, comprising the following steps: a) coating the part of the surface to be protected with a coat...  
WO/2010/130687A3
The invention relates to a method for producing an aircraft fuselage (2) comprising at least two fuselage tubes (8, 10, 12). According to the invention, the connecting sections (20, 22) used for forming a transversal joining region (18) ...  
WO/2010/127595A1
Disclosed is a nylon conveyor roller (110) used for a lift platform device of a transit vehicle for airport goods. A shaft hole (111) extends through the center of the nylon conveyor roller (110). The front end and the back end (112) of ...  
WO/2010/128246A2
The invention relates to equipment for refueling an aircraft, including a pipe (40) provided with means (42) for connecting onto an intake port (301) of the fuel tank of the aircraft (400) and, at or in the vicinity of the connection mea...  
WO/2010/128246A3
The invention relates to equipment for refueling an aircraft, including a pipe (40) provided with means (42) for connecting onto an intake port (301) of the fuel tank of the aircraft (400) and, at or in the vicinity of the connection mea...  
WO/2010/126228A2
The present invention relates to a universal platform and an aircraft assembly method using the same. The universal platform of the present invention comprises a number of scissors lifts arranged around an air craft, each of the scissors...  
WO/2010/125172A2
The invention relates to a device for spatially orienting at least two large-size subgroup components, in particular at least one side shell (7,8), at least one upper shell (12), at least one lower shell (11), and/or at least one floor f...  
WO/2010/125172A3
The invention relates to a device for spatially orienting at least two large-size subgroup components, in particular at least one side shell (7,8), at least one upper shell (12), at least one lower shell (11), and/or at least one floor f...  
WO/2010/127217A1
A high intensity LED based lighting array for use in an obstruction light with efficient uniform light output is disclosed. The high intensity LED based lighting array has a first concentric ring having a plurality of reflectors and ligh...  
WO/2010/126228A3
The present invention relates to a universal platform and an aircraft assembly method using the same. The universal platform of the present invention comprises a number of scissors lifts arranged around an air craft, each of the scissors...  
WO/2010/118768A1
In a wheel chock arrangement, a first and a second chock (1a, 1b), are each connected to one respective end of two pivotally arranged members (18a, 18b) of a handle arrangement (18). Each chock (1a, 1b) further comprising a release mecha...  
WO/2010/115673A1
The invention relates to a method for determining the route of transport units, especially in material flow systems (e.g. luggage conveyor systems in airports). According to said method, a prognosis is established as to how many transpor...  
WO/2010/115704A1
The invention relates to a component of a material flow system for transporting goods, said component comprising a mechatronics arrangement with transport elements, sensors and actuators for transporting the goods, a control device for c...  
WO/2010/116658A1
A first method comprises a step (S5) for investigating the start point of a shear layer as the flow field characteristics around the original shape of an object to be designed, and a step (S7) for giving a planar object to the vicinity o...  
WO/2010/115317A1
A step route structure for controlling the folding and unfolding of foldable steps comprises a main wheel rail (1), an auxiliary wheel control rail (2), a folding control rail (3) and a stopper rail (4) that pushes a latch hook stopper (...  

Matches 351 - 400 out of 3,038