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Patent Searching and Data


Matches 501 - 550 out of 5,931

Document Document Title
WO/2010/060595A3
The invention relates to an air start unit (1) for starting jet engines in aircraft and other flying devices, comprising a compressor (2) for generating compressed air, and an electricity supply device (3) for operating the compressor (2...  
WO/2010/061384A3
A towbarless airplane tug configured for receiving a landing gear of an airplane and towing it thereby is provided. The tug comprises a chassis configured for receiving thereon at least a portion of the landing gear, a propulsion arrange...  
WO/2010/061384A2
A towbarless airplane tug configured for receiving a landing gear of an airplane and towing it thereby is provided. The tug comprises a chassis configured for receiving thereon at least a portion of the landing gear, a propulsion arrange...  
WO/2010/060595A2
The invention relates to an air start unit (1) for starting jet engines in aircraft and other flying devices, comprising a compressor (2) for generating compressed air, and an electricity supply device (3) for operating the compressor (2...  
WO/2010/057817A4
The invention relates to a structural element (1) for a fuselage cell structure of an aircraft, in particular a stringer profile (2) or an annular frame segment, wherein the structural element (1) is formed using a composite material, in...  
WO/2010/057817A1
The invention relates to a structural element (1) for a fuselage cell structure of an aircraft, in particular a stringer profile (2) or an annular frame segment, wherein the structural element (1) is formed using a composite material, in...  
WO/2010/057942A1
The invention relates to a maintenance device (100) for large-area steel building surfaces (200), comprising a mobile support system, wherein the support system comprises at least one vertical support (10) on which at least one horizonta...  
WO/2010/058027A4
A method for laying a floor covering (2) onto a floor in a cabin of a vehicle comprises the steps of applying a connection means (8, 10) to an element of a group comprising the floor covering (2) and a floor, compacting the floor coverin...  
WO/2010/059024A1
This invention relates to an apparatus for the temporary storage and/or conveyance of articles that consists of a structure, a set of active or live rollers, one or more mobile platforms, a mechanism for lifting the mobile platforms, an ...  
WO/2010/058027A3
A method for laying a floor covering (2) onto a floor in a cabin of a vehicle comprises the steps of applying a connection means (8, 10) to an element of a group comprising the floor covering (2) and a floor, compacting the floor coverin...  
WO/2010/054624A1
The invention relates to a method for determining a position (III) and/or orientation (IV) of a displaceable load (2). The invention further relates to a position and orientation determination system for a combination (4) which comprises...  
WO/2010/052164A3
The invention relates to a device (1, 24, 39) for fixing in position a first fuselage section with a second fuselage section (2, 3) in a transversal joining region (8). The first fuselage section (2) is planked with a first skin (4) and ...  
WO/2010/052164A4
The invention relates to a device (1, 24, 39) for fixing in position a first fuselage section with a second fuselage section (2, 3) in a transversal joining region (8). The first fuselage section (2) is planked with a first skin (4) and ...  
WO/2010/052164A2
The invention relates to a device (1, 24, 39) for fixing in position a first fuselage section with a second fuselage section (2, 3) in a transversal joining region (8). The first fuselage section (2) is planked with a first skin (4) and ...  
WO/2010/049205A3
The invention relates to an apparatus for guiding an aircraft (A) during the approach of an airport runway (R). Said apparatus comprises a device for outputting orientation data to a pilot of the aircraft (A) on whether the aircraft is l...  
WO/2010/049394A2
The aim of the invention is to reduce the circulation of wake turbulences behind an airplane that takes off or lands. For this purpose, annular turbulences (9) are generated on the ground (4) at both sides of the airplane which annular t...  
WO/2010/049205A2
The invention relates to an apparatus for guiding an aircraft (A) during the approach of an airport runway (R). Said apparatus comprises a device for outputting orientation data to a pilot of the aircraft (A) on whether the aircraft is l...  
WO/2010/049224A2
The invention relates to an apparatus for lighting the airfield of an airport, comprising at least one lighting unit (10C, 10S) for emitting an optical signal to a pilot of an aircraft (A), and a monitoring device for verify whether the ...  
WO/2010/049394A3
The aim of the invention is to reduce the circulation of wake turbulences behind an airplane that takes off or lands. For this purpose, annular turbulences (9) are generated on the ground (4) at both sides of the airplane which annular t...  
WO/2010/049224A3
The invention relates to an apparatus for lighting the airfield of an airport, comprising at least one lighting unit (10C, 10S) for emitting an optical signal to a pilot of an aircraft (A), and a monitoring device for verify whether the ...  
WO/2010/048176A1
An aircraft launcher includes a base frame, a first sliding frame that slides with respect to the base frame, a second sliding frame that slides with respect to the first sliding frame, an aircraft support located on the second sliding f...  
WO/2010/046605A2
The invention relates to a method for controlling at least one appliance (12) for moving aircrafts (10): at least one appliance (12) connected to an aircraft is driven to a position (80) that is closer to an entry corridor (74) of a take...  
WO/2010/046603A3
The invention relates to a method according to which an aircraft (10) is moved along the ground by means of at least two separate appliances (12) connected to the aircraft independently from each other or other appliances. A control elem...  
WO/2010/046603A9
The invention relates to a method according to which an aircraft (10) is moved along the ground by means of at least two separate appliances (12) connected to the aircraft independently from each other or other appliances. A control elem...  
WO/2010/045800A1
A lower horizontal-end steering mechanism of a foldable escalator comprises a main wheel steering step way (1) and an auxiliary wheel steering step way (2). A main wheel penetrating gap (14) is arranged between the main wheel steering st...  
WO/2010/046605A3
The invention relates to a method for controlling at least one appliance (12) for moving aircrafts (10): at least one appliance (12) connected to an aircraft is driven to a position (80) that is closer to an entry corridor (74) of a take...  
WO/2010/046603A2
The invention relates to a method according to which an aircraft (10) is moved along the ground by means of at least two separate appliances (12) connected to the aircraft independently from each other or other appliances. A control elem...  
WO/2010/043815A1
The invention relates to a system for guiding a drone during the approach phase to a platform, in particular a naval platform, with a view to landing same, characterised in that the platform is provided with equipment indicating the angl...  
WO/2010/037964A2
The invention relates to a panel assembly for an aircraft fuselage, in which a first panel (10) and a second panel (20) respectively have a first end portion (11) and a second end portion (21) overlapping one another and connected to one...  
WO/2010/031591A2
The invention relates to a method for covering light aircraft and/or parts thereof with a polyester covering fabric, and to a dispersion hot-melt adhesive and to the use thereof for covering. The invention further relates to a light airc...  
WO/2010/031241A1
A cold-launch method and apparatus are provided. The present invention follows the formula of “accumulated energy quick releasing + effective transmission = launching movement”. A gas-liquid combined cylinder (1) is used as the catap...  
WO/2010/031384A2
The method for launching a drone (10) is carried out by means of a launch catapult (9) which applies the launch energy, such that the launch catapult (9) is first of all aligned, before launch. In this case, the launch catapult (9) is co...  
WO/2010/031384A3
The method for launching a drone (10) is carried out by means of a launch catapult (9) which applies the launch energy, such that the launch catapult (9) is first of all aligned, before launch. In this case, the launch catapult (9) is co...  
WO/2010/031591A3
The invention relates to a method for covering light aircraft and/or parts thereof with a polyester covering fabric (17, 18, 19, 29), and to a dispersion hot-melt adhesive and to the use thereof for covering. The invention further relate...  
WO/2010/028360A1
A method for analyzing tolerances for features for an object. A framework may be created from the plurality of features for the object. The framework may be fitted to a plurality of manufactured features for the object based on the plura...  
WO/2010/025910A1
The invention relates to a method for measuring the interior of an elongated body (1, 2), which has a longitudinal axis x in a global xyz coordinate system, a laser profile scan being carried out, during which a laser scanner (6) carryin...  
WO/2010/023371A1
The invention relates to a method for steadying an aircraft using jack props (1), in which: - the number and location of the props to be used is determined as a function of the area of operation, on the basis of a prop map, - strain gaug...  
WO/2010/025376A1
A large scale composite structure is fabricated by forming a plurality of composite laminate modules (208d, 208e) and joining the modules together along their edges (210) using scarf joints.  
WO/2010/020049A1
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/2010/020050A1
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/2010/020751A3
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/2010/020751A2
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/2010/018292A1
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/2010/018090A2
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/2010/018090A4
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...  

Matches 501 - 550 out of 5,931