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Patent Searching and Data


Matches 551 - 600 out of 3,006

Document Document Title
WO/2009/074913
A light indication system for airport runways, road routes and the like, comprising a circuit (9) consisting of at least one series of LED-type individual lighting units (4) arranged in series along an electric line (12, 13), being part ...  
WO/2009/074705
The invention relates to an all-terrain robot system comprising a gyrostabilised platform for co-operating with unmanned aerial vehicles. Said system comprises a platform which is mobile in a tractive manner by means of caterpillars, an ...  
WO/2009/068063
The present invention relates to a tester, its use and a method for testing signal lines of a flight control system for a trimmable horizontal stabilizer (THS) motor of an aircraft. The tester comprises at least one test-relay (52, 54) t...  
WO/2009/068063
The present invention relates to a tester, its use and a method for testing signal lines of a flight control system for a trimmable horizontal stabilizer (THS) motor of an aircraft. The tester comprises at least one test-relay (52, 54) t...  
WO/2009/068062
The present invention relates to a method for testing power lines and signal lines onboard of an aircraft, wherein the power lines and signal lines normally connect a 3- phase AC motor with the power supply system of the aircraft, and wh...  
WO/2009/068069
The present invention provides a method and apparatus (1) for testing a valve control system in an aircraft fuel supply system (100) having a plurality of control valves, wherein the control system includes relay means for outputting con...  
WO/2009/070347
Systems and methods are described for condition-based maintenance of mechanical systems. In one embodiment, a method for performing condition-based maintenance on a mechanical system includes providing a radio frequency identifier (RFID)...  
WO/2009/068057
An apparatus (10) for pressurising an aircraft cabin structure (12) and measuring the amount of leakage of the aircraft cabin structure (12) comprises an air supply line (14) which at a first end is connectable to a pressurized air sourc...  
WO/2009/068106
According to an exemplary embodiment of the present invention, a positioning system for mounting a wing (101) of an aircraft to a fuselage (102) of the aircraft is provided, the positioning system comprising a programmable mounting unit ...  
WO/2009/068067
The invention relates to a testing device (12) for checking the operability of a bow steer control unit (10) in an aircraft. The bow steer control unit has a plurality of input ports and a plurality of output ports, wherein at least one ...  
WO/2009/068097
According to an exemplary embodiment of the present invention, a method for mounting a wing of an aircraft to a fuselage of the aircraft is provided, in which a difference between a vertical target position and a vertical actual position...  
WO/2009/068107
The present invention relates to a method of preparating the connection of two fuselage sections (2, 3). A less complicated and time consuming method was found by using High-Speed- Drilling (HSD) for a group of final bore holes through t...  
WO/2009/068097
According to an exemplary embodiment of the present invention, a method for mounting a wing of an aircraft to a fuselage of the aircraft is provided, in which a difference between a vertical target position and a vertical actual position...  
WO/2009/068105
According to an exemplary embodiment of the invention, a determination system (200) for determining a distance between a first hydraulic line of a wing of an airplane and a second hydraulic line of a fuselage of an airplane is provided, ...  
WO/2009/068066
An apparatus (10) for fuelling an aircraft, in particular during performing a tank leakage test on the aircraft, comprises a fuel supply line (14) for supplying fuel to an aircraft tank system (12), at least one pressure sensor (26) for ...  
WO/2009/068065
An apparatus (10) for testing an aircraft tank system (12) comprises a fuel supply device (14) including a fuel reservoir (16), a fuel supply line (18) for supplying fuel from the fuel reservoir (16) to a fuel outlet (20) of the fuel sup...  
WO/2009/058672
Ground support equipment for servicing an airplane includes a ground support equipment cart upon which are mounted at least two equipment modules (20,1308,400) and a control module (22). A first equipment module (20) mounted upon the car...  
WO/2009/058680
An airplane ground support system includes a multi-voltage power supply. This system includes an air conditioning module and a control module having a display and a processor, the display and processor presenting an airplane type or clas...  
WO/2009/058677
A ground support equipment air conditioning system detachably connects to a port on an airplane. An air conduit connects an air intake and filter to a coupling that is adapted to be connected to one end of an air duct or hose (26) the ot...  
WO/2009/058680
An airplane ground support system includes a multi-voltage power supply. This system includes an air conditioning module and a control module having a display and a processor, the display and processor presenting an airplane type or clas...  
WO/2009/058627
A modular and compact air conditioning system is designed to be conveyed by a ground support equipment cart and to occupy minimal space within the cart. The system is constructed within a rectangular frame supporting top, bottom, left si...  
WO/2009/058646
A frame, panel, and fastener system for use in constructing modules (20) that are to be installed on a ground support equipment cart (10). The modules have a rectangular frame (40) that is constructed primarily by connecting together mem...  
WO/2009/058646
A frame, panel, and fastener system for use in constructing modules (20) that are to be installed on a ground support equipment cart (10). The modules have a rectangular frame (40) that is constructed primarily by connecting together mem...  
WO/2009/058643
A captive fastener system for use in removably attaching cover panels to openings in the sides of modules containing equipment on airplane ground support equipment carts. Sets of fasteners each include: a nut (98) having mounted on its s...  
WO/2009/058628
Airplane ground service equipment includes an air conditioning system for an airplane (823) and also a fluid cooling system for airplane electronics (825) which detachably connects to a first port and a second port on the airplane. The f...  
WO/2009/058639
A ground support equipment cart (10) contains one or more removable equipment modules. The cart contains a rectangular module (400) containing airplane air conditioning components mounted upon the cart and extending the width of the cart...  
WO/2009/058475
According to one embodiment, code embodied in a computer readable storage medium is configured to generate a checklist for a vehicle by receiving a measured value obtained from at least one sensor configured on the vehicle, setting a par...  
WO/2009/055219
In non-limiting, illustrative embodiments, methods, systems, and manufacturing facilities are provided for locating components of a structure. Locations of features (18) of components (12) of a structure (14) are simultaneously determine...  
WO/2009/055218
Nondestructive inspection (NDI) on a structure having a cavity includes exciting the structure with electromagnetic radiation and analyzing the cavity's electromagnetic field response to detect a state change of the structure.  
WO/2009/055353
A ground support system configured to support servicing of aircraft may include a main body housing one or both of an engine and/or a blower, a control panel that is used to control operation of one or both of the engine and/or blower, a...  
WO/2009/055218
Nondestructive inspection (NDI) on a structure having a cavity includes exciting the structure with electromagnetic radiation and analyzing the cavity's electromagnetic field response to detect a state change of the structure.  
WO/2009/055353
A ground support system configured to support servicing of aircraft may include a main body housing one or both of an engine and/or a blower, a control panel that is used to control operation of one or both of the engine and/or blower, a...  
WO/2009/053539
This maintenance trolley (17) for the air intake (9) of the nacelle of an aircraft turbojet engine is notable in that it comprises a base (19) and a platform (23) cantilever-mounted on this base (19) and designed to enter said air intake...  
WO/2009/047825
A liftable vehicle provided with a single cab (A) wherein both the operator/driver of the vehicle and the load and/or passengers (in general, disabled persons) are positioned. The cab is operatively connected with a flatbed (B) bearing t...  
WO/2009/046703
The invention relates to a method and a device for detecting and safely neutralizing hazardous goods to be selected from a quantity of non-hazardous goods, having the following characteristics: a) the consecutively delivered quantity of ...  
WO/2009/046503
Method to decrease the turnaround time of aircraft, whereby if an airplane (7) is to carry passengers (10) or a combination of passengers (10) and cargo, the airplane (7) contains at least one passenger module (1) provided with seats (2)...  
WO/2009/047405
The invention relates to a riveting tack (50) to be introduced into coaxial openings of at least two elements to be assembled, and comprising a hollow cylindrical body (51), a rod (53) passing through the hollow body and partially provid...  
WO/2009/047405
The invention relates to a riveting tack (50) to be introduced into coaxial openings of at least two elements to be assembled, and comprising a hollow cylindrical body (51), a rod (53) passing through the hollow body and partially provid...  
WO/2009/047578
Spraying installation (1 ) on a chassis (2) of a truck (3), comprising a spraying nozzle (4) at the free end of a telescopic arm (5) attached to the chassis (2) via elevation means, characterized by the telescopic arm (5) being supported...  
WO/2009/046933
In areas of the apron of an airport where the underground power supply system for temporarily parked airplanes is not sufficiently powerful or even missing, diesel-power electrodynamic generators are conventionally used. According to the...  
WO/2009/048666
The invention is a method for launching and recovering a child aircraft, manned or unmanned, as well as providing a method for continuous flight to and from a parent aircraft, manned or unmanned, from a pylon that is mounted externally o...  
WO/2009/044004
The invention relates to a baggage container (10) with at least one loading platform (14, 16) for single items of hand baggage (12), said baggage items each having a base on which are two opposed lateral walls, said loading platform comp...  
WO/2009/044362
The inner structure (20) of a wing is first fixed on the top surface (11) of the bottom panel (10). The inner structure and the top panel (12) are retained separately in the respective forms which they must assume in accordance with a pr...  
WO/2009/044362
The inner structure (20) of a wing is first fixed on the top surface (11) of the bottom panel (10). The inner structure and the top panel (12) are retained separately in the respective forms which they must assume in accordance with a pr...  
WO/2009/042549
A method and apparatus for manufacturing and installing a fairing on an aircraft. In one advantageous embodiment, a composite fairing (402) is installed on the aircraft (400). A composite sheet having a form of the composite fairing is f...  
WO/2009/042549
A method and apparatus for manufacturing and installing a fairing on an aircraft. In one advantageous embodiment, a composite fairing (402) is installed on the aircraft (400). A composite sheet having a form of the composite fairing is f...  
WO/2009/037475
A load indicator comprises a load bearing assembly of first and second load bearing members (23, 22) connected together to bear a lateral load applied to the first member (23), the first load bearing member defining a cavity (25) with th...  
WO/2009/037465
An overload detecting assembly comprises a first load bearing member (10) adapted to flex laterally in response to a load to be monitored, a second load bearing member (11) spaced from the first under normal load conditions and which is ...  
WO/2009/037007
Disclosed is a method for producing a fuselage airframe of an aircraft. Said method, in which several fuselage sections that are arranged one behind another are joined together, comprises the following steps: a) an external skin segment ...  
WO/2009/033221
The invention is a process for the repair of materials used in the manufacture of non structural aircraft interior components which utilises the application of cyanoacrylate type material to a damaged underlying surface. The invention in...  

Matches 551 - 600 out of 3,006