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Patent Searching and Data


Matches 551 - 600 out of 3,033

Document Document Title
WO/2009/091315
A system for automatic or auto pilot controlled landing of air vehicle (2) with an undercarriage (10) with a substantially plane lower side, at a stationary or mobile landing place is described. The system is primarily characterized in t...  
WO/2009/085940
An osculating device (100) for a mobile boarding bridge includes an air charge part (110) that is attached to the end of the canopy (140) of a mobile boarding bridge into which air can be injected. A buffer material (120) is provided in ...  
WO/2009/086025
A mobile boarding bridge (101) is equipped with climate control facilities. The mobile boarding bridge is furnished with multiple collapsible tunnels (110, 120). A heating/cooling device (160) comprising a climate controller (161) genera...  
WO/2009/086025
A mobile boarding bridge (101) is equipped with climate control facilities. The mobile boarding bridge is furnished with multiple collapsible tunnels (110, 120). A heating/cooling device (160) comprising a climate controller (161) genera...  
WO/2009/085940
An osculating device (100) for a mobile boarding bridge includes an air charge part (110) that is attached to the end of the canopy (140) of a mobile boarding bridge into which air can be injected. A buffer material (120) is provided in ...  
WO/2009/079984
The invention relates to a tensile-force limiter for the use in particular for recovering heavy sensitive loads, comprising a housing (2), at one end of which is provided a deflecting roller (8) for the traction means and at the opposite...  
WO/2009/077833
Assembling unit for use inside housings of luminous signallers arranged in airport areas, comprising an electronic board (1) and at least an electronic or electro-mechanical switching component (4), which is connected to the electronic b...  
WO/2009/079616
An exemplary shock-absorbing device for a boarding bridge is for use with lift columns (200) that support the boarding bridge tunnel (100). The device comprises a first transverse support (310) coupled to the bottom of said lift columns ...  
WO/2009/079045
Methods and apparatus for marine deployment according to various aspects of the present invention may operate in conjunction with a floatable housing adapted to be deployed by a marine vehicle. The floatable housing may be adapted to be ...  
WO/2009/076793
An electromagnetic ejector for mini-satellite and spacecraft on the moon is provided. Present application adopts the electromagnetics principles of that current elements are driven by the ampere-force generated in the strong electromagne...  
WO/2009/079614
An exemplary apparatus is for moving a tunnel part of a boarding bridge equipped with a tunnel (100) that consists of a first tunnel part (110), a second tunnel part (120), and a third tunnel part (130) in sequence from one side and can ...  
WO/2009/079614
An exemplary apparatus is for moving a tunnel part of a boarding bridge equipped with a tunnel (100) that consists of a first tunnel part (110), a second tunnel part (120), and a third tunnel part (130) in sequence from one side and can ...  
WO/2009/079616
An exemplary shock-absorbing device for a boarding bridge is for use with lift columns (200) that support the boarding bridge tunnel (100). The device comprises a first transverse support (310) coupled to the bottom of said lift columns ...  
WO/2009/077010
An airfield lighting device comprises, in particular, at least one first light-emitting diode (LED) (1) on a first base body (2), a first heat conduction pipe (3) with a heat transfer medium (31), a first heat sink (4) and a housing (5) ...  
WO/2009/079045
Methods and apparatus for marine deployment according to various aspects of the present invention may operate in conjunction with a floatable housing adapted to be deployed by a marine vehicle. The floatable housing may be adapted to be ...  
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 ...  

Matches 551 - 600 out of 3,033