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Matches 501 - 550 out of 2,962

Document Document Title
WO/2009/113911
The invention relates to systems for ground handling operation of airships and can be used for testing aircraft engines in airport areas. The inventive device comprises a body which is mounted on a trailing truck, contains facilities for...  
WO/2009/113327
Provided is a joint of a boarding bridge in which smooth alighting and boarding can be ensured while suppressing a feeling of uneasiness of a passenger by eliminating the level difference between the alighting/boarding section of an airc...  
WO/2009/106792
The present invention is a collector (56) for collecting washing fluid issuing (40, 41) from a gas turbine engine (10) during and/or after a washing operation. The collector (56) comprises a collection tray (58, 53) and an inlet collecto...  
WO/2009/101346
The invention relates to a method for managing the operations in an aircraft (A) assembly and outfitting workshop, characterised in that said method comprises, for each operation or for a given operation sequence, preparing and storing t...  
WO/2009/098012
An aircraft tank system (10) comprises a tank cell for housing fuel, a fuel line (12), connecting the tank cell to fuel inlet connector (14) and a venting device (16), which connects the tank cell to the environment for venting. A shut-o...  
WO/2009/098439
A baggage handling system comprising: a plurality of pre-loading queues (10) operable to receive baggage; and a loading station (17) operable to receive baggage from individual ones of said queues. Thereby, a single loading station can b...  
WO/2009/098012
An aircraft tank system (10) comprises a tank cell for housing fuel, a fuel line (12), connecting the tank cell to fuel inlet connector (14) and a venting device (16), which connects the tank cell to the environment for venting. A shut-o...  
WO/2009/098439
A baggage handling system comprising: a plurality of pre-loading queues (10) operable to receive baggage; and a loading station (17) operable to receive baggage from individual ones of said queues. Thereby, a single loading station can b...  
WO/2009/098012
An aircraft tank system (10) comprises a tank cell for housing fuel, a fuel line (12), connecting the tank cell to fuel inlet connector (14) and a venting device (16), which connects the tank cell to the environment for venting. A shut-o...  
WO/2009/096285
A boarding bridge which has an inexpensive rigid structure having less trouble and in which a difference in level between passages of adjoining passage bodies is eliminated to minimize the occurrence of falls etc. of passengers. The boar...  
WO/2009/092886
This modular tool storage system comprises: a set of tools designed to be used in carrying out different types of tasks, each tool belonging to a subset corresponding to a given type of task or to a subset of tools containing tools commo...  
WO/2009/094566
Systems and methods for recovering unmanned aircraft and controlling post- recovery motion of the aircraft are disclosed herein. An aircraft recovery system for recovering an unmanned aircraft in flight in accordance with one embodiment ...  
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...  

Matches 501 - 550 out of 2,962