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Patent Searching and Data


Matches 551 - 600 out of 2,962

Document Document Title
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...  
WO/2009/031083
A sensor device is described being designed to detect the phasetransition ofat least a part of a test material from the solid phase to the liquid phase. The sensor device comprises a light source (1) for initiating the phase transition f...  
WO/2009/028913
A safety landing apparatus for an aircraft is disclosed, which allows an airplane to land in safe on a runway in case that an emergency landing is inevitable. The safety landing apparatus for an aircraft is configured to minimize a frict...  
WO/2009/022349
A system (10) for launching aircraft (11) actuated by deflagration of anaerobic fuel is disclosed. The system comprises at least one cylinder (19) and reciprocating piston (20) accommodated therein; a plurality of fuel feeding systems (6...  
WO/2009/023342
An apparatus (10) and method for blending fluids and applying the blended fluid to a surface of an aircraft during deicing and anti-icing operations having a first tank (13), second tank (15), blend tank (22), pumps (24 - 27), conduits, ...  
WO/2009/012035
A system for supporting a hose (14) configured to deliver preconditioned air from a source to an aircraft is disclosed. The system includes a base support (24) and a stationary bearing assembly (26) connected to the base support (24) pro...  
WO/2009/012035
A system for supporting a hose (14) configured to deliver preconditioned air from a source to an aircraft is disclosed. The system includes a base support (24) and a stationary bearing assembly (26) connected to the base support (24) pro...  
WO/2009/007549
The invention relates to a device intended for a hold that can receive containers (16) and luggage (12) simultaneously. The hold is provided with a freight loading system including rollers defining a rolling surface on which a container ...  
WO/2009/007614
The invention relates to a method for the maintenance of an aircraft tank (10) including a flexible bladder (12) provided in a chamber (14) formed in the structure (16) of said aircraft, an interstitial gap (20) being provided between sa...  
WO/2009/007520
The invention relates to a securing plate (1) for removably securing a one-piece propulsion unit (17) to a wing of an aircraft, characterised in that it includes first connection means (4, 5, 8, 13, 14) for securing the plate to the wing...  
WO/2009/007520
The invention relates to a securing plate (1) for removably securing a one-piece propulsion unit (17) to a wing of an aircraft, characterised in that it includes first connection means (4, 5, 8, 13, 14) for securing the plate to the wing...  
WO/2009/007549
The invention relates to a device intended for a hold that can receive containers (16) and luggage (12) simultaneously. The hold is provided with a freight loading system including rollers defining a rolling surface on which a container ...  
WO/2009/009194
An aircraft tail number identification system for detecting, identifying, capturing, decoding, and recording pictures of all arriving and departing aircraft on airport pathways, 24 hours a day, 7 days a week, in all kind of weather.  
WO/2009/007614
The invention relates to a method for the maintenance of an aircraft tank (10) including a flexible bladder (12) provided in a chamber (14) formed in the structure (16) of said aircraft, an interstitial gap (20) being provided between sa...  
WO/2009/009194
An aircraft tail number identification system for detecting, identifying, capturing, decoding, and recording pictures of all arriving and departing aircraft on airport pathways, 24 hours a day, 7 days a week, in all kind of weather.  
WO/2009/005875
This disclosure involves aerial robots (1) that dispense conductive filament (110) or systems, methods, and software for supporting such aerial robots (1). One remotely powered aerial robot system includes an aerial robot (1) and a power...  
WO/2009/004364
A composite material elongate structural member (102), such as a spar or stringer, for use in an aerospace structure, comprises a web (108) having an angled portion, for example in the form of a chamfer (107), which joins a foot (106) of...  
WO/2009/000761
The invention relates to a method for the economic production of entire fuselage cells of airplanes and to a site for carrying out the method. Differing from the conventional sectional assembly according to the invention separate shells ...  
WO/2009/000734
This invention provides a coupling method for coupling a first (104) and a second (106) stiffening profile element for an outer skin of an aircraft or space craft. In a first step the stiffening profile elements are arranged on the outer...  
WO/2009/000734
This invention provides a coupling method for coupling a first (104) and a second (106) stiffening profile element for an outer skin of an aircraft or space craft. In a first step the stiffening profile elements are arranged on the outer...  
WO/2009/000761
The invention relates to a method for the economic production of entire fuselage cells of airplanes and to a site for carrying out the method. Differing from the conventional sectional assembly according to the invention separate shells ...  
WO/2009/000734
This invention provides a coupling method for coupling a first (104) and a second (106) stiffening profile element for an outer skin of an aircraft or space craft. In a first step the stiffening profile elements are arranged on the outer...  
WO/2009/000270
Loading device using a pendular movement for the displacement of cargo. The loading device consists of a pole (2) and a cable (6), which may be attached to a winch (5). The pole may be telescopic enabling the loading device to obtain dif...  
WO/2008/157434
Exemplary systems and methods are provided for imaging a unit under test. Orientation of an imaging system is determined with a machine vision system, a unit under test is scanned with the imaging system, and the scanned image is process...  

Matches 551 - 600 out of 2,962