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Patent Searching and Data


Matches 701 - 750 out of 6,077

Document Document Title
WO/2009/055219A1
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/2009/055218A3
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/2009/055353A2
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/2009/055218A2
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/2009/055353A3
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/2009/053539A1
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/2009/047825A1
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/2009/046703A1
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/2009/046503A1
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/2009/047405A3
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/2009/047405A2
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/2009/047578A1
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/2009/046933A1
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/2009/048666A3
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/2009/044004A2
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/2009/044362A3
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/2009/044362A2
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/2009/042549A2
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/2009/042549A3
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/2009/037475A1
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/2009/037465A1
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/2009/037007A1
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/2009/033221A1
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/2009/031083A1
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/2009/028913A1
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/2009/022349A1
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/2009/023342A3
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/2009/012035A3
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/2009/012035A2
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/2009/007549A3
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/2009/007614A2
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/2009/007520A3
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/2009/007520A2
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/2009/007549A2
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/2009/009194A3
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/2009/007614A3
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/2009/009194A2
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/2009/005875A2
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/2009/004364A3
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/2009/000761A4
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/2009/000734A3
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/2009/000734A4
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/2009/000761A3
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/2009/000734A2
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/2009/000270A1
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/2008/157434A1
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...  
WO/2008/154062A2
Aircraft arresting beds at ends of runways may be subject to damaging effects of jet blast phenomena. Arresting units for that and other applications and which are resistant to such effects are described, with related methods.  
WO/2008/154062A3
Aircraft arresting beds at ends of runways may be subject to damaging effects of jet blast phenomena. Arresting units for that and other applications and which are resistant to such effects are described, with related methods.  
WO/2008/150700A2
Methods and systems for fabricating a composite structure are provided. The method (400,500,600) includes receiving data representing a portion of a surface (312) of the structure, measuring a surface of the structure, the measured surfa...  
WO/2008/147681A2
An unmanned aerial vehicle (UAV) is launched and recovered using a UAV management system. The UAV is stored in a magazine and moved from the magazine during a launch operation and to the magazine during a recovery operation.  

Matches 701 - 750 out of 6,077