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Patent Searching and Data


Matches 701 - 750 out of 6,061

Document Document Title
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.  
WO/2008/147681A3
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.  
WO/2008/146034A3
A method of manufacturing a stiffened panel, and a datum part (10) for use in such a method. The method comprises: holding the panel with a jig (4); holding a datum part with the jig; engaging the panel and the datum part with a stringer...  
WO/2008/146034A2
A method of manufacturing a stiffened panel, and a datum part (10) for use in such a method. The method comprises: holding the panel with a jig (4); holding a datum part with the jig; engaging the panel and the datum part with a stringer...  
WO/2008/147630A1
A method of replacing an existing part or parts on a structure such as an aircraft. The structure is inducted for modification. An existing part is removed and a new part is temporarily installed. Hole locations are digitally transferred...  
WO/2008/138041A1
A modular, temporary and portable staircase assembly comprising at least one stair section and at least one landing platform. The landing platform has multiple attachment points thereon, which are adapted to releasably engage with the st...  
WO/2008/138135A1
The invention provides systems to optimize the heat being transferred from a gaseous heat carrier to a contaminated surface. The invention also provides Retraction/Deployment System to facilitate the transportation of delivery heads.  
WO/2008/139440A2
A towbarless airplane tug including a chassis mounted on a plurality of tug wheels, a base assembly, an airplane nose wheel support turret assembly, rotatably mounted on the base assembly, for supporting wheels of nose landing gear of an...  
WO/2008/139437A4
A method for transferring airplanes and an unmanned airplane transfer system. The airplane transferring system includes: receiving a transfer signal responsive of a movement of an airplane control component; and transferring an airplane,...  
WO/2008/139437A1
A method for transferring airplanes and an unmanned airplane transfer system. The airplane transferring system includes: receiving a transfer signal responsive of a movement of an airplane control component; and transferring an airplane,...  
WO/2008/132297A2
The invention relates to a rear nacelle structure (1) for a jet engine, such as a thrust reverser, comprising: a front frame (25), an inner structure (15) which can move between an operating position and an intermediate maintenance posit...  
WO/2008/128026A1
A system and method are provided for retrofitting a fluorescent lighting system, for example a passenger cabin fluorescent lighting system on a vehicle such as an aircraft. The present system may include at least one LED lighting unit fo...  
WO/2008/123806A1
A system for mixing and pumping deicing fluid, comprising a water tank connected to a water flow meter, which water flow meter is further connected to a water mixing valve, which water mixing valve is further connected to one of two inpu...  
WO/2008/123807A1
A vehicle for de-icing of aircrafts comprising a vehicle chassis unit (105) carrying a crane unit (108), said crane unit (108) comprising an extendable boom (110) being erectable, the boom being provided with a cabin (115) for an operato...  
WO/2008/118633A2
A system (12) for measuring parameters at a plurality of loci associated with an aircraft includes: (a) a central unit (14); (b) a plurality of communicating nodes (16n) coupled with the central unit; and (c) a respective plurality of se...  
WO/2008/116965A1
A telescopic passenger or a goods transportation bridge (2, 3) of a vehicle (1) which can be moved to a doorway of a vehicle which bridge has at least one support pillar (7) which is fixed to the ground which supports said bridge in such...  
WO/2008/116976A1
The invention relates to a device for detecting the passage of objects (1, 2), persons or animals with a radio-frequency identification (RFID) label (3, 4), characterised in that it comprises at least one mobile support (5, 5a, 5b, 5c, 5...  

Matches 701 - 750 out of 6,061