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Patent Searching and Data


Matches 701 - 750 out of 3,022

Document Document Title
WO/2008/027458
An undercarriage wheel is disclosed comprising an axle member that supports a drive member, for example but not limited to a compact high torque electric motor, a wheel member driven by said drive member, and a tire attached to the wheel...  
WO/2008/025940
A mobile aeroengine washing cart (50) , and a method of their operation, comprises a platform (52) having two lateral walls (64) , a front wall (62) and a drip tray (58) for capturing washing medium during an engine washing operation. Th...  
WO/2008/022977
The invention relates to the loading and unloading of items of flight luggage in an airport.  
WO/2008/020248
A rib bay platform (1) for use in an aircraft rib bay, is adjustable in length (for example it comprises two telescopically mounted sections (3, 5). The platform (1) comprises a first end (7) configured for mounting on a stringer of the ...  
WO/2008/019561
A Cable conveying apparatus for passenger bridge particularly for three-tunnel bridge is provided. The first chain conduit is provided beneath the first tunnel and includes a first chain bracket (4) and a first chain. The first chain bra...  
WO/2008/020084
A cart (100) for storage of items, such as air passenger luggage, and transport thereof between, e.g., airport sorting apparatus and aircrafts, comprises a chassis (104) and a storage sect ion (102). The storage section comprises one or ...  
WO/2008/016311
A self-powered mobile platform that is configured to be remotely wirelessly controlled, said platform including a base with a first face that is dimensioned and configured to allow a vertical landing aircraft to land and take off.  
WO/2008/015663
A system for landing UAV's comprising a slingshot structure (25) that includes a central arm (26) and an axis means (45) installed along the central arm of the structure and wherein it enables the central arm to move around it in additio...  
WO/2008/016311
A self-powered mobile platform that is configured to be remotely wirelessly controlled, said platform including a base with a first face that is dimensioned and configured to allow a vertical landing aircraft to land and take off.  
WO/2008/010159
According to the invention, a shell handling carriage (19) is provided with grippers (194) which grip the end edges of a shell (2) made of composite material still fixed to a molding drum (11). An expeller strut (13) prevents the drum (1...  
WO/2008/010159
According to the invention, a shell handling carriage (19) is provided with grippers (194) which grip the end edges of a shell (2) made of composite material still fixed to a molding drum (11). An expeller strut (13) prevents the drum (1...  
WO/2007/147210
The invention is a portable, modular stairway unit for use on a building site during construction of a multistorey building, the stairway unit including: a stair run section with a plurality of rise-separated stair treads, the stair run ...  
WO/2007/139603
An inspection system (10) includes a passenger identity verification system, a passenger screening system, and a computer (18, Fig.5) coupled to the passenger verification system and the passenger screening system, the computer configure...  
WO/2007/137812
According to an exemplary embodiment of the present invention, an improved method for assembling and/or disassembling an airplane engine unit (200), having a pylon (201) with an engine (104) and a wing (203) is provided, in which a pre-a...  
WO/2007/139603
An inspection system (10) includes a passenger identity verification system, a passenger screening system, and a computer (18, Fig.5) coupled to the passenger verification system and the passenger screening system, the computer configure...  
WO/2007/139603
An inspection system (10) includes a passenger identity verification system, a passenger screening system, and a computer (18, Fig.5) coupled to the passenger verification system and the passenger screening system, the computer configure...  
WO/2007/138366
The new technical solution meets the requirements under EU Directives and the Clean Air Act EPA/USA; by means of a closed system fuel is loaded onto the aircraft, the collected vapours from road tankers are stored in fixed tanks at the t...  
WO/2007/135103
The invention relates to an air-conditioning unit (1) comprising an air circuit with an air inlet (5), a main fan (10) and an air outlet (6) designed to be connected to a chamber such as, for example, an aircraft parked on the ground, pr...  
WO/2007/135103
The invention relates to an air-conditioning unit (1) comprising an air circuit with an air inlet (5), a main fan (10) and an air outlet (6) designed to be connected to a chamber such as, for example, an aircraft parked on the ground, pr...  
WO/2007/135318
The object of the invention is method of cutting out a damaged area from an aircraft fuselage, in particular in order to repair said damaged area, consisting in making at least one cut-out in the fuselage (20) in order to delimit a cut-o...  
WO/2007/133819
A visual navigational (100) aid for guiding the approach path of incoming aircrafts (402), ships or other vehicles. The visual navigational aid (100) comprises high intensity light emitting diodes (LEDs) (102, 104) or LED arrays and opti...  
WO/2007/132025
The device for recovering unmanned airborne vehicles comprises support means connected to the ground and retention means connected to the support means, it being possible for the device to occupy a non-operational position and an operati...  
WO/2007/134087
System and method (100) for storing energy using electromechanically active materials in micro-electromechanical systems. A preferred embodiment comprises a movable element, an intermediate layer formed under the movable element, and ele...  
WO/2007/130545
A system and methods for x-ray backscatter reverse engineering of structures. One embodiment includes a plurality of articulated arms attached to a movable base. Another embodiment includes a single counterweighted arm attached to a mova...  
WO/2007/130545
A system and methods for x-ray backscatter reverse engineering of structures. One embodiment includes a plurality of articulated arms attached to a movable base. Another embodiment includes a single counterweighted arm attached to a mova...  
WO/2007/124673
A secure system and method for aircraft emergency landing are provided. Said system includes a movable board (1), a detecting device (4), a controlling system (5) and a buffering device (2). The detecting device detects the landing locat...  
WO/2007/120266
A method of protecting luggage from tampering includes steps of receiving a piece of luggage at a baggage check-in station (1302), and encoding passenger and routing information at the baggage check-in station onto an identification tag ...  
WO/2007/120266
A method of protecting luggage from tampering includes steps of receiving a piece of luggage at a baggage check-in station (1302), and encoding passenger and routing information at the baggage check-in station onto an identification tag ...  
WO/2007/115401
A system for wirelessly controlling marker lights comprising a remote controller comprising a transmitter and one or more marker lights. Each of the marker lights comprise a receiver and processing means, and each of the marker lights ha...  
WO/2007/110566
A steering angle warning system (4) comprising a rotation-measuring unit located on an aircraft (6), and an alarm unit (19). The rotation-measuring unit is arranged to output a first signal dependent on the steering angle between a nose ...  
WO/2007/110067
The invention relates to a testing device for fuselage shells, wherein the test piece is connected to a complementary cross-sectionally U-shaped structure with legs, wherein longitudinal flanges are provided at the ends of the legs in th...  
WO/2007/110067
The invention relates to a testing device for fuselage shells, wherein the test piece is connected to a complementary cross-sectionally U-shaped structure with legs, wherein longitudinal flanges are provided at the ends of the legs in th...  
WO/2007/107180
A support serves to support loads and has at least one supporting element (2) with a docking head (3) for supporting a load (15) at a load-receiving point (16). In order to raise the unloaded support (1), a lifting element (5) is provide...  
WO/2007/108726
An aircraft docking system (115, 117) is configured to be located at a docking site (103, 105). The system comprises distance determining means configured to determine, using electromagnetic radiation signal reception means, at least a d...  
WO/2007/106741
An expansible and collapsible tubular conduit (10), which is especially- adapted for use in supplying pre-conditioned air to an aircraft while the aircraft is located upon the ground and is being serviced, comprises a plurality of annula...  
WO/2007/106741
An expansible and collapsible tubular conduit (10), which is especially- adapted for use in supplying pre-conditioned air to an aircraft while the aircraft is located upon the ground and is being serviced, comprises a plurality of annula...  
WO/2007/104807
Device that allows connection and use of a conduit for air from a supply outside an aircraft to the air intakes inside the latter, which consists basically of a small carriage, formed by a supply and channelling chamber on which housings...  
WO/2007/093442
Circuit arrangement for a navigational light device on an airport runway (10), with the navigational light device comprising guide beacons (14, 16) which are arranged in the rolling direction and are connected to a guide-beacon power sup...  
WO/2007/093212
A lifting system (1) is used for lifting loads, for example for lifting and recovering an aircraft (2) following an accident, and has a lift (6) which can be positioned underneath a load, in particular underneath a mainplane (5) of an ai...  
WO/2007/093442
Circuit arrangement for a navigational light device on an airport runway (10), with the navigational light device comprising guide beacons (14, 16) which are arranged in the rolling direction and are connected to a guide-beacon power sup...  
WO/2007/091461
A floor section (15) is formed at the rear of a vehicle body (11), at one side of it. A lifting floor device (21) having a floor body (22) lifted and lowered by a lifting drive device is placed above the vehicle body (11). The floor body...  
WO/2007/087018
A system for monitoring the free play in aircraft control surfaces includes one or more accelerometers secured in or on the aircraft control surfaces and a computer system connected to the one or more accelerometers and to one or more co...  
WO/2007/086055
The invention provides a system, method and landing device for landing an aircraft (50) with respect to a predetermined landing location (P). The aircraft is configured for powered flight at least when the parafoil (60) is deployed, and ...  
WO/2007/084172
An embodiment of the invention is directed to a system for controlling and managing a small unmanned air vehicle (UAV) between capture and launch of the UAV. The system includes an enclosure that provides environmental protection and iso...  
WO/2007/084172
An embodiment of the invention is directed to a system for controlling and managing a small unmanned air vehicle (UAV) between capture and launch of the UAV. The system includes an enclosure that provides environmental protection and iso...  
WO/2007/084101
A measuring tool for a blade cuff mounted on a rotor blade assembly includes a cam follower assembly which simulates a longitudinal profile of an ideal blade cuff within a contour plane. A cam lock locks the gauge at a desired longitudin...  
WO/2007/078473
A takeoff assist device for an air vehicle, such as an unmanned air vehicle is provided. The device features an electric motor and is much less complex and lighter than takeoff assist devices heretofore known. A body member is shaped to ...  
WO/2007/078473
A takeoff assist device for an air vehicle, such as an unmanned air vehicle is provided. The device features an electric motor and is much less complex and lighter than takeoff assist devices heretofore known. A body member is shaped to ...  
WO/2007/074013
A hazard light of types B and C in accordance with ICAO Annex 14, Table 6-3 is proposed, comprising a cylindrical supporting element (1), formed as a hollow body which is flowed through by the ambient air in the internal region provided ...  
WO/2007/074084
The invention concerns a method of dimensioning and producing stiffened structural components (4) comprising at least one shell component (6) and at least one stiffening component (8) which can be connected thereto, in which the shell co...  

Matches 701 - 750 out of 3,022