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Patent Searching and Data


Matches 701 - 750 out of 2,962

Document Document Title
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...  
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...  
WO/2007/068949
A method is provided for preparing a first part for assembly to form an aircraft component, by applying a shim to a first surface of the first-part, the method comprising the steps of placing the first surface of the part (4) adjacent to...  
WO/2007/068499
An aircraft (1) according to the invention comprises a module carrier (2) for accommodating a plurality of module elements (3) in which in each case at least one system element is integrated, wherein the module elements and system elemen...  
WO/2007/065659
A method for reconstructing gusts and/or structural loads at aircraft, in particular passenger aircraft, characterised by the process steps: a) generating an observer on the basis of a nonlinear model of the aircraft which describes the ...  
WO/2007/061622
A modular aircraft support system (10) is disclosed. In one embodiment, the modular system (10) includes a mobile cart (14) and an air conditioning system (28) configured to provide conditioned air to an aircraft (12). The embodiment als...  
WO/2007/060018
The invention relates to a passenger terminal consisting of mobile room units (modules). In said terminal, all installations that are necessary for passenger traffic, at least for the following terminal areas: check-in, arrivals, departu...  
WO/2007/057411
The invention relates to a method for producing at least one fuselage cell of an aircraft with the following steps : at least partial production of surface protection and thermal insulation in the region of the at least one shell part, a...  
WO/2007/055709
A UAV capture system (104) is disclosed. In the illustrative embodiment, the UAV capture system is coupled to the deck (102) of a sea-faring vessel (100). The UAV capture system includes a single arresting line (306) that is supported by...  
WO/2007/055709
A UAV capture system (104) is disclosed. In the illustrative embodiment, the UAV capture system is coupled to the deck (102) of a sea-faring vessel (100). The UAV capture system includes a single arresting line (306) that is supported by...  
WO/2007/055634
A method for the transport of an aircraft, such as a transport or passenger aeroplane, on the ground after nightfall, a towing tractor being coupled to a nose wheel of the aircraft, the propulsion engines of which are shutdown, the aircr...  
WO/2007/054076
The invention relates to a method for determining an optimum runway lighting intensity based on the determination of an optimum lighting intensity for a configurable target value of the runway visual range taking into account the runway-...  
WO/2007/053156
A one-piece barrel assembly cart (10) includes a right assembly cart base (210) connected with a left assembly cart base (220) and at least three stabilizer rings (17, 18, 19) that are attached to the assembly cart base. The one-piece ba...  
WO/2007/053156
A one-piece barrel assembly cart (10) includes a right assembly cart base (210) connected with a left assembly cart base (220) and at least three stabilizer rings (17, 18, 19) that are attached to the assembly cart base. The one-piece ba...  
WO/2007/053216
A system and method for docking an airship to a mooring mast includes a thruster that is mounted to the fore end of the airship. When activated, the thruster generates a thrust vector that is substantially perpendicular to the longitudin...  
WO/2007/050310
A ground power unit that supplies electricity to an aircraft . The ground power unit may include a generator (98) coupled to a diesel piston engine (16) . A turbocharger (86) may pre-compress the air consumed by the diesel engine, and a ...  
WO/2007/048302
Running mechanism for a passenger boarding bridge and the control method thereof are provided. The running mechanism comprises a beam, two rotary supporting members and two running wheel sets, wherein each of said rotary supporting membe...  
WO/2007/050164
Remotely performed maintenance of a transportation unit such as an aircraft is disclosed, wherein the maintenance is performed utilizing a networked environment. In one implementation, a first network, located within the mobile transport...  
WO/2007/045095
A hangar structure features a roof assembly extending across an opening in the ground surface, for example as defined by an abandoned pit mine. The roof assembly defines covered and uncovered portions of the opening used as a hangar and ...  
WO/2007/044404
A portable system (8) for handling gases when treating a surface within an interior space of an object. The object has one or more openings (20a, 22) that can be used as an inlet opening (26) and one or more openings that can be used as ...  
WO/2007/042492
The invention relates to a glide-angle light for approach guidance of aircraft, comprising a housing (10) with a light outlet opening (11) in which a light channel (13) with an optical axis (O) is arranged, along which a light source (20...  
WO/2007/042491
The invention relates to a flush-mounted flashing light for approach guidance of aircraft, having a housing which has a housing pot (10) which can be inserted below ground level (F) and a housing cover (12) which covers this approximatel...  
WO/2007/042609
A telescopic passenger or freight hauling bridge (11, 12) movable into connection with the doorway of a vehicle, the bridge having at least one, on ground firmly founded supporting pillar (14), which holds up so the bridge (11, 12) that ...  
WO/2007/042770
A check-in system for receiving and transporting luggage from a passenger, comprising: a conveyor for transporting luggage, the conveyor having a top surface on which luggage is received and which extends from a front end to a rear end; ...  
WO/2007/043463
[PROBLEMS] An acceleration device capable of safely and efficiently accelerating an aircraft even it is a high-speed and heavy-weight one. [MEANS FOR SOLVING PROBLEMS] The acceleration device has a support base for supporting an aircraft...  
WO/2007/042770
A check-in system for receiving and transporting luggage from a passenger, comprising: a conveyor for transporting luggage, the conveyor having a top surface on which luggage is received and which extends from a front end to a rear end; ...  
WO/2007/041197
A method for analyzing test data from nondestructive evaluation of an aircraft (102) includes generating a model (302) of the aircraft with an inspection point (304). The aircraft (102) is mapped to the model of the aircraft (306). Then,...  
WO/2007/040448
Method for automatically docking a passenger bridge (1, 2) to an airplane (5) door (3, 4) at an airport gate, wherein the airplane is brought to and stopped in a predetermined position by contact less measurement of the distance between ...  
WO/2007/040790
A power delivery system for parked aircraft includes protective rings (20) on the power cords (18). These protective rings (20) protect the power cord jackets from wear and facilitate movement of the power cords across the ground. The ri...  
WO/2007/041197
A method for analyzing test data from nondestructive evaluation of an aircraft (102) includes generating a model (302) of the aircraft with an inspection point (304). The aircraft (102) is mapped to the model of the aircraft (306). Then,...  
WO/2007/036812
The aim of the invention is to reduce the mechanical stress to which an aircraft is exposed when decelerated during landing. For this process, a stationary device (2) produces, in the area of the landing strip (1), an electromagnetic fie...  
WO/2007/036546
The invention concerns a composite structure consisting of two outer skins (2, 3) and an inner core (1) therebetween, wherein a portion (6) of one of the outer skins (2) must be replaced, with pressure of a backing block (8) and suction....  
WO/2007/036545
The invention concerns a method whereby repair portions (6, 20, 21, 22 and 23), set through two core layers (16, 19), for example with honeycomb structure and three polymer skins (2, 3, 17) two of which being outer skins and the third an...  

Matches 701 - 750 out of 2,962