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Patent Searching and Data


Matches 1 - 50 out of 195

Document Document Title
WO/2018/020077A1
The present invention relates to a device comprising a set of means for creating points of light of different sizes and colours, which together form figures intended to create a sign in front of the eyes of a driver or operator, in order...  
WO/2017/182686A1
The invention relates to a system for detecting the tip of the pole of the flying boom of a tanker and the mouth of the receptacle of a receiver, for semiautomatic or automatic contact for in-flight refuelling with a boom, ensuring that ...  
WO/2017/178683A1
In operations that require a 3-D view and need a global view of a work area when it is advisable to have an enlarged view of a part of said area, having two pairs of cameras, one pair being stationary and the other being moveable and con...  
WO/2017/139730A1
An aerial refueling system for refueling a receiver aircraft in flight comprises a hose reel assembly mounted onto a fuel supply aircraft's fuselage. The hose reel assembly has a rotatable drum defined by an outside diameter. A hose is w...  
WO/2017/093584A1
The invention relates to a system for detecting the tip of the pole of the flying boom of a tanker plane and the mouth of the receptacle of the receiver for semiautomatic or automatic contact for refuelling during flight with a boom, whi...  
WO/2017/066607A1
A system including a coupling (100) configured to couple a hose associated with a tanker aircraft to a nozzle associated with a receiving aircraft. The coupling may include a housing that houses a main poppet and a pilot poppet. The main...  
WO/2017/051056A1
The invention relates to a haptic augmented reality device for facilitating actions to control a boom in full flight, allowing the boom to be controlled with a single hand, without the need for any training in what the manoeuvres refer t...  
WO/2017/051057A1
The invention relates to a position-finding system comprising means for locating the position of the receiver, and means for locating the position of the end of the boom, which allow the exact determination of the positions and inclines ...  
WO/2016/181116A1
Disclosed is a data transfer method comprising: performing a refuelling process including receiving, by an aircraft (104), aircraft fuel from a first entity (for example, a tanker aircraft (102)), the first entity being remote from the a...  
WO/2016/181117A1
AIRCRAFT COUPLING METHOD AND SYSTEM Disclosed is a method and apparatus for physically coupling together a first aircraft (102) and a second aircraft (104), for example for the purpose of performing air-to-air refuelling. The first aircr...  
WO/2016/065343A1
An unmanned aerial vehicle (UAV) that includes a light and a cooling system is described. The light fitted to the UAV may be bright since heat it generates will be cooled by thermal conduction, convection and/or heat absorption. The ligh...  
WO/2015/136138A1
The invention relates to a system for obtaining a continuous image of the environment of an operation such as that of in-flight refuelling, using a camera (8) (or two in the case of a redundant system being required, since the geometry o...  
WO/2015/136139A1
The subject matter of the present patent is a complete or global monitoring and illumination system installed externally on a single point on the aircraft, on a platform that would be called the "base platform", which includes all the li...  
WO/2015/126320A1
Device (100) for achieving a temporary connection between two objects (101,102) which are movable relative to each other, comprising • respective connecting means (114,154), being brought together in order to jointly establish said con...  
WO/2015/057832A1
A motor vehicle system includes a motor vehicle including an aircraft landing portion, and an actively propelled unmanned aircraft configured to be supported on the aircraft landing portion. The vehicle and aircraft are configured such t...  
WO/2015/047632A1
An aerial refueling assembly includes, for example, a pressure transducer (260), a processor (230), and one or more light sources (200). The processor (230) is coupled to the pressure transducer (260). The one or more light sources (200)...  
WO/2015/026436A2
A refueling coupling regulator assembly including a housing forming a fluid path. A first stage pressure regulator may be provided within the housing, and may be operable between an un-modulated position and a modulated position to regul...  
WO/2015/026436A3
A refueling coupling regulator assembly (10) including a housing (12) forming a fluid path (24). A first stage pressure regulator (30) may be provided within the housing (12), and may be operable between an un-modulated position and a mo...  
WO/2014/204539A1
A refueling system may include a refueling hose (220) and a refueling drone (240) coupled to the hose aft end (224). The refueling drone (240) may be rearwardly deployable from the tanker aircraft such that the refueling drone (240) is t...  
WO/2014/170635A1
A reception coupling (6) for air-to-air refuelling. The reception coupling has a main body (17') and a fuel passage (28). A movable valve member (32) is provided for opening and closing the fuel passage. The reception coupling has a cham...  
WO/2014/133632A3
An in flight refueling probe 20 for an aircraft includes a circular shaped hollow tubular member 22, 31, 46 having a first end attached to the aircraft and a second end extending from the aircraft terminating in an external convex shape ...  
WO/2014/133632A4
An in flight refueling probe 20 for an aircraft includes a circular shaped hollow tubular member 22, 31, 46 having a first end attached to the aircraft and a second end extending from the aircraft terminating in an external convex shape ...  
WO/2014/096144A1
The subject of the invention is a system for recharging the batteries (6) carried on board an electrically powered aircraft (10), characterized in that it comprises a charging aircraft (1), means (2, 3a, 3b, 4) of temporarily electricall...  
WO/2014/043789A1
An aircraft comprising a hydrogen-containing envelope, a water-collection system for collecting water from the envelope, an electrolyser to convert the water collected using the water-collection system into hydrogen, and a hydrogen- repl...  
WO/2013/153549A1
A refueling airplane converted from a non-refueling airplane having an original tail section and an original tail-strike pitch attitude. The refueling airplane comprises the original tail section and a recess formed therein, both constit...  
WO/2013/153356A1
The invention is directed to a liquid dispensing system (10) comprising a container (11) having an aperture. A feed plug (12) is configured to fit into the aperture, said feed plug (12) defining a fluid passage therethrough and having me...  
WO/2013/102906A2
A variety of refueling devices, systems and methods are disclosed for use in in-flight refueling. In one example one such device is towed by a tanker aircraft via a fuel hose at least during in-flight refueling, and has a boom member wit...  
WO/2013/102903A3
A variety of refueling devices, systems and methods are disclosed for use in in-flight refueling. In one example one such device is towed by a tanker aircraft via a fuel hose at least during in-flight refueling, and has a boom member wit...  
WO/2013/102906A3
A variety of refueling devices, systems and methods are disclosed for use in in-flight refueling. In one example one such device is towed by a tanker aircraft via a fuel hose at least during in-flight refueling, and has a boom member wit...  
WO/2013/100807A1
The invention relates to the aircraft industry field, in particular to tactical aviation aircraft providing for the detection and striking of air, above-water and land-based targets. The technical result to which the invention is dire...  
WO/2013/082719A1
Herein is disclosed a tool, system and method for refueling on-orbit spacecraft. The tool and system are configured to allow for resupply of spacecraft configured to be propelled by either a bipropellant (oxidizer and fuel) or a monoprop...  
WO/2013/071438A1
Herein is disclosed a propellant transfer system and method for refueling on-orbit spacecraft. The system and method are configured to allow for resupply of spacecraft configured to be fueled by either a bipropellant (oxidizer and fuel) ...  
WO/2013/043290A1
A refueling boom (106) is described. The refueling boom includes a non-telescoping portion (114) configured to be coupled to a fuel tanker vehicle (100) and a telescoping portion (110) that is extendable and retractable relative to the n...  
WO/2013/016173A2
An aerial refueling system utilizes the full drogue-probe coupling event as a control parameter for hose control. A variety of different types of signal sending and signal receiving devices may be used to indicate a coupling event betwee...  
WO/2013/016173A3
An aerial refueling system utilizes the full drogue-probe coupling event as a control parameter for hose control. A variety of different types of signal sending and signal receiving devices may be used to indicate a coupling event betwee...  
WO/2012/091828A2
An inlet for a ram air turbine. The inlet is positioned forward of a turbine shaft, which is configured to rotate about a portion of an object. The inlet has a fixed geometry that chokes airflow through the inlet to prevent overspeed of ...  
WO/2012/091828A3
An inlet for a ram air turbine ( 200 ). The inlet is positioned forward of a turbine shaft, which is configured to rotate about a portion of an object ( 100 ). The inlet has a fixed geometry that chokes airflow through the inlet to preve...  
WO/2012/030347A1
Methods, systems, and non-transitory computer-readable storage media are disclosed to limit movement of a boom system or other teleoperator in response to a control input. Control input is received at a controller of a boom system, where...  
WO/2012/030444A1
Apparatus and methods described herein provide for a boom/receiver- type aerial refueling system (102) having a pressure regulator (202) integrated into the system at the tanker boom nozzle (110). During refueling operations, pressure of...  
WO/2012/027029A3
An aerial refueling boom may include a refueling boom assembly (100) and a pivot assembly (102) for attaching the aerial refueling boom to a tanker aircraft (106). The refueling boom assembly includes a main boom section (126) and a holl...  
WO/2012/027035A1
An aerial refueling system has a fluid conduit (110). A plurality of actuators (120) is coupled to the fluid conduit and a refueling aircraft (102) housing the aerial refueling system (100) to move the fluid conduit in a three perpendicu...  
WO/2012/027029A2
An aerial refueling boom may include a refueling boom assembly and a pivot assembly for attaching the aerial refueling boom to a tanker aircraft. The refueling boom assembly may include a main boom section and a hollow telescoping boom s...  
WO/2012/021233A1
A braking apparatus of an aerial refueling boom system (10) is provided to reduce the likelihood of or to prevent anomalous boom extension. The braking apparatus includes a pulley (30) about which a cable (34) wraps. The pulley is config...  
WO/2011/157875A1
The invention relates to a night vision system for viewing selected objects, in order to provide improved night viewing of an object such as the refuelling device (21, 41) used in aerial refuelling operations between an aircraft tanker (...  
WO/2011/131817A3
System for providing an enhanced night vision of a scene from an observation place, such as a system for providing an enhanced night vision of the scene (15) of an aerial refuelling operation of tanker aircraft (11), the system operating...  
WO/2011/093886A1
A method and apparatus may be present for managing a hoist cable (340) for a refueling boom (316) for an aircraft (301). A position (332) of the refueling boom (316) for the aircraft (301) may be identified. A desired length (366) for th...  
WO/2011/073493A3
A telescoping tube (42) for fuel transfer operations, this tube (42) comprising a fixed part (41 ) and a moving part (40), such that this moving part (40) comprises in turn means for dynamic sealing (21 ) which guarantee the sealing of t...  
WO/2011/073493A2
A telescoping tube (42) for fuel transfer operations, this tube (42) comprising a fixed part (41 ) and a moving part (40), such that this moving part (40) comprises in turn means for dynamic sealing (21 ) which guarantee the sealing of t...  
WO/2011/051533A3
Control post that comprises: a seat (10) for the operator of said control post, the seat (10) comprising at least one armrest (30), and a control and command assembly, said assembly comprising a command lever (1) with controls, mechanica...  
WO/2010/118131A2
An aerial identification and fuel inventory control system is disclosed. An RFID transponder mounted on a refueling aircraft transmits an identifier identifying the refueling aircraft in proximity to a fuel delivery aircraft. Substantial...  

Matches 1 - 50 out of 195