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Patent Searching and Data


Matches 1 - 50 out of 236

Document Document Title
WO/2020/249447A1
The invention relates to a power assistance system (1) for supporting an electrically drivable aircraft (2) capable of vertical start and landing, wherein the power assistance system (1) is designed to support the aircraft (2) during asc...  
WO/2020/235161A1
Provided is an image processing system capable of detecting the location of an unmanned mobile body and measuring the timing when the unmanned mobile body passed a predetermined location. An image processing system S is provided with: ...  
WO/2020/121067A3
A metal air battery electrolyte replenishment system comprised of a base station with docking receptor apparatus and matching docking probe on a flying drone. The probe onboard the drone has a sensor that guides the drone to connect with...  
WO/2020/156931A1
The present invention relates to system for transferring a fluid from a first spacecraft to a second spacecraft, the first spacecraft comprising a fluid transfer system comprising: a pressurant supply system, a first fluid tank configure...  
WO/2020/121067A2
A metal air battery electrolyte replenishment system comprised of a base station with docking receptor apparatus and matching docking probe on a flying drone. The probe onboard the drone has a sensor that guides the drone to connect with...  
WO/2020/084291A1
A fuel hose assembly for inflight fuelling of aircraft comprises: a flexible inner tube for conveying fuel under pressure; an outer cover comprising a plurality of rigid parts; and an actuator configured to move the rigid parts lengthwis...  
WO/2020/079935A1
Provided is a flying body comprising: an antenna for forming a terrestrial communication area and providing wireless communication services to user terminals in the communication area; and an attachment/detachment unit that physically at...  
WO/2020/079934A1
Provided is a control apparatus controlling a plurality of flying bodies including a first flying body which forms communication area by using a beam radiated to the ground, and includes an antenna for providing a radio communication ser...  
WO/2020/065322A1
A propellant-handling module for installation in a host aircraft comprises: a motorised drum unit comprising a line and drogue for engagement with a propellant supply line of a propellant supply aircraft and for drawing the propellant su...  
WO/2020/065271A1
A method of operating a supply aircraft for in-flight recharging comprises: transmitting a deploy command signal from a communication unit of the supply aircraft to a communication unit of a receiver aircraft, to cause a line and drogue ...  
WO/2020/065247A1
A method of operating a fuel tanker aircraft for in-flight fuelling comprises: transmitting a deploy command signal from a communication unit of the tanker aircraft to a communication unit of a fuel receiver aircraft, to cause a line and...  
WO/2020/028118A1
Systems, apparatuses, and methods are provided herein for charging an unmanned aerial vehicle (UAV) in flight. A method comprises controlling motions of a UAV via a locomotion system, wherein the UAV comprises a charging antenna coupled ...  
WO/2019/208440A1
The present invention relates to a fire extinguishing system for carrying the nozzle of a fire hose connected to a drone to a high place. The fire extinguishing system comprises: a fire hose (10) having a nozzle (11) for spraying a fire ...  
WO/2018/182577A8
A computer that includes a processor and memory which stores instructions executable by the processor. The instructions include: initiate, from a vehicle, a fuel delivery request for fuel delivery by an unmanned aerial vehicle (UAV); in ...  
WO/2019/137919A1
A flow booster for optimizing flow of fuel passing into an aircraft. The flow booster includes a fuel intake fluidly coupled to the fuel circuit, and includes a housing and a piston. The piston has a piston head slidably movable in the h...  
WO/2019/035080A1
A system and method for distributing power to racing aircraft systems is provided. The system includes a race course, a power transmitter directed towards a power delivery section of the race course, the power transmitter configured to r...  
WO/2019/012523A1
Computerized system and method of controlling a refueling device including, when the device is in a non-engaged state: receiving a first roll angle of a tanker, determining a first desired roll angle, and providing a command for controll...  
WO/2018/235071A1
A method for controlling maneuver of a refueling device, that includes: a refueling device is attached by a hose to a component of an aircraft. That component maintains a reference force on the hose. The desired position and current posi...  
WO/2018/218321A1
Cargo aircraft having a cargo ramp and cargo door oppositely hinged relative to one another to allow access to the aircraft's cargo space may be provided with a flying boom mast that is physically mounted at the aft portion of the fusela...  
WO/2018/190944A1
Capture assemblies and compliant extension assemblies may be utilized for insertion into a nozzle of a liquid engine of a spacecraft. The capture assembly may include an apparatus such as a probe for insertion into the nozzle and an asse...  
WO/2018/182577A1
A computer that includes a processor and memory which stores instructions executable by the processor. The instructions include: initiate, from a vehicle, a fuel delivery request for fuel delivery by an unmanned aerial vehicle (UAV); in ...  
WO/2018/182576A1
A system that includes a vehicle fuel-receiver comprising a port located on a vehicle surface; and an onboard computer programmed to: send a fuel delivery request to an unmanned aerial vehicle (UAV); actuate the port to permit the UAV to...  
WO/2018/142925A1
An in-flight battery changing method for multicopters according to an aspect of the present invention is provided with: a first step of securing a supply path for supplying a battery between both multicopters while both a supply-side mul...  
WO/2018/105054A1
The purpose of the present invention is to efficiently supply power to a power storage device (battery 260), and efficiently and safely deliver goods when goods are being transported by an unmanned flying body 3. The unmanned flying body...  
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/2015/026436A3
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/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/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/2014/204539A1
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/2014/133632A3
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/2014/170635A1
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/2014/096144A1
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/2013/102906A3
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/2013/102903A3
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...  

Matches 1 - 50 out of 236