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WO/2001/067115A2 |
A flow aligned device (12, 66, 100, 122, 150, 176, 214, 234) comprises a probe or vane (12, 66, 100, 122, 150, 176, 214, 234) that will sense angle of attack of an aircraft (10, 74, 106, 124, 164, 180, 210, 231). The flow aligned device ...
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WO/2000/032470A1 |
A deployable probe arrangement, e.g. for an inflight refuelling probe, comprises a proximal tube portion (18) which is carried by a compliant mounting comprising inner and outer spherical bearing arrangements (28, 30) respectively. The o...
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WO1999064942A3 |
The airspeed limiting performance envelope of a helicopter is converted to a groundspeed envelope by factoring-in the wind speed and direction. A groundspeed command for an unmanned helicopter is provided as a function of the range to th...
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WO/1999/064942A2 |
The airspeed limiting performance envelope of a helicopter is converted to a groundspeed envelope by factoring-in the wind speed and direction. A groundspeed command for an unmanned helicopter is provided as a function of the range to th...
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WO/1998/054053A1 |
A drogue assembly (10) for in-flight refuelling includes a circumferential array of triangular support arms which carry a drogue parachute (29) which extends circumferentially around their shorter sides. Each support arm is pivoted and m...
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WO/1998/046484A1 |
An apparatus includes a unitary hollow device (70) for covering sources (96, 97, 98) of lightwave energy and portable directional receivers (95) which convert infrared signals emitted from the source (96, 97, 98) to intelligible communic...
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WO/1998/039208A1 |
A drogue assembly (10) comprises a circumferential array of triangular support arms (11). Each support arm (11) is pivoted and mounted on a pivot pin (21) at its apex (19) for swinging movement in a radial direction. Each juxtaposed pair...
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WO/1998/039207A1 |
A reusable rocket airplane (10) which may be utilized to launch satellites (26) and other payloads into space. The airplane may also be used for rapid surface to surface flight. The reusable rocket airplane (10) may be safely supplied wi...
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WO/1998/017874A1 |
An improved fuel transfer pump (10) is provided for relatively high flow transfer of fuel from one aircraft to another during an inflight refueling procedure, wherein the fuel transfer pump (10) includes a jet-type scavenge pump (12) for...
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WO/1998/007623A1 |
The present invention pertains to the field of aeronautics and more precisely to equipment for the in-flight refuelling of a an aircraft. This invention relates to an in-flight aircraft refuelling system that performs the autonomous sear...
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WO/1997/043180A1 |
The invention relates to aircraft in-flight refuelling. To facilitate the connection of an in-flight-refuelling line on an adjustable boom at the rear of a refuelling aircraft with a connection receptacle on an aircraft being refuelled, ...
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WO/1997/033792A1 |
A method of refuelling a cargo-carrying aircraft and a suitable refuelling system are proposed. The cargo-carrying aircraft is an aircraft with liquid-fuel engines and the tanker aircraft carries fuel for the other aircraft and transfers...
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WO/1994/018068A1 |
A ramp system (10) in a first embodiment incorporates a fore (12) and an aft (14) ramp section interconnected by a spindle (24) which permits both pitch and roll movement of the aft section relative to the fore section. The fore section ...
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WO/1993/009030A1 |
The present invention is related to a launch system for launching a payload into earth orbit. A system and a method of launching a payload into earth orbit is provided which utilizes an airframe (1) capable of flight from the earth's sur...
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WO/1993/007055A1 |
An in-flight hose-and-drogue refueling system has the capability of steering the drogue (10) using four thrusters (20, 30) which are energized by pressurized air. The system measures the drogue's 3-dimensional position relative to either...
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WO/1993/001090A1 |
A vehicle propulsion system for accelerating a vehicle (12) along a desired travel path in the atmosphere, space, or aerospace includes a trail laying device (10) for laying a trail of fuel (14, 16) along at least part of the desired tra...
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WO/1991/006471A1 |
An in flight refueling apparatus mountable on a tanker aircraft (10) has a probe receptor (13) coupled with a fuel line (11). The receptor is arranged to be deployed outboard of the aircraft and can be provided on a drogue (12) or a boom...
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WO/1991/005703A1 |
The invention relates to the field of aeronautical drogues. The prior art aeronautical drogues require a tanker aircraft to use different drogues to enable the tanker to refuel aircraft having widely differing speeds such as helicopters ...
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JP6801949B2 |
Aerial positioning systems and methods include a Light Detection and Ranging (LIDAR) device mounted to a hub and one or more reflectors attached to a portion of an aircraft and configured to encode information scanable by the LIDAR devic...
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JP6801402B2 |
To provide an antenna direction adjustment system capable of performing advance verification with ease even at a position where installation of a directional antenna is difficult.An antenna direction adjustment system comprises: an unman...
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JPWO2019168052A1 |
[Subject] A drone with high safety is provided. [Solution] Flight means 101-1a, 101-1b, 101-2a, 101-2b, 101-3a, 101-3b, 101-4a, and 101-4b, A drone provided with flight control part 23 which works the flight means, crash judgment part 25...
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JP6714668B2 |
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...
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JP2020062918A |
To provide an air vehicle which enables electric power and a fuel to be provided between multiple air vehicles and enables intercommunication by the air vehicles integrating with/separating from each other.An air vehicle 100 is provided ...
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JP2020012810A |
To provide a system of aiding maneuvering of obscured objects.An aiding system includes a camera on a refueling aircraft 11 to obtain an image of a receiver aircraft 10 having a receptacle for refueling the receiver aircraft 10. The aidi...
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JP2020011659A |
To solve the problem in which a part of existing drones are mounted with engines but most of them are driven by batteries, generally can fly only for 15 minutes, and cannot fly a long distance.A metal thick and robust wire is stretched, ...
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JP2019166965A |
To provide a system capable of transporting an object to a high place without causing any restriction on flight time of a drone.A system includes: a top drone 1 to be connected to an object 11; a wired cable 4 connected to the top drone ...
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JP6584743B2 |
A method of projecting into space, from a first object, a plurality of modulated lines to form a grid defining a first relative reference frame, the method includes projecting polarized light having a first orientation to form a horizont...
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JP6571739B2 |
A method for transporting liquid with a UAV transport that includes docking the UAV transport with a first station and supplying the UAV transport with liquid from the first station. The UAV transport undocks from the first station and f...
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JPWO2018185939A1 |
An imaging control apparatus is provided with an acquisition part which acquires the 2nd picture contained in the 2nd image pick-up picture picturized in the state where the 1st picture contained in the 1st image pick-up picture picturiz...
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JP6492065B2 |
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JP2019504798A |
The inflight-refueling system for refueling the airplane under flight is provided with the hose reel assembly object attached to the body of a fueling airplane. A hose reel assembly object has a rotation drum demarcated by the outside di...
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JP2018177195A |
To provide indications to a receiver aircraft during aerial refueling operation.In one example, an indication system includes a plurality of light sources communicatively coupled with a control system. The indication system can be used w...
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JP2018135084A |
To provide a system and a method for delivering food and medicine to a beehive.A method for transporting liquid by UAV transportation means includes: a step for docking the UAV transportation means with a first station; and a step for su...
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JP2018088622A |
To provide an antenna direction adjustment system capable of performing advance verification with ease even at a position where installation of a directional antenna is difficult.An antenna direction adjustment system comprises: an unman...
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JP2018062324A |
To provide an electric rotary blade-type unmanned aircraft of a multiple aircraft connection method that can secure electricity for work and work hours for an unmanned aircraft for work and unmanned aircrafts for supplying electricity by...
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JP6282421B2 |
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JP6215605B2 |
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JP6055181B2 |
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JP2016536184A |
An inflight-refueling assembly is provided with the following. For example, a pressure transducer, Processor, One or more light sources. A processor is combined with a pressure transducer. One or more light sources are combined with a pr...
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JP2015202860A |
To solve the problem in which conventional aerial positioning systems require expensive position determination devices and high-speed data links to allow relative position information to be calculated and communicated during aerial refue...
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JP5592394B2 |
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JP5479338B2 |
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JP2014034394A |
To provide a refueling boom control system of an aircraft whose input control is not complicated and which does not require time in training and in practicing on different types of tanker aircraft.A refueling controller 426 is configured...
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JP2014019441A |
To provide an aerial refueling controller which securely operates when necessary and does not operate when unnecessary.A refueling controller 326 is configured to receive data about a current rate of movement of a refueling boom 312 whil...
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JP5369090B2 |
A method, apparatus, and computer usable program code for planning refueling. In one advantageous embodiment, the apparatus includes an air refueling plug-in application capable of calculating air refueling routes for a formation of airc...
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JP2012140122A |
To provide a refueling drogue that provides reliable latch indication of a refueling probe.The system includes a coupling latch assembly 310 including a latch member 312 configured to matingly engage a complementary latch-receiving membe...
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JP2012112738A |
To determine a control mode from a fluctuation value of relative position posture relation between a tracking antenna loaded on a flight vehicle and a ground antenna and mutual position relation, to generate a tracking antenna target val...
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JP2012512104A |
A method and a device for managing power concerning a refueling boom are shown. Power information is received from a force sensor (326) relevant to a refueling boom. In addition to arbitrary numbers concerning a refueling boom of aerodyn...
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JP4931832B2 |
An aerial refueling system including a refueling drogue assembly (100) including a refueling drogue and a refueling hose (110) in captive relation with the refueling drogue and a drogue positioning system. The drogue positioning system i...
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JP4695649B2 |
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