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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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JP2019166965A |
[Subject] A system which can be conveyed at a height is provided for an object, without making flight time of a drone produce restrictions. [Means for Solution] A system is provided with top drone 1 connected with object 11, cable cable ...
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JP6584743B2 |
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JP6571739B2 |
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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 |
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JP4695649B2 |
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JP2011507755A |
A command and control system (100) for vessel includes a distributed control system utilizing bi-directional fiber optics to connect a control computer to various controls, including valves, pumps, and lights. A touch screen (102) allows...
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JP2010536633A |
A system and method for refueling unmanned aerial vehicles. The system is adapted to refuel a first unmanned aerial vehicle from a second unmanned aerial vehicle and includes an arrangement for flying the first and second vehicles to pro...
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JP2010208623A |
To provide a tether continuous energy feeding system for an unmanned aircraft.The tether continuous energy feeding system has a ground station 14; a ground station energy system 16; a spool 18 connected to the ground station energy syste...
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JP2010523395A |
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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JP2009528940A |
A system for effecting automatic identifying of a receiving aircraft receiving fuel from a fuel delivery apparatus in a delivering aircraft during an airborne fueling operation includes: (a) a first unit coupled with the receiving aircra...
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JP4289795B2 |
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JP4176718B2 |
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JP2008531377A |
[Subject] A refueling probe enables it to insert into refueling ドローグ more easily. [Solution means] Air refueling system equipped with the refueling ドローグ assembly (100) containing refueling ドローグ and the refueling h...
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JP2008513279A |
The present invention relates to the equipment for connecting an airplane with the refueling equipment of an air refueling tanker, while flying. The tubular cylinder object (15) in which the supporting-structure object (9) which carries ...
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JP2008506898A |
It is the joint assembly 1 for enabling internal connection of the removal to a channel. The female coupling member 3 has the 1st end 10 配設 (ed) so that it might connect with the 1st channel, and the 2nd end equipped with the receivi...
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JP2008500927A |
Refueling ドローグ made as [connect / with the refueling hose prolonged from a refueling airplane]. This ドローグ may contain the active stabilization system made as [stabilize / refueling ドローグ / when refueling ドロー...
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JP2007515329A |
The pilot guidance light (PDL) attached to the outside of a tanker plane (10) uses a light emitting diode (LED) (213) as a light source, in order to provide the pilot of the airplane (30) which approaches with visual information. PDL can...
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JP2006103481A |
To provide a system for performing air refueling in a short time by controlling a boom and an oil feeding hose in the air refueling by using position information.The air refueling is performed from a tanker aircraft 1 to an aircraft 2 to...
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JP2005533721A |
The present invention is a hose reel drive system (10) by which the variable-capacity liquid pressure motor control of [for carrying out inflight refueling to a tanker plane from an air refueling tanker] is carried out. This system is eq...
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JP2004533958A |
Determine the position of an airplane using a navigation sensor, control an airplane automatically, and from an initial position (410, 502), The navigation guidance computer system which intersects the rendezvous orbit (208) which the cr...
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JP2002531314A |
(57) summary, for example, the probe assembly object for refueling which can be developed, is equipped with the supported proximal pipe portion (18) by flexible wearing which consists of an inner side and outside surface-of-a-sphere-like...
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JP2002517357A |
(57) The airspeed marginal performance envelope of a summary helicopter is changed into a ground speed envelope by using the speed of a wind, and direction as an element. Ground speed instructions of an unmanned helicopter are offered as...
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JP3098036B2 |
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JP2000509343A |
(57) Summary book invention relates to inflight refueling of an airplane. In order to make easy connection between the oil supply line at the rear of a tanker airplane supported by the boom which can appoint a direction, and the connecti...
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