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Patent Searching and Data


Matches 201 - 237 out of 237

Document Document Title
JP4695649B2  
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...  
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...  
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...  
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...  
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...  
JP4289795B2  
JP4176718B2  
JP2008531377A
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...  
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 ...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
JP3098036B2  
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...  
JPH08507030A
(57) The lamp system (10) of the 1st case of the operation of a summary has the front lamp classification (12) and back lamp classification (14) which were linked by the spindle (24) so that both pitch movement and roll movement might be...  
JPH072190A
PURPOSE: To perform lower-cost and more rapid air transportation with a large quantity, to provide advantages for enviromnent protection, and to reduce an amount of consumed fuel by using an automatic inflight refueling airplane at a dis...  
JPH05193588A
PURPOSE: To eliminate the need for installing complex and costly automated systems in an unmanned aircraft to be refueled by providing apparatuses, by which a manned in-flight refueling aircraft performs the rendezvous and probe- drogue ...  
JPH0211494A
PURPOSE: To carry out smooth refueling and to miniaturize a device by providing a reel winding a line member around it in the inside of a refueling system main body free to rotate and providing a means to put the line member in and out b...  
JPS6456299A
PURPOSE: To accomplish refueling safely by diffusing to the rear a plurality of frequency waves from a microwave landing gear provided on the tail end of a tanker aircraft to an aircraft to be refueled so that frequency waves may not be ...  
JPS579830B2  
JPS5668464A  
JPS54127024A  
JPS54104756U  
JPS5461800A  
JPS5346720Y2  
JPS53121400A  
JPS5120791B1  
JPS5175000U  
JPS5141899U  
JPS5025240B1  
JPS4829356B1  

Matches 201 - 237 out of 237