CN105480426A - Self-service plane refueling technique in air - Google Patents
Self-service plane refueling technique in air Download PDFInfo
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- CN105480426A CN105480426A CN201510972239.XA CN201510972239A CN105480426A CN 105480426 A CN105480426 A CN 105480426A CN 201510972239 A CN201510972239 A CN 201510972239A CN 105480426 A CN105480426 A CN 105480426A
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- oil
- plane
- refueled
- pipe
- refueling
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D39/00—Refuelling during flight
Abstract
The invention discloses a self-service plane refueling technique in the air. The self-service plane refueling technique is performed through the following components at least consisting of a winch, a suspension rod, a suspension cable, a suspension hook, an oil pipe, an oil pump, chain cables and oil bags. While refueling is performed, a refueled plane and an oil loading transport plane fly to a scheduled airspace at the same time, a plurality of the chain cables are released from a plane belly or plane wings of the oil loading transport plane, and a plurality of special designed oil bags are hung on each of the chain cables; the flying speed of the refueled plane is regulated so that the refueled plane slowly approaches the oil bags from the rear upper side, hanging loops on the oil bags are hooked by the suspension rod which is provided with the suspension hook and extends in advance from the refueled plane, and the refueled plane is accelerated to fly forward so as to hook away the oil bags from the chain cables of the transport plane; the oil pipe extending from a fuselage of the refueled plane enters the oil bags through an explosion-proof drilling head; the oil pump on the refueled plane is started to pump fuel oil in the oil bags to an oil tank on the refueled plane; then the empty oil bags are abandoned, the suspension rod, the suspension cable, and the oil pipe are taken back, and one self-service refueling task is completed; second or more refueling operations can be performed operated if needed.
Description
Technical field
The invention belongs to Aircraft Air oiling technical field, be specifically related to a kind of Aircraft Air self-service refueling technology.
Background technology
In modern war, the effect that air force plays is more and more outstanding, for this reason, countries in the world all researching and developing energetically, the New Fighter of production various uses; In numerous performance perameters of opportunity of combat, combat radius and flying power are one of important indicators weighing opportunity of combat and even air operation ability, for improving the combat radius of aircraft, people always increase the fuel load of aircraft as much as possible, but excessive oil plant load, must to sacrifice other performances of aircraft for cost for example minimizing bomb load, although adopt various measures, once the voyage of fully loaded oil is also limited, in order to the combat duty of executive chairman's distance, still have to the supplementary fuel oil that lands in midway, result causes temporal delaying, and sometimes even bungles the chance of winning a battle.
In order to solve this kind of problem, people have invented again tanker aircraft, achieve the object of the supplementary fuel oil that do not land.Research shows, through an air refuelling, the combat radius of bomber can increase by 25 ~ 30%; The combat radius of fighter plane can increase by 30 ~ 40%; The voyage of transport plane almost can double.If implement repeatedly air refuelling, operational aircraft just can realize extra long distance flight and even circumaviation, thus greatly extends battle line, realizes Global Strike task.In addition, tanker aircraft has been had, just can by bomber, the landing Airport Authority (AA) of the heavy airplanes such as early warning plane is deployed to the place comparatively, greatly reduces chance under fire, and alleviates the pressure on airport, front.The use of tanker aircraft can make aircraft carry bullet to greatest extent, thus improves fighting efficiency; In addition, at the aircraft of plateau and hot area's activity, can air refuelling be relied on, reduce fuel load, to improve its hover performance and to improve the flight safety performance on complex-terrain; Patrol plane, early warning plane, scout etc. perform the aircraft of special duties, then by air refuelling, a small amount of aircraft just can complete more task.Why early warning plane can even for longer periods leave a blank for tens hours is executed the task, and mainly relies on air refuelling; To the aircraft that may have an accident because of oil starvation oil-break, carry out aerial hot refueling, it can be made to make a return voyage smoothly.
Tanker aircraft is many to be converted by large transport airplane or strategic bomber, bunkering facilities is contained in afterbody or machine underwing pod mostly, handled by aviator or oiling person. at present, tanker aircraft mainly contains KC-10 and KC-135 and Muscovite Ilyushin-78 type of the U.S.. at present, about 700 frame fuel chargers of U.S. air force equipment, can ensure that its more than 600 frame strategic bomber and 1000 multi rack fighter planes go to sea operation simultaneously.Domestic tanker aircraft research and development are started late, and current fuel charger quantity is few, and one time volume read-out is less, far can not meet the requirement of highlight lines air battle.
The flexible pipe that current fuel charger extensively adopts mode of refueling once can only be refueled to three airplanes at most, docking operation is larger by aerial airflow influence, although refueling time is long. hard tube mode of refueling adds speed oil and once can only refuel to an airplane soon, there is refueled aircraft accompanying flying queuing phenomena, for no reason add oil consumption.More importantly, no matter flexible pipe hard tube, this mode of refueling by transport pipe, harsh to the requirement of oil transporting appliance, need to carry out a large amount of training on operations to the operating personal of fuel charger and refueled aircraft, take time and effort, air draught fast changing during practical operation makes refueling process very dangerous, and risk of refueling in the spatial domain breaking out war is larger.
In view of the situation, the present invention devises a kind of aerial self-service refueling mode, only need can complete the task of postcombustion under the cooperation of common year oily transport plane, its principle is in oiling spatial domain, carry oily transport plane and discharge several chain cable from ventral or wing, the several custom-designed oil sac of carry on every root chain cable, refueled aircraft adjustment flying speed is slowly from behind close to oil sac, the suspension rod of band suspension hook is stretched out from the fuselage of refueled aircraft, the chain cable of oil sac from transport plane is risen to the bait away, then the oil pipe that refueled aircraft fuselage stretches out utilizes the explosion-proof drill head on top to enter oil sac, fuel oil in capsule is extracted in machine top tank by the oil pump started on refueled aircraft, then sky oil sac is abandoned, regain oil pipe, complete self-service refueling task, second time or more time refueling operation can be carried out again if needed.
Summary of the invention
Technical matters to be solved by this invention is to provide a kind of simple and reliable, processing ease and utilizes common year oily transport plane can complete the Aircraft Air self-service refueling technology of refueling mission.
A kind of Aircraft Air self-service refueling technology, is at least made up of following a few part: winch, suspension rod, hoist cable, suspension hook, oil pipe, oil pump, chain cable and oil sac.
During oiling, refueled aircraft and carry an oily transport plane and to fly to designated flying zone; Several chain cable hanging oil sac is discharged from the ventral or wing of transport plane; Refueled aircraft from back upper place slowly close to oil sac, stretch out from fuselage and tie up the suspension rod of hoist cable and suspension hook, oil sac is hung on hoist cable after the chain cable of transport plane hooks up, startup winch tightens up hoist cable makes oil sac close to fuselage, then oil pipe is stretched out, utilize the explosion-proof drill head on oil pipe top to enter oil sac, start oil pump and fuel oil in capsule is extracted in machine top tank; Abandon sky oil sac, regain suspension rod, hoist cable and oil pipe, complete once aerial self-service refueling operation, second time or more time refueling operation can be carried out if needed again.
Described suspension rod can be any one in high strength stainless steel pipe, aluminium-alloy pipe, carbon fiber pipe and carbon fiber rod, and suspension rod can stretch, and suspension rod and hoist cable are held together, even if suspension rod ruptures after hooking up oil sac also do not affect refueling operation.
Described hoist cable be have in high-tensile steel rope, nylon rope, carbon fiber rope and ultra-high molecular weight polyethylene rope any one; Ining succession suspension hook in one end of hoist cable, and ties up on suspension rod, and the other end is connected on winch.
Described suspension hook is made up of the alloy steel of high strength or other non-metallic material such as polyformaldehyde resin, band automatic open close function; Suspension hook is connected in the top of hoist cable.
The rigid circular pipe that described oil pipe is corrosion-resistant stainless steel pipe or is made up of other composite material; Explosion-proof drill head is equipped with on the top of oil pipe; The pipe wall of contiguous drill bit there is several oil-sucking hole; The other end of oil pipe is connected with oil pump by flexible pipe.
Described chain cable is that high strength alloy steel or composite material are made, and is fixed on and carries on the wing of oily transport plane or ventral, can discharge and withdrawal; On chain link, carry is with the oil sac of rigging, multiple oil sac can compartment simultaneously carry on chain cable; Described oil sac shape is with cylinder or spheroid, is made up of multiple layers of different materials.
Further, described oil sac there are crotch and rigging thereof, are used for hanging on chain cable; Also there is three-dimensional link, hook up for refueled aircraft suspension hook; Oil sac and link are all coated with fluorescent material, but fluorescent material color is different.
Described a kind of Aircraft Air self-service refueling technology, its refueling mission is by carrying the aerial transfer mode of oil sac between oily transport plane and refueled aircraft, completes by refueled aircraft is self-service.
Further, a described year oily transport plane can be that large transport airplane is reequiped specially, also can be served as by conventional transport, bomber or fighter plane temporarily.
Beneficial effect of the present invention is: 1) breaching air refuelling must, by the Traditional Thinking of Cemented filling, adopt the aerial transmission of oil sac to complete refueling mission; 2) oil sac carry is on chain cable, and refueled aircraft, with to getting, accelerates speed oil greatly, avoids the phenomenon that accompanying flying queuing is refueled, decreases unnecessary oil consumption; 3) refueling operation is simple, occurs that unexpected probability is very low, can realize the air refuelling under complicated meteorology; 4) only with conventional transport plane even fighter plane can complete flight-refueled task, and without the need to researching and developing the tanker aircraft of transformation specially, be particularly suitable for minority or fragmentary air refueling mission; 5) because fuel charger quantity reduces in a large number and various opportunity of combat quantity for the protection of fuel charger reduce, and can save a large amount of convoy opportunities of combat lower flood tide fuel oil and be used for a line operation, that greatly improves fuel oil utilizes usefulness, saving war cost.
Accompanying drawing explanation
Fig. 1 is chain cable and upper oil sac schematic diagram thereof.
Fig. 2 is oil sac schematic diagram.
Detailed description of the invention
Below in conjunction with embodiment, this patent is further described.
The present invention is at least made up of winch 1, suspension rod 2, hoist cable 3, suspension hook 4, oil pipe 5, oil pump 6, chain cable 7 and oil sac 8.
When aircraft execute the task way in send the alarm of Low oil Fuel time, immediately call out command centre send carry an oily transport plane, after obtaining instruction, refueled aircraft and carry an oily transport plane fly to designated flying zone simultaneously; The operating personal of transport plane is discharged from ventral and wing by the chain cable 7 of hydraulic actuator by carry oil sac 8, and chain cable 7 and oil sac are in the effect declivity back lower place random flight of 8 air-flows and gravity; The refueled aircraft adjustment speed of a ship or plane, from the back upper place of transport plane slowly close to oil sac 8, stretch out from fuselage and tie up the suspension rod 2 of hoist cable 3 and suspension hook 4, oil sac 8 is hooked up from the chain cable 7 of transport plane and is hung on hoist cable 3, the winch 1 started on machine tightens up hoist cable 3 makes oil sac 8 close to fuselage, then stretch out oil pipe 5, utilize the explosion-proof drill head on oil pipe 5 top to enter oil sac 8, start oil pump 6 and fuel oil in capsule is extracted in machine top tank; Abandon sky oil sac 8, regain suspension rod 2, hoist cable 3 and oil pipe 5, complete once aerial self-service refueling operation, second time or more time refueling operation can be carried out by above program if needed.
Above embodiment just one of preferred embodiment; to make those skilled in the art understand the present invention better; unintelligible is restriction to right protection scope of the present invention; on the contrary; for the common scientific research personnel of this area; the change of any unsubstantiality that all the present invention of utilization carry out or adjustment, all should fall within protection scope of the present invention.
Claims (10)
1. an Aircraft Air self-service refueling technology, is characterized in that, is at least made up of following a few part: winch, suspension rod, hoist cable, suspension hook, oil pipe, oil pump, chain cable and oil sac; During oiling, refueled aircraft and carry an oily transport plane and to fly to designated flying zone; Several chain cable hanging oil sac is discharged from the ventral or wing of transport plane; Refueled aircraft from back upper place slowly close to oil sac, stretch out from fuselage and tie up the suspension rod of hoist cable and suspension hook, oil sac is flown away from transport plane from the getting of rising to the bait of the chain cable of transport plane in hoist cable, start winch to tighten up hoist cable and make oil sac close to fuselage, then oil pipe is stretched out, utilize the explosion-proof drill head on oil pipe top to enter oil sac, start oil pump and fuel oil is extracted in machine top tank; Abandon empty oil sac, regain suspension rod, hoist cable and oil pipe, complete once aerial self-service refueling operation, second time or more time refueling operation can be carried out if needed again.
2. a kind of Aircraft Air self-service refueling technology according to claim 1, it is characterized in that, described suspension rod can be any one in high strength stainless steel pipe, aluminium-alloy pipe, carbon fiber pipe and carbon fiber rod, suspension rod can stretch, suspension rod and hoist cable are held together, and also do not affect refueling operation even if rupture after hooking up oil sac.
3. a kind of Aircraft Air self-service refueling technology according to claim 1, is characterized in that, described hoist cable be have in high-tensile steel rope, nylon rope, carbon fiber rope and ultra-high molecular weight polyethylene rope any one; Ining succession suspension hook in one end of hoist cable, and ties up on suspension rod, and the other end is connected on winch.
4. a kind of Aircraft Air self-service refueling technology according to claim 1, is characterized in that, described suspension hook is made up of the alloy steel of high strength or other non-metallic material such as polyformaldehyde resin, band automatic open close function; Suspension hook is connected in the top of hoist cable.
5. a kind of Aircraft Air self-service refueling technology according to claim 1, is characterized in that, the rigid circular pipe that described oil pipe is corrosion-resistant stainless steel pipe or is made up of other composite material; Explosion-proof drill head is equipped with on the top of oil pipe; The pipe wall of contiguous drill bit there is several oil-sucking hole; The other end of oil pipe is connected with oil pump by flexible pipe.
6. a kind of Aircraft Air self-service refueling technology according to claim 1, is characterized in that, described chain cable is that high strength alloy steel or composite material are made, and is fixed on and refuels on the wing of transport plane or ventral, can discharge and withdrawal; On the chain of rings, carry is with the oil sac of rigging, multiple oil sac can compartment simultaneously carry on chain cable.
7. a kind of Aircraft Air self-service refueling technology according to claim 1, it is characterized in that, described oil sac shape is with cylinder or spheroid, is made up of multiple layers of different materials.
8. a kind of Aircraft Air self-service refueling technology according to claim 7, is characterized in that described oil sac having crotch and rigging thereof, is used to hang on chain cable; Also there is three-dimensional link, hook up for refueled aircraft suspension hook; Oil sac and link are all coated with fluorescent material, but fluorescent material color is different.
9. a kind of Aircraft Air self-service refueling technology according to claim 1-8, is characterized in that, refueling mission is the aerial transfer mode by oil sac, completes by refueled aircraft is self-service.
10. a kind of Aircraft Air self-service refueling technology according to claim 1-9, is characterized in that, the transport plane that refuels can be large transport airplane repacking, also can be served as by conventional transport, bomber or fighter plane temporarily.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510972239.XA CN105480426A (en) | 2015-12-22 | 2015-12-22 | Self-service plane refueling technique in air |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510972239.XA CN105480426A (en) | 2015-12-22 | 2015-12-22 | Self-service plane refueling technique in air |
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| Publication Number | Publication Date |
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| CN105480426A true CN105480426A (en) | 2016-04-13 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201510972239.XA Pending CN105480426A (en) | 2015-12-22 | 2015-12-22 | Self-service plane refueling technique in air |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108674675A (en) * | 2018-05-13 | 2018-10-19 | 雷子墨 | A kind of mother and sons' tanker aircraft |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6142421A (en) * | 1998-01-13 | 2000-11-07 | Science Applications International Corporation | Vehicle refueling system |
| US20030136874A1 (en) * | 2001-12-10 | 2003-07-24 | Gjerdrum David Michael | Method for safer mid-air refueling |
| US20060202088A1 (en) * | 2003-08-14 | 2006-09-14 | Nir Padan | Apparatus and method for air-to-air arming of aerial vehicles |
| CN102847977A (en) * | 2012-09-21 | 2013-01-02 | 上海交通大学 | Drilling device of scraped automobile oil tank |
-
2015
- 2015-12-22 CN CN201510972239.XA patent/CN105480426A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6142421A (en) * | 1998-01-13 | 2000-11-07 | Science Applications International Corporation | Vehicle refueling system |
| US20030136874A1 (en) * | 2001-12-10 | 2003-07-24 | Gjerdrum David Michael | Method for safer mid-air refueling |
| US20060202088A1 (en) * | 2003-08-14 | 2006-09-14 | Nir Padan | Apparatus and method for air-to-air arming of aerial vehicles |
| CN102847977A (en) * | 2012-09-21 | 2013-01-02 | 上海交通大学 | Drilling device of scraped automobile oil tank |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108674675A (en) * | 2018-05-13 | 2018-10-19 | 雷子墨 | A kind of mother and sons' tanker aircraft |
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Application publication date: 20160413 |
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