CN103129745B - Carrier-borne aircraft omnidistance even acceleration mechanical traction high speed takeoff method and device - Google Patents
Carrier-borne aircraft omnidistance even acceleration mechanical traction high speed takeoff method and device Download PDFInfo
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- CN103129745B CN103129745B CN201110383169.6A CN201110383169A CN103129745B CN 103129745 B CN103129745 B CN 103129745B CN 201110383169 A CN201110383169 A CN 201110383169A CN 103129745 B CN103129745 B CN 103129745B
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/80—Energy efficient operational measures, e.g. ground operations or mission management
Abstract
The present invention relates to a kind of carrier-borne aircraft omnidistance even acceleration mechanical traction high speed takeoff method and device thereof, in order to solve, prior art help-fly energy is little, takeoff speed slow, cost high problem, and it is to use high-power winch traction carrier-borne aircraft to take off.Taking off at bow one high-power repacking winch forward traction carrier-borne aircraft, one low power universal hoist of stern reversely draws the hook system of carrier-borne aircraft adapted or reciprocal car return.The gear of a part of reduction box is removed in described repacking exactly, increases the rotating speed of cylinder；Change a major diameter cylinder.Device is to configure high-power winch belowdecks, and winch drives carrier-borne aircraft again by rope traction hook system or reciprocal car, hook system or reciprocal car.It is owing to have employed high-power independent power winch, can guarantee that the full oil of any heavy type, large aircraft, full bullet, completely fills various goods and materials and take off at a high speed, and high-quality, low cost, high speed safe and pollution-free, noiseless are taken off, and saved Fuel On Board.Having extremely low cost, few investment, high energy utilization rate, few plant equipment etc. advantage, far better than Electromagnetical ejector and steam catapult.
Description
Technical field
The present invention relates to a kind of carrier-borne aircraft take off boosting technology.Particularly relate to a kind of carrier-borne aircraft omnidistance even acceleration mechanical traction high speed takeoff method and device.
Background technology
Due to the Electromagnetical ejector of the developed countries such as Britain of the U.S. and steam catapult to launch energy little, operation principle is unreasonable, has great defect, causes carrier-borne aircraft take-off weight little, and speed is slow, it is impossible to meet the requirement that aircraft takes off at a high speed.In face of heavy and large aircraft, the most unable to do what one wishes or heavy airplane and large aircraft cannot be made normally to take off at all.The investment adding them is huge, and energy utilization rate is the lowest, and cost is the highest, R&D cycle is oversize, and volume and weight is huge, occupies the limited space of a large amount of mother ship carrier and load, defect is many, it is highly difficult to keep in repair, need to be the most uneven by the stress of substantial amounts of human and material resources, aircraft.Stress high concentration, compromises the life-span of carrier-borne aircraft fuselage, causes major part energy and is wasted, and takeoff speed is low.Aircraft, after warship, also wants falling head, forms a spill track before deck.Totally unfavorable situation passive and vulnerable to attack it is in fight.The especially high pressure-temperature boiler of steam catapult inherently a suicide big bomb, once this boiler of the projectile impacts of enemy, will ruin people and dies by warship.Absolutely proved that their operation principle is unreasonable, not science, do not reach required by all kinds of carrier-borne aircrafts light-duty, heavy, large-scale safety, do not have under conditions of any pollution and electromagnetic interference to take off at a high speed, be climbed to the purpose in hollow, high-altitude.
Summary of the invention
In order to all are light-duty, heavy, large aircraft can take off at a high speed on aircraft carrier or dreadnaught, the most quickly climb, cost can be greatly reduced again simultaneously, save the substantial amounts of energy, there is no the pollution of a large amount of steam, do not have destructive strong-electromagnetic field to disturb.For the interests of country, national dignity, the severe situation at the especially current South Sea, it is necessary to propose the application.
Present invention aim to overcome that the drawbacks described above of prior art, it is provided that a kind of carrier-borne aircraft omnidistance even acceleration mechanical traction high speed takeoff method, the invention still further relates to device for implementing the method.Launching energy due to the maximum of Electromagnetical ejector advanced in the world and only have trivial 122,000,000 Jiao, end speed only has 28-103 meter per second.Owing to its operation principle is unreasonable, not science etc. significant deficiency, it is to be doubled that to launch energy extremely difficult, the tip speed of aircraft to be improved is practically impossible to, steam launch to improve it again launch energy, its temperature and pressure have to be improved, and this is breakneck, being nearly impossible, the present invention can bring up to more than ten times of they energy existing the most completely.And, it is with great energy and at high speed, uses instead reasonably, the whole process of science does uniformly accelerated motion.The present invention method and apparatus that omnidistance even acceleration mechanical draws makes the end speed of various aircraft all can reach 120-200 meter per second.
For achieving the above object, carrier-borne aircraft of the present invention omnidistance even acceleration mechanical traction high speed takeoff method is to use high-power winch traction carrier-borne aircraft to take off.The hundreds of rice in colliery, on the deep under ground of km promote tens tons of coals every time and add the high-power winch of mine car, there is the hugest pulling force.And the lifting speed of steel wire rope can reach 5 meter per seconds.They are vertical shaft hoisting or the inclined shaft hoisting of 25 °-30 °, and type aircraft carrier deck be level or swash plate 12 ° upwarp deck, difference in height only has trivial 2-4 rice, takes off at horizontal deck: have only to overcome the frictional force of bearing, and the height at swash plate rising part only has 2--4 rice.So above two ejector is far smaller than the power of above-mentioned winch to aircraft with power necessary to run-up.If civilian powerful winch being adapted as the dynamic power machine of aircraft carrier high speed traction, guarantee that various aircraft takes off at a high speed perfectly safely by the method for low load with strong power.
As optimization, taking off at bow one high-power repacking winch forward traction carrier-borne aircraft, one low power universal hoist of stern reversely draws the hook system of carrier-borne aircraft adapted or reciprocal car return.Assembly of the invention is extremely simple, only a high-power repacking winch of bow, one low power universal hoist of stern.Only two one thick thin steel wire ropes and two eave tiles on deck.
As optimization, the gear of a part of reduction box is removed in described repacking exactly, increases the rotating speed of cylinder；Change a major diameter cylinder.Changing the swift of a diameter 3-4 rice, the function one of swift is to be greatly improved rope speed, two be steel wire rope when running up, neat being arranged in a row can be accomplished.Row's rope is only arranged, must not multiple-layer stacked together.In order to avoid stinging rope or layer of restricting.If there is stinging rope and rope falls layer and arises that by a loosening and a tightening, cannot make aircraft in uniformly accelerated motion from slow to fast, then take off to very fast high speed.Modified segment is exactly the gear removing a part of reduction box, increases the rotating speed of cylinder.
Being to configure high-power winch belowdecks for realizing the device of said method of the present invention, winch drives carrier-borne aircraft again by rope traction hook system or reciprocal car, hook system or reciprocal car.Civilian powerful winch is adapted as the dynamic power machine of aircraft carrier high speed traction, guarantees that various aircraft takes off at a high speed perfectly safely by the method for low load with strong power.Only two one thick thin steel wire ropes and two eave tiles on deck.
As optimization, taking off at bow one high-power repacking winch forward traction carrier-borne aircraft, one low power universal hoist of stern reversely draws the hook system of carrier-borne aircraft adapted or reciprocal car return.Assembly of the invention is extremely simple, only a high-power repacking winch of bow, one low power universal hoist of stern.Only two one thick thin steel wire ropes and two eave tiles on deck.
As optimization, the gear of a part of reduction box is removed in described repacking exactly, increases the rotating speed of cylinder；Change a major diameter cylinder.Universal hoist is former mature technology.Now it is desirable that rope speed is up to the high speed winch of 120-200 rice per second, it is necessary to repacking.Modified segment is exactly the gear removing a part of reduction box, increases the rotating speed of cylinder.Second changes a diameter exactly: the swift of 3-4 rice, the function of swift-be to be greatly improved rope speed, two be steel wire rope when running up, neat being arranged in a row can be accomplished.Row's rope is only arranged, must not multiple-layer stacked together.In order to avoid stinging rope or layer of restricting.If there is stinging rope and rope falls layer and arises that by a loosening and a tightening, cannot make aircraft in uniformly accelerated motion from slow to fast, then take off to very fast high speed.
As optimization, bow is high-power diesel engine or motor-driven major diameter cylinder, and cylinder drives Large-diameter Steel cord, and major diameter haulage cable is walked around the concave groove type flywheel end of bow configuration and connected traction eave tile or reciprocal car；Stern is light duty diesel engine or motor-driven major diameter cylinder, and cylinder drives minor diameter to return and draw steel wire rope, and minor diameter returns and draws steel wire rope and walk around the concave groove type flywheel of stern configuration and connect back to draw eave tile or traction eave tile or reciprocal car.
As optimization, described diameter of cylinder 3-4 rice；Described steel wire rope is only arranged in a row on cylinder, it is to avoid multiple-layer stacked is together；Described steel wire rope is the newest old steel wire rope；Described eave tile front portion is shaped with the double end of U-shaped bidentate and hooks.
As optimization, the power of described high-power diesel engine or motor is >=1000KW；Bow is fitted with V-type rope blocking plate at concave groove type flywheel, and this V-type rope blocking plate can guide major diameter haulage cable to be slipped in enegine pit when enegine pit run out of by major diameter haulage cable automatically；Described eave tile front end base portion is also shaped with connecting hole.
As optimization, the speed of described major diameter haulage cable is 120-200 meter per second；Described high-power diesel engine or motor drive major diameter cylinder by clutch；Described bow and stern are configured with sensor and advertiser and automatic control system.
So use great speed reducing ratio？Subtract with what, increase gear？It is how many？This most just must can draw parameter accurately.Because diesel engine or motor are hundreds of KW？Or 1000KW？Or more than 1000KW's？It is take off full oil, the light fighter of full bullet？In Hai Shi, large-scale bomber？Also it is equipped with the transporter of many tanks？Concrete condition is made a concrete analysis of, and many experiments just can be reached a conclusion.In a word, as long as repacking power winch has sufficiently large independent power power, required pull strength and high speed can just be obtained.The just fortunately good help-fly power of the present invention, energy, speed can be accomplished very big very big, and the two of above-mentioned world lead level kinds of ejectors, owing to they operation principles are unreasonable, not science, can not accomplish.With the clutch of power winch and brake brake rubber block, adjust hauling speed and pulling force as required.The repacking power winch (such as figure) of a 1000KW installed below in the front end of type aircraft carrier deck.Its diameter of cylinder 3-4 rice, the speed utilizing existing technology can repack steel wire rope into is 120-200 meter per second.This is Electromagnetical ejector and steam catapult, invests 100,000,000,000 dollars, may accomplish never.And the main device as the present invention only invested 600,000 yuans in one month, the easiest obtain.
After using technique scheme, the inventive method and device are owing to have employed high-power independent power winch, foregoing 1000KW or add again high-power must take with the method for low load with strong power guarantee in the 2--3 second within have sufficiently large pulling force and ensure any heavy type perfectly safely at high speed, the full oil of large aircraft, full bullet, completely fill various goods and materials to take off at a high speed, high-quality, low cost, safety, pollution-free, noiseless high speed is taken off, cycle is the 30-45 second, and save Fuel On Board, owing to independent power winch starts the most immediately, not used time hard stop, overall process only have the 30-60 second about available machine time, so the energy consumed is few, and energy conversion be kinetic energy for once.Methods and apparatus of the present invention is with extremely low cost, few investment, the R&D cycle of most 3-4 months, high energy utilization rate, and few plant equipment etc. advantage, far better than Electromagnetical ejector and steam catapult.Satisfactorily realize any carrier-borne aircraft can take off at a high speed, be climbed to the challenge in high-altitude.
Accompanying drawing explanation
Fig. 1 is that apparatus of the present invention are taken off the structural representation of original state；
Fig. 2 is that apparatus of the present invention are taken off the structural representation of end state；
Fig. 3 is the structural representation drawing eave tile in apparatus of the present invention；
Fig. 4 is the structural representation returning in apparatus of the present invention and drawing eave tile；
Fig. 5 is the main TV structure schematic diagram that apparatus of the present invention middle front part is shaped with the double end traction eave tile of U-shaped bidentate；
Fig. 6 is the side-looking structural representation that apparatus of the present invention middle front part is shaped with the double end traction eave tile of U-shaped bidentate；
Fig. 7 is the structural representation of V-type rope blocking plate part in apparatus of the present invention.
Detailed description of the invention
Carrier-borne aircraft of the present invention omnidistance even acceleration mechanical traction high speed takeoff method is to use high-power winch traction carrier-borne aircraft to take off.Taking off at bow one high-power repacking winch forward traction carrier-borne aircraft, one low power universal hoist of stern reversely draws the hook system of carrier-borne aircraft adapted or reciprocal car return.The gear of a part of reduction box is removed in described repacking exactly, increases the rotating speed of cylinder；Change a major diameter cylinder.
As it can be seen, be at 4 times, deck configuration high-power winch 2 for realizing the device of the method for the invention, winch drives carrier-borne aircraft 1 again by rope traction hook system or reciprocal car, hook system or reciprocal car.
Specifically: take off at bow one high-power repacking winch 2 forward traction carrier-borne aircraft 1, the low power universal hoist 9 of stern one reversely draws the hook system of carrier-borne aircraft 1 adapted or reciprocal car return.The gear of a part of reduction box is removed in described repacking exactly, increases the rotating speed of cylinder；Change a major diameter cylinder.
More specifically: bow is high-power diesel engine or the major diameter cylinder of motor-driven diameter 3-4 rice, cylinder drives Large-diameter Steel cord 3, and major diameter haulage cable 3 is walked around bow concave groove type flywheel 5 end of bow configuration and connected traction eave tile 6；Stern is light duty diesel engine or the major diameter cylinder of motor-driven diameter 3-4 rice, and cylinder drives minor diameter to return and draw steel wire rope 10, and minor diameter returns and draws steel wire rope 10 and walk around the stern concave groove type flywheel 11 of stern configuration and connect back to draw eave tile 7.
Described steel wire rope is only arranged in a row on cylinder, it is to avoid multiple-layer stacked is together；Described steel wire rope is the newest old steel wire rope；Described traction eave tile 6 can be the anterior double end eave tile being shaped with U-shaped bidentate 61.The power of described high-power diesel engine or motor is >=1000KW；Bow is fitted with V-type rope blocking plate 16 at bow concave groove type flywheel 5, and this V-type rope blocking plate 16 can guide major diameter haulage cable 3 to be slipped in enegine pit when enegine pit run out of by major diameter haulage cable 3 automatically；Described traction eave tile 6 front end base portion is also shaped with back and draws eave tile connecting hole 60.The speed of described major diameter haulage cable 3 is 120-200 meter per second；Described high-power diesel engine or motor drive major diameter cylinder by clutch 18；Described bow and stern are configured with sensor and advertiser and automatic control system.
Operational approach is as follows: at the straight deck of aircraft carrier 4 or the repacking high-power winch 2 (front main car) of the front end 1000KW installed below upwarping deck 4, supporting 300 meters of long seizing wires, the newest steel wire rope (must not be restricted with new, because new rope to bend, the most handy, length changes, elongated, instrument can not accurately read its length.Will colliery full load run more than 300 times reciprocal roping coal (because coal mine output is big, within several days, get off just can heavy duty is reciprocal uses hundreds of secondary, do not bend, straight handy.And length no longer changes).The much help-flys to be seen of diameter are that light aerocraft can use diameter 24-26mm: the heavy filament rope using diameter 30-34mm.The universal hoist installing a 20-30KW at aircraft carrier rear end (afterbody) is 9. in position on schedule, diameter of cylinder 3-4 rice.The same main car of rope capacity is identical, and diameter wants little No. one, and specification is all filament, and purposes is at undercarriage on schedule before 3. the steel wire rope of main car returns to take off before pulling back.
Before taking off, carrier-borne aircraft 1 is the position of A point in mother ship carrier afterbody is such as figure.High-power winch 2 (front main car) is at bow B: the position of point, in the concave groove of the V-type rope blocking plate 16 bow concave groove type flywheel 5 (flywheels of central authorities) of mother ship carrier type aircraft carrier deck 4 front portion foremost, (purposes of V-type rope blocking plate 16 is when outside flywheel groove run out of at the volley by main rope to Large-diameter Steel cord 3 (main rope), can be automatically slipped in groove), main rope tightly links traction eave tile 6.Traction eave tile 6 hangs over a firm place of carrier-borne aircraft 1 nose-gear 15.If the nose-gear 15 only one of which wheel of this carrier-borne aircraft 1, then just hook the undercarriage 15 on wheel with single eave tile 6.Its tensile strength to be strengthened by the undercarriage of the aircraft that this undercarriage 15 takes off than airfield, that is for as carrier-borne aircraft, no matter it is with steam ejection, electromagnetic launch, or the whole process even acceleration mechanical traction of the present invention, an active force specialized spare part accepting help-fly must be had, to guarantee that aircraft obtains the energy of help-fly at stress action spot position.If there being the heavy airplane of two wheels below this aircraft nose landing gear, just catch on below the axle in the middle of two wheels with the anterior double end eave tile 6 being shaped with U-shaped bidentate 61 from below, up catch on two wheel jackshafts, it is therefore an objective to take off at a high speed voluntarily after carrier-borne aircraft 1 obtains at high speed double end traction eave tile 6 and steel wire rope when leaving deck can freely drop on deck 4.Want standby for takeoff, first traction eave tile 6 or double end traction eave tile 6 are caught in the middle part of carrier-borne aircraft 1 undercarriage 15, hook after being in the steel wire rope link of stern rear car on schedule, return and draw eave tile (afterwards hook) and catch on list traction eave tile or the hole of double end traction eave tile of main rope, then notify that Diesel engine that high-power winch 2 (front main car) starts in advance or motor clutch 18 control first major diameter haulage cable 3 to be critical in alignment with signal lights and signal bell simultaneously.Now carrier-borne aircraft 1 is in braking state, and the minor diameter haulage cable 10 of small-power winch 9 (rear car) being simultaneously in E point position links with the connecting hole 60 of traction eave tile 6.Now the commander of pilot or unmanned plane orders the start of a race, sends stroke and the illumination of signal lights 20 of signal bell 19 to the driver of two winches front and back simultaneously.High-power winch 2 (front main car) is when carrier-borne aircraft 1 is lighted a fire, open brake starting, carrier-borne aircraft 1 starts to take off, simultaneously, the clutch 18 of high-power winch 2 (front main winch) is the most afterburning, speed at carrier-borne aircraft 1 is zero to begin to start traction with the power of high-power winch 2 (main winch), does not just have the destructive impact force of moment, makes the speed of major diameter haulage cable 3 do uniformly accelerated motion.Will gather way from every 0.1 second, arrive to 16 meter per seconds ... 60 meter per seconds, aircraft is opened the throttle simultaneously and is full speed aheaded.The power of aircraft self just can reach 70-90 rice per second plus the even acceleration of main winch when rising and going to 100 meters, 2. front main winch starts to kill clutch 18 from these 100 meters, winch is made to be in the energy of maximum power state 1000KW, if extra-heavy duty type and large aircraft can strengthen the power of winch again, must take off at a high speed with the speed of 120-200 rice per second traction carrier-borne aircraft 1 with all strength.Within 200 meters, any aircraft, when the high speed of this high-power machinery high speed traction, adds that the power of self, the high speed of the speed that all can automatically exceed steel wire rope take off and leaves deck 4 and traction eave tile 6 and quickly climb.Now the operating room rope speed table 21 of high-power winch 2 (front main car) shows the distance of traction and the speed of steel wire rope to arrive between 120--200 meter per second to open at once the clutch 18 of high-power winch 2 (front main car), stops power.Or see to take off from periscope and leave deck 4 and will open clutch 18 immediately, stop power.Necessarily make sure to keep in mind, now must let the clutch be slipped immediately and 18 allow swift only rotate with inertia, simultaneously by brake brake rubber block 23 braking, before now single double traction eave tile 6 draws eave tile 7 same time, the minor diameter haulage cable 10 of main car major diameter haulage cable 3 rear car all can drop on deck 4 automatically, as long as the driver of the rear car of stern E point sees aircraft from periscope 22 and starts to take off and leave deck 4, must braking immediately, the swift making eave tile and front main car decelerates to stop, start small-power winch 9 (rear winch) immediately, by steel wire rope, eave tile and main rope are all withdrawn into the position taken off.Simultaneously, small-power winch 9 (rear winch) braking holds eave tile 6 and 7, make eave tile 6 or 7 and major diameter haulage cable 3 slow down, depart from and contact with undercarriage 15, continue the inertia rotation after braking makes high-power winch 2 (main winch) swift run out of steam to stop, the power of winch after starting immediately, single double traction eave tiles 6 with major diameter haulage cable 3 (main rope), it is withdrawn into the E point position before carrier-borne aircraft 1 takes off with the minor diameter haulage cable 10 of small-power winch 9 (rear winch) backward, prepares to take off next time.In Fig. 1 and Fig. 2 19 are signal bells, and 20 is signal lights, and 21 is rope speed table, and 22 is periscope, and 18 is clutch, and 23 is brake brake rubber block.If traction is full oil, the fighter plane of full bullet, on 100 meters of more runways, the self power of high rope speed pull strength and aircraft is superimposed, and this machine reaches the speed taken off the most, and automatic takeoff leaves deck.Owing to rope speed is less than the speed of aircraft, eave tile 6 and 7 all can drop on deck 4 automatically, and high-power winch 2 (main winch) must open clutch immediately, stop power, and braking, after the necessary braking in time of small-power winch 9 (rear winch), simultaneously, start small-power winch 9 returned by minor diameter draw 10 eave tiles of steel wire rope 6 and 7 and major diameter haulage cable 3 be all withdrawn into the position before taking off, again take off.
Owing to have employed high-power independent power winch, foregoing 1000KW or add again high-power must take with the method for low load with strong power guarantee in the 2--3 second within have sufficiently large pulling force and ensure any heavy type perfectly safely at high speed, the full oil of large aircraft, full bullet, completely fill various goods and materials to take off at a high speed, high-quality, low cost, safety, pollution-free, noiseless high speed is taken off, cycle is the 30-60 second, and save Fuel On Board, owing to independent power winch starts the most immediately, not used time hard stop, overall process only have the 30-60 second about available machine time, so the energy consumed is few, and energy conversion be kinetic energy for once.And aforesaid two kinds of ejectors are before take-off with substantial amounts of fuel or electric power, the substantial amounts of time goes to do homework, consumes greatly.Being the most again the conversion through energy, the shock being finally converted to moment launches kinetic energy, and energy major part has been given each position of fuselage and has been forced by unnecessary energy loss, and little to the energy that help-fly is useful, and this operation principle is unreasonable, not science.Methods and apparatus of the present invention is with extremely low cost, few investment, the R&D cycle of most 3-4 months, high energy utilization rate, and the most few plant equipment etc. advantage, far better than Electromagnetical ejector and steam catapult.Satisfactorily realize any carrier-borne aircraft can take off at a high speed, be climbed to the challenge in high-altitude.
For the ease of comparing research respective performance, the quality of feature, special using two kinds of technical data of prior art, attached as application documents adnexa.
Claims (6)
1. a carrier-borne aircraft omnidistance even acceleration mechanical traction high speed takeoff method, it is characterised in that use and draw carrier-borne aircraft with forward
Take off supported complex high-power winch traction carrier-borne aircraft take off；Carrier-borne aircraft is drawn at bow one high-power repacking winch forward
Take off, stern one and hook system or the low power general strand of reciprocal car supported complex of reversely drawing carrier-borne aircraft adapted
Car reversely draws the hook system of carrier-borne aircraft adapted or reciprocal car return；Described repacking is exactly that civilian powerful winch removes
The gear of a part of reduction box, increases the rotating speed of cylinder；Change a 3-4 rice major diameter cylinder, to realize 120-200 per second
The speed of rice traction carrier-borne aircraft with all strength takes off at a high speed.
2. for realizing the device of method described in claim 1, it is characterised in that configure high-power winch, winch belowdecks
Carrier-borne aircraft is driven again by rope traction hook system or reciprocal car, hook system or reciprocal car；Big bow one
Power repacking winch forward traction carrier-borne aircraft takes off, and one low power universal hoist of stern reversely draws the extension of carrier-borne aircraft adapted
Hook system or reciprocal car return；Described repacking is exactly the gear that civilian powerful winch removes a part of reduction box, increases
The rotating speed of cylinder；Change a 3-4 rice major diameter cylinder, to realize the speed traction carrier-borne aircraft with all strength of 120-200 rice per second
Take off at a high speed.
Device the most according to claim 2, it is characterised in that bow is high-power diesel engine or motor-driven major diameter
Cylinder, cylinder drives and takes off the Large-diameter Steel cord of supported complex with forward traction carrier-borne aircraft, and major diameter haulage cable is walked around
The concave groove type flywheel end of bow configuration connects traction eave tile or reciprocal car；Stern is light duty diesel engine or motor drives
Dynamic major diameter cylinder, cylinder drives the hook system with reversely traction carrier-borne aircraft adapted or the minor diameter of reciprocal car supported complex
Return and draw steel wire rope, minor diameter return draw steel wire rope walk around the concave groove type flywheel of stern configuration connect back to draw eave tile or traction eave tile or
The reciprocal car of person.
Device the most according to claim 3, it is characterised in that described Large-diameter Steel cord and minor diameter steel wire rope are on cylinder
Only it is arranged in a row, it is to avoid multiple-layer stacked is together；Described Large-diameter Steel cord and minor diameter steel wire rope are the newest old steel wire
Rope；Described eave tile front portion is shaped with the double end eave tile of U-shaped bidentate.
Device the most according to claim 3, it is characterised in that the power of described high-power diesel engine or motor is >=
1000KW；Bow is fitted with V-type rope blocking plate at concave groove type flywheel, and this V-type rope blocking plate can run at major diameter haulage cable
When going out enegine pit, major diameter haulage cable is automatically guided to be slipped in enegine pit；Described eave tile front end base portion is also shaped with connection
Hole.
Device the most according to claim 3, it is characterised in that the speed of described major diameter haulage cable is 120-200 rice
/ the second；Described high-power diesel engine or motor drive major diameter cylinder by clutch；Described bow and stern are configured with biography
Sensor and advertiser and automatic control system.
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| CN201110383169.6A CN103129745B (en) | 2011-11-28 | 2011-11-28 | Carrier-borne aircraft omnidistance even acceleration mechanical traction high speed takeoff method and device |
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| CN201110383169.6A CN103129745B (en) | 2011-11-28 | 2011-11-28 | Carrier-borne aircraft omnidistance even acceleration mechanical traction high speed takeoff method and device |
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| CN103129745B true CN103129745B (en) | 2016-08-03 |
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| CN104760706B (en) * | 2014-05-12 | 2017-03-15 | 葛愉成 | A kind of flywheel energy storage propulsion plant |
| EP3034410B1 (en) * | 2014-12-16 | 2017-03-01 | The Boeing Company | Take-off system and method for unmanned aerial vehicles |
| ES2657050B1 (en) * | 2016-08-30 | 2018-12-17 | Francisco Javier Porras Vila | Train gear-cone in the engine launches-aircraft of an aircraft carrier |
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2011
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2301566A (en) * | 1995-06-02 | 1996-12-11 | Airscrew Howden Ltd | Launching air vehicles or projectiles |
| CN1419508A (en) * | 2000-02-24 | 2003-05-21 | 弗雷德里克·让-皮埃尔·德莫勒 | An acceleration system |
| CN101301933A (en) * | 2007-05-11 | 2008-11-12 | 尚德敏 | Water ejector of aircraft carrier |
| CN201784808U (en) * | 2010-06-22 | 2011-04-06 | 吕铁燕 | Launching catapult for carrier-based aircraft |
| CN102120495A (en) * | 2011-04-09 | 2011-07-13 | 朱惠芬 | Ski jump carrier-based aircraft catapult and catapulting method thereof |
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| CN103129745A (en) | 2013-06-05 |
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