CN103761901A - Carrier-based aircraft pilot dynamic simulated training system - Google Patents
Carrier-based aircraft pilot dynamic simulated training system Download PDFInfo
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- CN103761901A CN103761901A CN201410034464.4A CN201410034464A CN103761901A CN 103761901 A CN103761901 A CN 103761901A CN 201410034464 A CN201410034464 A CN 201410034464A CN 103761901 A CN103761901 A CN 103761901A
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Abstract
The invention relates to a carrier-based aircraft pilot dynamic simulated training system which comprises a simulator, wherein the simulator is provided with wheels and a rotating mechanism, and the wheels of the simulator are in contact with a sliding rail. The sliding rail is provided with a lower horizontal section and a higher horizontal section, and a slope section is arranged between the lower horizontal section and the higher horizontal section. Hoisting mechanisms are arranged below the lower horizontal section and the higher horizontal section of the sliding rail respectively, traction ropes located inside the hoisting mechanisms are arranged on hoisters in a rolling mode, and the traction ropes are connected with the simulator through traction arms and traction hooks. A controlling device used for controlling the hoisting mechanisms, the rotating mechanism and the traction arms is arranged in the simulator, and a braking device is also arranged inside the simulator. The simulated training system truly simulates the takeoff and landing of a carrier-based aircraft on an aircraft carrier, the carrier-based aircraft pilot can experience the feeling of takeoff and landing of the carrier-based aircraft on the aircraft carrier, the problem that the pilot has not enough flying psychological experiment is solved, the defects that the carrier-based aircraft pilot faces lots of dangerousness in real training and cost is high are overcome, and training effect can be improved greatly.
Description
Technical field
The present invention relates to pilot's simulated training, be specifically related to a kind of ship-board aircraft pilot dynamic simulated training system.
Background technology
Powerful along with country, first aircraft carrier " Liaoning " number is on active service, and China's sea power obtains landmark development.Next will have successively second, the 3rd aircraft carrier is on active service.Aircraft carrier will form powerful fighting capacity, just must carry carrier-borne aircraft.It is crucial training a collection of high-quality carrier-borne pilot.Common common fighter-pilot will could carry out combat mission by the flight training of 500～600 hours, and carrier-borne aircraft pilot not only will complete these substances, also needs to overcome all difficulties of aircraft carrier landing, and the training time is longer, and risk is larger.
Aircraft-carrier flight deck is because environment is severe, and narrow space, trains and become dangerous, and accident rate is high, so carrier-borne aircraft pilot must train to adapt to the special environment of aircraft carrier for a long time.The key of aircraft carrier flight landing is takeoff speed, sinking speed and flight downslide angle.General flight simulator is the six degree of freedom fly simulation training in static state, can not reflect really the impression of carrier-borne aircraft key element of landing on aircraft carrier, carrier-borne aircraft pilot must constantly increase flying experience through a large amount of real flight trainings, could ensure the success ratio of landing.
Summary of the invention
The object of the present invention is to provide ship-board aircraft pilot dynamic simulated training system, the landing flight of real simulation ship-board aircraft on aircraft carrier, make ship-board aircraft pilot experience the impression of carrier-borne aircraft landing on aircraft carrier, solve the problem that ship-board aircraft pilot training's cost flight psychology high, pilot is lacked experience.
Ship-board aircraft pilot dynamic simulated training system of the present invention, comprises simulator, and its simulator arranges wheel and rotating mechanism, and the wheel of simulator contacts with slide rail; Slide rail arranges low level horizontal segment and high-order horizontal segment, between low level horizontal segment and high-order horizontal segment, is slope section; Under the low level horizontal segment of slide rail He under high-order horizontal segment, hoisting mechanism is all set, the dragrope in hoisting mechanism twists on windlass; Simulator is connected dragrope by draft arm with draw hook; The control device of controlling hoisting mechanism, rotating mechanism and draft arm is set in simulator, clamping device is also set in simulator.
For simulator is moved better, in moving process, keep stable, the present invention also further arranges simulator mobile platform, and simulator is placed on mobile platform, the rotating mechanism of simulator is arranged between simulator and mobile platform, and wheel and draft arm are all arranged under mobile platform; Power supply wheel is also set under mobile platform, and power supply wheel contacts with the power cable on slide rail; Electric device and electric control gear are also set in simulator.Here, the power cable on slide rail is taken turns electric energy to simulator is provided by power supply, and electric device can make simulator electricity start and electric drive.
In the present invention, draw hook is connected for linking up with draft arm.Make draft arm be convenient to hang up with dragrope or throw off.
In system of the present invention, slide rail is selected rail, and slide rail radical is two or four, and wheel is rubber guide wheel.
Slide rail shape is preferably I shape, and upper and lower two wheels contact respectively the both sides up and down of the upper traverse rod of I shape slide rail.Such structure is equivalent to the top rail rail clip of track to enter between upper and lower two wheels,, because there is slide rail both sides, has just realized the simulator alignment restrictions of four direction up and down meanwhile, and simulator is steadily moved along slide rail.
In order to simulate more truly the landing flight of ship-board aircraft on aircraft carrier, in system of the present invention, the angle of slope and level is 8～15 degree, and low level horizontal section length is 100～120m, and high-order horizontal section length is 100～120m, and slope section length is 40～60m.
In order to apply larger damping force when shutting down, the present invention also arranges obstruction device at the low level horizontal segment of slide rail and the end of high-order horizontal segment.During shutdown, draft arm touches this obstruction device, and obstruction device will play Intercepting effects.
In order to apply larger boosting power at block clearance time, the present invention preferably adopts spring by obstruction device.During shutdown, spring is compressed, plays Intercepting effects.And give and draft arm thrust when the compressed spring of block clearance time, bring into play booster action.
In the present invention, a side of the motor of hoisting mechanism connects flywheel by clutch coupling, and the opposite side of motor connects windlass by another clutch coupling, and flywheel and windlass are connected with respectively brake drum.
Preferably, flywheel diameter is shaft diameter 6～10 times.
As the critical component in system, the Main Function of hoisting mechanism is to make the simulator can be in a short period of time in (more than 1 second less than 2 seconds), very short distance (100～120m) at block clearance time, reaches very high speed.The ship-board aircraft start of a race that is virtually reality like reality is taken off, and will, in short 100m, make the speed of simulator reach 200km/h left and right.Equally, another Main Function of hoisting mechanism is when shutting down, to make simulator in a short period of time, in very short distance, from very high speed (200km/h left and right), reduce to zero.
For this reason, the structure that hoisting mechanism of the present invention has taked double clutch, double-brake to rouse, and taked flywheel to turn round in advance and assisted the mode of accelerating.Simulator needs block clearance time, first the clutch coupling of one side of the windlass in hoisting mechanism is unclamped, and the clutch coupling of opposite side is closed; Actuating motor, flywheel will rotate, until reach maximum (top) speed; Then the clutch coupling of flywheel one side is unclamped, flywheel is with very high speed inertial rotation afterwards; Meanwhile the clutch coupling of windlass one side is closed, motor drives windlass to rotate, and then drives dragrope to move, and finally drives simulator motion; When simulator motion reaches certain speed (due to the restriction of time, this speed does not reach maximum (top) speed certainly, also certainly low than the rotating speed of flywheel now), again the clutch coupling of flywheel one side is closed, the flywheel of inertial rotation just applies boosting power to windlass, further improve windlass rotating speed, the movement velocity of simulator is accelerated greatly, in official hour, reach the speed of regulation.Now draft arm must be thrown off with dragrope.No matter be low-level section of standby for takeoff, or prepare landing in high level section, above-mentioned shape is all the same.Only hoisting mechanism is not same set of.Here, because the diameter of flywheel is very large, therefore the inertia of flywheel is also just very large, when flywheel is issued to after maximal rate in direct motor drive, even if clutch coupling unclamps, motor is no longer given flywheel power, within very short time, flywheel relies on inertia, and its rotating speed does not just have too many reduction, still can keep very large.
When simulator need to be shut down, draft arm must hang up again with the dragrope of another set of hoisting mechanism.Two clutch couplinges of this set of hoisting mechanism are all closed, brake two brake drums simultaneously, by double-brake drum to windlass effect, make dragrope as far as possible motionless, and then give restraining function to simulator, and give effective deceleration to simulator, make it in official hour (more than 1 second less than 2 seconds) and stop.
System of the present invention, has three devices that driving force is provided: hoisting mechanism, electric device and obstruction device, so can in a short period of time the speed of simulator be brought up to required degree.Similarly, also have three devices that damping force is provided: the clamping device in hoisting mechanism, obstruction device and simulator (clamping device in simulator is for braking the wheel of simulator), so can in a short period of time the speed of simulator be reduced to zero from very high.
System of the present invention, is skillfully constructed, and can carry out circulating analog training continuously.The rotating mechanism of simulator is convenient to easily simulator be turned around after shutdown, like this, trained take off and stop after can starting again training landing.Similarly also can trained land and stop after can starting again training take off.Obstruction device can also be as roll booster in addition.Two cover hoisting mechanisms are exquisite especially, not only can accelerate, and can also slow down.And after the start of a race, the draw hook of this set of hoisting mechanism will stop at front end, until simulator, turn to and later land while shutting down, hook will tangle draft arm in this position, for slowing down, leaves enough distances.
Ship-board aircraft pilot dynamic simulated training system of the present invention, simulated truly the landing flight of ship-board aircraft on aircraft carrier, make ship-board aircraft pilot experience the impression of carrier-borne aircraft landing on aircraft carrier, solved the problem that pilot's flight psychology is lacked experience, overcome ship-board aircraft pilot and truly trained the defect that danger is large, cost is high, can greatly improve training effect.
Accompanying drawing explanation
Fig. 1 is total figure of dynamic simulated training system of the present invention;
Fig. 2 is the horizontal schematic diagram that the simulator in system of the present invention contacts with slide rail;
Fig. 3 is longitudinal schematic diagram that the simulator in system of the present invention contacts with slide rail;
Fig. 4 is the structured flowchart of the hoisting mechanism in system of the present invention.
In figure, have: high-order obstruction device 1, simulator 2, higher traction hook 3, slide rail 4, low level obstruction device 5, low level hoisting mechanism 6, low level dragrope 7, higher traction rope 8, high-order hoisting mechanism 9, mobile platform 10, rotating mechanism 11, power supply wheel 12, rubber wheel 13, draft arm 14, low level draw hook 15, motor 21, left clutch 22, flywheel 23, right clutch 24, windlass 25, left brake drum 26, right brake drum 27, main shaft 28.
Embodiment
See Fig. 1, Fig. 2 and Fig. 3.
Ship-board aircraft pilot dynamic simulated training system of the present invention, comprises simulator 2, and simulator 2 arranges rubber wheel 13 and rotating mechanism 11, and the rubber wheel 13 of simulator 2 contacts with slide rail 4; Slide rail 4 arranges low level horizontal segment (left side section of Fig. 1) and high-order horizontal segment (the right section of Fig. 1), is slope section (interlude of Fig. 1) between low level horizontal segment and high-order horizontal segment; Under the low level horizontal segment of slide rail 4 He under high-order horizontal segment, hoisting mechanism (low level hoisting mechanism 6 is all set, with high-order hoisting mechanism 9), the dragrope in hoisting mechanism (low level dragrope 7 and higher traction rope 8) twists on windlass (seeing the windlass 25 of Fig. 4); Simulator 2 is connected dragrope (low level dragrope 7 and higher traction rope 8) by draft arm 14 with draw hook (higher traction hook 3 and low level draw hook 15); The interior control device (in simulator 2, not shown in FIG.) of controlling hoisting mechanism, rotating mechanism 11 and draft arm 14 that arranges of simulator 2, also arranges clamping device (in simulator 2, not shown in FIG.) in simulator 2.
Draw hook (higher traction hook 3 and low level draw hook 15) is connected for linking up with draft arm 14.
The slope of slide rail 4 and the angle of level are 8～15 degree, and low level horizontal section length is 100～120m, and high-order horizontal section length is 100～120m, and slope section length is 40～60m.
End at the low level horizontal segment of slide rail 4 arranges low level obstruction device 5, and the end of high-order horizontal segment arranges high-order obstruction device 1.
High-order obstruction device 1 and low level obstruction device 5 are spring.
See Fig. 4.
The left clutch 22 that passes on left of the motor 21 of hoisting mechanism connects flywheel 23, and the right side of motor 21 connects windlass 25 by right clutch 24, and flywheel 23 and windlass 25 are connected with respectively brake drum (left brake drum 26 and right brake drum 27).
The diameter of flywheel 23 is 6～10 times of main shaft 28 diameters.
The training of taking off:
Trainer is in the interior preparation of simulator 2.Then give the 6 energising work of low level hoisting mechanism, the electric device in simulator 2 and electric control gear start.Referring to Fig. 4.Motor 21 runnings, unclamp left brake drum 26 and right brake drum 27, and right clutch 24 is unclamped, and left clutch 22 closes, now, and motor 21 flywheel driven 23 runnings.
When flywheel 23 runs to maximal rate, unclamp left clutch 22, the right clutch 24 that simultaneously closes, unclamps the braking in simulator 2.Windlass 25 in low level hoisting mechanism 6 rotates, and drives low level dragrope 7 to move.Low level dragrope 7 moves right by low level draw hook 15 and the draft arm 14 traction simulators 2 that are hooked together.By the power cable on slide rail 4 and power supply wheel 12, power to the electric device in simulator 2, electric device also drives simulator 2 to move right simultaneously.Meanwhile, because draft arm 14 is along with simulator moves right, compressed low level obstruction device 5 lifts restrictions, and the elastic force of spring also gives 2 one, simulator ejection force to the right.Under the acting in conjunction of tractive force, motor driving force and ejection force, simulator 2 can reach very high speed within very short time.But owing to wanting the takeoff condition of real simulation ship-board aircraft, thereby must the very strict condition of restriction, in 100m, be no more than in time of 2 seconds and make the speed of simulator 2 reach 200km/h left and right.This point is not still accomplished in the effect of above-mentioned three power, because the time is too short, the rotating speed of windlass 25 and motor 21 can not reach maximum speed within the so short time.And flywheel 23 is because diameter is very large, so inertia is very large, accelerated in advance after maximal rate, in the extremely short time, still can keep great speed, the speed that this speed can reach within the extremely short time than motor 21 is large.So now need left clutch 22 again to close, allow the flywheel 23 running up give windlass 25 1 accelerating forces.The translational speed of simulator 2 is brought up to setting the most at last.
Afterwards, simulator 2, after low level horizontal segment high speed slide 100m, will be climbed up the slope section that angle is 8 degree, enter takeoff condition.Now trainer need to throw off being connected of draft arm 14 and low level draw hook 15 and by control device, low level draw hook 15 be rested near taking off place.Give the electric device power-off in simulator 2 simultaneously.Simulator 2 enters inertia and takes off.
When simulator 2 is after slope section high speed slide 40m, enter high-order horizontal segment.Now take off and trained, start the training of stopping.The higher traction hook 3(higher traction hook 3 that draft arm 14 under simulator 2 articulates on higher traction rope 8 stops in place in advance), by the left brake drum 26 in high-order hoisting mechanism 9 and right brake drum 27, to simulator 2, give a damping force.Move the clamping device in simulator 2 simultaneously, rubber wheel 13 is braked.When simulator 2 slides the end to high-order horizontal segment in deceleration, the high-order obstruction device 1 of draft arm 14 touching, high-order obstruction device 1 applies resistance at the compressed simulator 2 of giving simultaneously.Under the triple role of high-order hoisting mechanism 9, high-order obstruction device 1 and simulator 2 wheel brakings, simulator 2 just reduces at a high speed zero and stop from 200km/h in short 100m.Thereby complete the training of stopping.
Finally, by controlling, rely on rotating mechanism 11, simulator 2 Rotate 180 degree, training can decline downwards.
Training declines:
Just the same with simulator 2 training of taking off, simulator 2 is subject under the acting in conjunction of the motor driving force in the tractive force of high-order hoisting mechanism 9, the ejection force of high-order obstruction device 1 and simulator 2, and simulator 2 can reach very high speed within very short time.The inertial force of the flywheel 23 in high-order hoisting mechanism 9 accelerates in addition, and the translational speed of simulator 2 is brought up to setting the most at last.
Afterwards, simulator 2 is in high-order horizontal segment end, throws off being connected and making higher traction hook 3 rest on close decline place by control device of draft arm 14 and higher traction hook 3.Give the electric device power-off in simulator 2 simultaneously.Simulator 2, by being the slope section of 8 degree along angle, enters decline state.
Afterwards, simulator 2 enters the parking of low level horizontal segment.Draft arm 14 hooks the low level draw hook 15 that has just rested on correct position (the close place of taking off) while taking off, under the triple role of low level hoisting mechanism 6, low level obstruction device 5 and simulator 2 wheel brakings, simulator 2 just reduces at a high speed zero and stop from 200km/h in short 100m.
Finally, by controlling, rely on rotating mechanism 11, simulator 2 Rotate 180 degree, the training of can taking off again again.
Claims (10)
1. ship-board aircraft pilot dynamic simulated training system, comprises simulator, it is characterized in that: simulator arranges wheel and rotating mechanism, and the wheel of simulator contacts with slide rail; Slide rail arranges low level horizontal segment and high-order horizontal segment, between low level horizontal segment and high-order horizontal segment, is slope section; Under the low level horizontal segment of slide rail He under high-order horizontal segment, hoisting mechanism is all set, the dragrope in hoisting mechanism twists on windlass; Simulator is connected dragrope by draft arm with draw hook; The control device of controlling hoisting mechanism, rotating mechanism and draft arm is set in simulator, clamping device is also set in simulator.
2. according to the system of claim 1, it is characterized in that: simulator mobile platform is set, and simulator is placed on mobile platform, the rotating mechanism of simulator is arranged between simulator and mobile platform, and wheel and draft arm are all arranged under mobile platform; Power supply wheel is also set under mobile platform, and power supply wheel contacts with the power cable on slide rail; Electric device and electric control gear are also set in simulator.
3. according to the system of claim 1, it is characterized in that: draw hook is connected for linking up with draft arm.
4. according to the system of claim 1, it is characterized in that: slide rail is rail, slide rail radical is two or four, and wheel is rubber guide wheel.
5. according to the system of claim 1, it is characterized in that: slide rail is shaped as I shape, upper and lower two wheels contact respectively the both sides up and down of the upper traverse rod of I shape slide rail.
6. according to the system of claim 1, it is characterized in that: the angle of slope and level is 8～15 degree, and low level horizontal section length is 100～120m, and high-order horizontal section length is 100～120m, and slope section length is 40～60m.
7. according to the system of claim 1, it is characterized in that: at the low level horizontal segment of slide rail and the end of high-order horizontal segment, obstruction device is set.
8. according to the system of claim 7, it is characterized in that: obstruction device is spring.
9. according to the system of claim 1, it is characterized in that: a side of the motor of hoisting mechanism connects flywheel by clutch coupling, the opposite side of motor connects windlass by another clutch coupling, and flywheel and windlass are connected with respectively brake drum.
10. according to the system of claim 9, it is characterized in that: flywheel diameter is shaft diameter 6～10 times.
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| CN201410034464.4A CN103761901B (en) | 2014-01-24 | 2014-01-24 | Ship-board aircraft pilot dynamic simulated training system |
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| CN201410034464.4A CN103761901B (en) | 2014-01-24 | 2014-01-24 | Ship-board aircraft pilot dynamic simulated training system |
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| CN106292334A (en) * | 2016-09-29 | 2017-01-04 | 大连理工大学 | A kind of along cableway aircraft device |
| CN108243801A (en) * | 2018-01-31 | 2018-07-06 | 沈阳农业大学 | A kind of external power type slip lid greenhouse wind-proof device |
| CN108961915A (en) * | 2018-09-07 | 2018-12-07 | 中国工程物理研究院总体工程研究所 | Roll freedom for helicopter Dynamic Flight Simulator turns round stop mechanism |
| CN110085088A (en) * | 2019-06-05 | 2019-08-02 | 福州高新区玲富科技有限公司 | A kind of airport baby plane seating simulation detection system |
| CN113155393A (en) * | 2021-03-03 | 2021-07-23 | 中国人民解放军95795部队 | Air-drop buffering air bag test device |
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| CN108961915B (en) * | 2018-09-07 | 2023-07-14 | 中国工程物理研究院总体工程研究所 | Rolling freedom degree rotation stopping mechanism for helicopter dynamic flight simulator |
| CN110085088A (en) * | 2019-06-05 | 2019-08-02 | 福州高新区玲富科技有限公司 | A kind of airport baby plane seating simulation detection system |
| CN110085088B (en) * | 2019-06-05 | 2021-01-26 | 南京奔联软件科技有限公司 | Small airplane riding simulation detection system for airport |
| CN113155393A (en) * | 2021-03-03 | 2021-07-23 | 中国人民解放军95795部队 | Air-drop buffering air bag test device |
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| CN103761901B (en) | 2016-04-13 |
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