CN1168810A - Tech. for launching man carried amusement rocket or space ship after single expelling - Google Patents

Tech. for launching man carried amusement rocket or space ship after single expelling Download PDF

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Publication number
CN1168810A
CN1168810A CN 96108710 CN96108710A CN1168810A CN 1168810 A CN1168810 A CN 1168810A CN 96108710 CN96108710 CN 96108710 CN 96108710 A CN96108710 A CN 96108710A CN 1168810 A CN1168810 A CN 1168810A
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China
Prior art keywords
chamber
detonation
plunger
pressure
ship
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Pending
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CN 96108710
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Chinese (zh)
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杨宝全
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Individual
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Individual
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Priority to CN 96108710 priority Critical patent/CN1168810A/en
Publication of CN1168810A publication Critical patent/CN1168810A/en
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Abstract

The present invention utilizes a motive device to regulate the space volume of combustion chamber, buffer chamber, high and low pressure reduction chambers so as to carry out manual control of the detonation velocity and pressure of detonotive fuel with different states and different quantiies, so that the initial launching velocity of rocket car or boat is controlled within disign range, and further by the secondary pressure reduction through low pressure reduction chamber to make the detonative tail gas pressure near or equal to atmospheric pressure reduction chamber to make the detonativetail gas pressure near or equal to atmospheric pressure so as to fulfill sounless lannching. It uses the dotomation principle in the ignitinng explosive technology to realizefulfill soundless. It uses the dotonation principle in the igniting explosive technology to realize rocket car to speed along runway and teh rocket loat to fly from land to water surface and go back to land by water jet force.

Description

A detonation does not have acoustic emission manned rocket car, ship technology
A kind of technology of utilizing solid, liquid, gas attitude detonation fuel through manned car of detonation emitted transverse, ship.
The objective of the invention is to provide a kind of and utilize power that a detonation of detonation fuel produces the adjusting of detonation parameter and control to be realized emitted transverse to manned rocket car, ship, be applicable to the manned entertainment device of land, the land water surface by the power set of the present invention shown in figure three, figure four, figure five.
The present invention is achieved in that by functional sequence
1, the emission of mellerwagon: mellerwagon divides single, double or many people, at transmitter site, be provided with parallel cement or pool pasta runway that two length are no less than 250 meters long, width is not less than 5 times of width of the carbody, respectively establish a transmitting station at two runway offsides, stand the other latter end of runway the brake direction board.Power set of the present invention are made up of three parts: cylinder body that (1) hull back is installed and high-pressure buffer device, low pressure silencer; (2) piston bush of installing on the transmitting station and plunger and igniter; (3) manipulation device that provides fuel and igniting to launch by transmitting station.
At first on the launching site, settle in an area, open mellerwagon top hatchcover, please the occupant be sitting in into the car on the vehicle seat position, fasten seat belts, worn the helmet and the helmet is closely fixing with head back backrest, both hands are held on control wheel, before car is pushed into transmitting station by the staff, carefully tailstock portion cylinder mouth being aligned the transmitting station piston is pushed into backward and stops after spacing, after getting in touch with the transmitting station personnel, hatchcover is shut (electronics countdown stopwatch on the interior instrument board of the car that links simultaneously), the transmitting station operating personnel begin to charge into detonation fuel (solid fuel pack into plunger) to power set before butt joint, after finishing, when transmitting station stopwatch (stopwatch is synchronous in car) occurs 0, press the emission push button, fuel produces detonation in power set, the promotion mellerwagon advances, after detonation forms, after once reducing pressure in the high pressure relief chamber, reduced explosion velocity, again through make after the low pressure pressure-reducing chamber decompression cylindrical implosion Hong gas tail gas pressure near or equal atmospheric pressure after, the transmitting station piston bush, plunger breaks away from the mellerwagon cylinder body, realizes no acoustic emission.
Continue to quicken, slide to run and progress into to spare to slow down and slide according to self inertia behind the mellerwagon acquisition initial velocity, be provided with speedometer in the car, the occupant can carry out brake operation up to stopping with reference to the other indication of braking of runway when car body moves to low speed.
2, the land of rocket craft emission: rocket craft is taked the mode of car ship one, the same Dan Shuan, how human-like that divides, the emission of different is rocket craft is to implement on the dash road of building in the waterside with a fixed angle of altitude, and preparation is the same with mellerwagon with launching procedure.The power set of rocket craft are equipped with jetting formula power set on the ship except that power set of the present invention, do not have outstanding screw at the bottom of the ship, bikini high speed aluminium alloy wheel before the hull bottom side is equipped with.
After hull obtains initial velocity, fly out to the water surface with the certain speed and the elevation angle along runway, and at predetermined water surface high speed water receiving, hull is slowed down rapidly, when stopping, the occupant can press push button starting jetting power set and handle the rocket craft water surface and turn and make a return voyage, and aims at the cement taxiway and quickens to slide to rush at the water surface and stop land being supported hull to slide to settle in an area on predetermined by wheel after.
Effect of the present invention is by controlling the explosion velocity of detonation effectively, and the thrust size that produces, the initial velocity of mellerwagon emission is controlled in the scope of design, make the arrival of occupant's nervous wait x time before emission in car, the ship simultaneously, T-time is realized the enormous impact power as rocket launching, but silence.When at a high speed sliding (water surface flying), take off or land as driving an airplane (water) proposed challenge to people's courage and resourcefulness.
The present invention is described in further detail below in conjunction with Figure of description 1,2,3,4,5.
2, with reference to shown in Fig. 1,2, this technology is adjusted the complete system that the jetting power set 7, transmitting station 4, plunger 5, high speed aluminum alloy wheel 6, positive waterside, elevation angle runway 9 etc. of hull 8 and car, power set of the present invention 3 that the ship afterbody is installed and hull are partly formed by the mellerwagon 1 of streamlined external form, sealed cabin 2 (combat trainer passenger cabin), car bottom.
Body 1 is the bulk flow line style equipment of taking advantage of manned member, power set, running gear being installed, and canopy 2 is streamliners that personal protection, sight line are observed, and the switch gearing of canopy the Kai Heguan of count-down stopwatch.Power set 3 are single cylinder two pressure-reducing chambers decompression, the noiseless launch power device of a detonation of surge chamber space, combustion chamber regulating plunger state type, will narrate in the back in conjunction with Fig. 3,4,5.Transmitting station 4 is a ladder type basis platform, is horizontally installed with above in the stationary part plunger 5, plunger of power set fuel filler tube 9 and 13 spark plugs 12 are housed, controlled by the transmitting station operator.High speed aluminum alloy wheel 6 is two big one little sliding wheels of installing of three preceding bikinis that are isosceles triangle, thin rubber flange is installed.Ram intake 9 is after emission, air-flow is imported the tailstock power set are implemented air cooled effect.At the bottom of hull 8 is high-speed boat, jetting power set 7 are housed, after entering aerial water surface flying after the emission of land, are used for the device that hydroplaning and the water surface make a return voyage.Runway 10 after rocket craft obtains initial velocity will along generation have the runway at the elevation angle realize the water surface 12 after carrying out the coasting flight of low-angle water surface parabola with the elevation angle at α angle 11 effect of water.
1, with reference to shown in Fig. 3,4,5, power set of the present invention are made up of transmitting station 1, static piston bush 3, plunger 2 first, movable part cylinders 4 and fuel injection nozzle 9, more than 13 major parts.Introduce its operation principle below in conjunction with accompanying drawing: these power set can be fit to use solid-state, liquid state and gaseous state, oxidant incendiary agent one-component and multicomponent mixing detonation fuel respectively.
(1) at first introduces use gas, the emission principle of liquid fuel: transmitting station 1 is installed with static plunger 2, plunger 2 outer walls are processed with the adjusting screw thread, piston bush 3 with plunger 2 by being threaded, rotary-piston cover 3 volume space that can enlarge and dwindle combustion chamber 11, stopper head is equipped with fuel and injects nozzle 9, oxidant injects nozzle 13 and spark plug 12, stopper head is the hermetic seal contact with the piston bush inwall, the piston bush forward part also is the hermetic seal contact with cylinder 4 inwalls, be processed with several high pressure gas holes 14 and low pressure exhaust hole 15 on the cylinder 4 respectively, high pressure relief chamber 7 with end plate 8 respectively with cylinder 4 by being threaded, and by rotation air chamber 7,8 pairs of air chamber volume space of end plate are implemented to adjust, to adapt to the needs that different parameters changes, low-pressure chamber 5 and end plate 6 are in like manner.
The piston bush 3 that level on 4 pairs of transmitting stations 1 of cylinder of installing in the mellerwagon 10 is installed at first, car is inserted in plunger 2 at leisure, piston bush 3 is owing to exist low pressure, high pressure two-stage air chamber, a large amount of air are subjected to less compression in the fashionable pressure-reducing chamber so overlap, the plunger propelling resistance is reduced, when plunger is delivered to stop, the transmitting station operating personnel are in cylinder, combustion chamber 11 filling incendiary agent and oxidants in plunger 2 and the piston bush 3, after reaching authorized pressure, close the filling valve, during igniting, produce spark by spark plug 12, fuel produces detonation, because piston 3, plunger maintains static by transmitting station 1, and detonation powered cylinder body 4 travels forward at a high speed, when piston bush moves to high pressure relief chamber steam vent, initial detonation has lowered explosion velocity after the decompression of hyperbaric chamber, promote car with initial big kinetic energy, suitable again explosion velocity promotes cylinder body and moves to low-pressure chamber after the hull motion, carry out the secondary decompression after, make detonation tail gas pressure reduce near or equal atmospheric pressure after, cylinder is with the piston bush high-speed separation.Realize that by adjustment a detonation do not have acoustic emission, and realize the artificial control of the launch velocity of mellerwagon, ship the equipment adjustment of detonation explosion velocity, detonation pressure, control ratio, prescription.
2, the use principle of solid-state propellant powder: at first its equipment difference of having any different the emission of gas-liquid attitude is done relatively in conjunction with Fig. 5.Be installed in plunger 2 first differences among the same Fig. 3 of plunger 2 second, 4 on the transmitting station and be closure plate 8 that an inwall processing generation has centre bore 7, cancelled fuel adding nozzle and spark plug.The volume space of piston bush 3 same rotatable adjustment surge chambers 6 is carried out IGNITION CONTROL by 4 pairs of powder charges of igniter 5.After detonation produces, by surge chamber 6 and motion after no acoustic emission is realized in high pressure relief chamber, decompression back, low pressure pressure-reducing chamber.

Claims (8)

1, a kind of by mellerwagon 1, passenger cabin 2, power set 3, plunger 5, cooling air inlet 9, high speed aluminum-alloy wheel 6, transmitting station 4, hull 8, jetting power set 7, high speed aluminum-alloy wheel 6, power set 3, emission stiff end (transmitting station) 1, plunger 2 first, piston bush 3, movable end cylinder body 4, low pressure anechoic room 5, low-pressure chamber end plate 6, hyperbaric chamber 7, hyperbaric chamber end plate 8, plunger fuel injects nozzle 9, the plunger oxidant injects nozzle 13, load (mellerwagon, ship) 10, combustion chamber 11, spark plug 12, high pressure gas hole 14, low pressure exhaust hole 15, plunger 2 second, igniter 4, closure plate 8 for centre bore 7, solid charge 5, the adjustable manned land and water type high-speed rocket car of launch velocity that surge chamber 6 is formed, the ship entertainment device.It is characterized in that mellerwagon, ship 1 adopt a detonation not have acoustic emission by power set 3 of the present invention and realize.
2, according to claim 1 described device, it is characterized in that the movable part cylinder 4 of mellerwagon, ship 1 power set is mounted in the afterbody of car, ship, standing part plunger 2, piston bush 3 are that horizontal fixed is installed in transmitting station (stiff end) 1 runway end.Piston bush 3, plunger 2 first, second are passed to transmitting station with explosive force and are balanced out during emission, and cylinder block then promotes load 10 motions.The detonation heat that cylinder body 4 absorbs is discharged by the absorption of air of air inlet 9 introducings of car, the installation of hull side and from afterbody.
3, according to claim 1,2 described devices, it is characterized in that car, ship are run for high speed wheel realization land, the Lu Shuilu cunning of rubber flange by preceding bikini two big one three little aluminium alloy bull wheels, the runway of rocket craft is the positive elevation angle to the water surface, land is returned in the hydroplaning of electricity startup jetting power maintenance after the entry, and rocket, ship are equipped with power set of the present invention and jetting power set simultaneously.
4, according to claim 1 described device, it is characterized in that power set 3 of the present invention are to utilize the detonation principle in the fiery explosive technology to take a detonation of single cylinder, can use the ternary detonation fuel of solid, liquid, gas respectively, by power set 3, by threaded adjusting respectively rotary-piston cover 3, low pressure pressure-reducing chamber 5, high pressure relief chamber 7, end plate 6,8 in order to adjustment to the volume space in combustion chamber 11, high pressure relief chamber 7, low pressure pressure-reducing chamber 5, increase high and low pressure pressure-reducing chamber volume, thrust reduces, improved erasure effect, otherwise add high thrust, erasure effect is poor.Explosion velocity, the detonation pressure of control detonation; Pass through detonation fuel oxidizer, incendiary agent prescription, the adjustment of ratio and dose control when liquid, gaseous fuel increase thrust, strengthens combustion chamber volume, otherwise reduces again; When solid fuel increases thrust, dwindle buffer chamber volume, otherwise reduce.Thereby realize what the mellerwagon launch velocity was controlled.
5, according to the described device of claim 1-4, the no acoustic emission that it is characterized in that mellerwagon, ship 1 is after once expanding the decompression of decompression, low pressure pressure-reducing chamber quadratic extension by the high pressure relief chamber, make detonation tail gas pressure near or be achieved when equaling atmospheric pressure.
6, according to the described device of claim 1-2, it is characterized in that liquid, gaseous state detonation fuel be by be fixed on transmitting station 4, plunger 2 first, fuel inject nozzle 9, oxidant inject nozzle 13 inject combustion chambers 11 and by fuel, oxidant that transmitting station 4 is realized by plunger 2 first, spark plugs 12 inject and igniting,
7, according to claim 1 described device, solid gun propellant 5 is earlier at the transmitting terminal plunger 2 of packing into.Solid gun propellant 5 is to cause and plunger 2 second is made up of the closure plate 8 of centre bore 7 processing generation and leave surge chamber 6 and also can adjust the surge chamber volume space by the rotary-piston cover simultaneously and realize controlling explosion velocity by igniter 4, thereby the control of detonation pressure realization launch velocity.
8,, it is characterized in that mellerwagon, 1 fen single and many people of ship according to claim 1,3 described devices; Be divided into land type and Lu Shuixing by accommodation, can establish in the passenger cabin 21 at the most the people vertically arrange realization.
CN 96108710 1996-06-17 1996-06-17 Tech. for launching man carried amusement rocket or space ship after single expelling Pending CN1168810A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 96108710 CN1168810A (en) 1996-06-17 1996-06-17 Tech. for launching man carried amusement rocket or space ship after single expelling

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 96108710 CN1168810A (en) 1996-06-17 1996-06-17 Tech. for launching man carried amusement rocket or space ship after single expelling

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CN1168810A true CN1168810A (en) 1997-12-31

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CN 96108710 Pending CN1168810A (en) 1996-06-17 1996-06-17 Tech. for launching man carried amusement rocket or space ship after single expelling

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102539178A (en) * 2011-10-27 2012-07-04 北京航天计量测试技术研究所 Heat flow guide passage system for suspended lifting platform
CN104747319A (en) * 2014-01-01 2015-07-01 冯石文 Solid fuel rocket motor
CN113003630A (en) * 2021-03-30 2021-06-22 南京御水科技有限公司 Industrial circulating water's quick settlement device

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102539178A (en) * 2011-10-27 2012-07-04 北京航天计量测试技术研究所 Heat flow guide passage system for suspended lifting platform
CN102539178B (en) * 2011-10-27 2014-03-26 北京航天计量测试技术研究所 Heat flow guide passage system for suspended lifting platform
CN104747319A (en) * 2014-01-01 2015-07-01 冯石文 Solid fuel rocket motor
CN104747319B (en) * 2014-01-01 2019-05-21 冯石文 A kind of solid propellant engine
CN113003630A (en) * 2021-03-30 2021-06-22 南京御水科技有限公司 Industrial circulating water's quick settlement device
CN113003630B (en) * 2021-03-30 2023-05-12 嘉兴诚毅环保科技有限责任公司 Quick sedimentation device of industrial circulating water

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