CN203572314U - Two-stage single-piston high-speed projectile launching system - Google Patents
Two-stage single-piston high-speed projectile launching system Download PDFInfo
- Publication number
- CN203572314U CN203572314U CN201320746757.6U CN201320746757U CN203572314U CN 203572314 U CN203572314 U CN 203572314U CN 201320746757 U CN201320746757 U CN 201320746757U CN 203572314 U CN203572314 U CN 203572314U
- Authority
- CN
- China
- Prior art keywords
- storage tank
- piston
- gas storage
- air accumulator
- projectile
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 238000002347 injection Methods 0.000 claims abstract description 12
- 239000007924 injection Substances 0.000 claims abstract description 12
- 239000008188 pellet Substances 0.000 claims description 9
- 230000001133 acceleration Effects 0.000 claims description 5
- 230000004927 fusion Effects 0.000 abstract description 4
- 230000006835 compression Effects 0.000 abstract description 3
- 238000007906 compression Methods 0.000 abstract description 3
- 239000007789 gas Substances 0.000 description 6
- 239000001307 helium Substances 0.000 description 3
- 229910052734 helium Inorganic materials 0.000 description 3
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000004134 energy conservation Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 238000005086 pumping Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
Images
Abstract
The utility model belongs to the field of fusion projectile injection, and particularly relates to a two-stage single-piston high-speed projectile launching system, which comprises a first gas storage tank, a second gas storage tank, a piston, a quick valve and an accelerating barrel, wherein the first gas storage tank is communicated with the second gas storage tank, and the quick valve and the piston are sequentially arranged in the second gas storage tank; the second gas storage tank is communicated with the accelerating barrel, and a projectile is arranged in the accelerating barrel. The two-stage single-piston high-speed projectile launching system provided by the utility model has the advantages that the pressure of the second gas storage tank can be improved by a gas adiabatic compression principle, the structure corresponds to serial connection of two single-stage pneumatic guns, and the pressure of the gas storage tank can be up to several hundred MPa, so that the projectile can be quickly accelerated.
Description
Technical field
The invention belongs to the reinforced field of a kind of fusion bullet, be specifically related to a kind of two-stage list high speed piston Pellet Injection System.
Background technology
At present, on lot of domestic and international fusion facility, conventionally from feeble field side, carry out bullet injection, adopt single-stage linear pattern pipeline transmission bullet, in engineering, be easier to realize.Bullet injection rate is easier to reach 1km/s, and can keep good integrality to be injected in plasma.But such initial velocity is nowhere near for the desired velocity of shot of large-scale fusion reactor core fueling, in order to break through the speed limit of single-stage Pneumatic acceleration, be necessary to design a kind of High-velocity Projectiles emission system, and adopting two-stage list piston emission system can solve this class problem, the theoretical velocity of shot calculating is up to thousands of metre per second (m/s)s.
Summary of the invention
The object of this invention is to provide a set of two-stage list piston emission system, a kind of High-velocity Projectiles transmitting is provided, realize bullet core fueling, thereby improve the reinforced efficiency of bullet etc.
The present invention realizes like this, two-stage list high speed piston Pellet Injection System, it comprises the first air accumulator, the second air accumulator, piston, fast valve, accelerates gun barrel, the first air accumulator is communicated with the second air accumulator, in the second air accumulator, be provided with successively fast valve and piston, the second air accumulator is communicated with acceleration gun barrel, accelerates to lay bullet in gun barrel.
Advantage of the present invention is, the gas adiabatic compression principle that its adopts improves the second air accumulator pressure, and its structure is equivalent to the series connection of two single-stage pneumatic gun, and its air accumulator pressure can be up to hundreds of MPas, thus ACCELERATING PROJECTILE rapidly.
Accompanying drawing explanation
Fig. 1 is two-stage list high speed piston Pellet Injection System structural representation provided by the present invention;
Fig. 2 is schematic diagram before pellet injection;
Fig. 3 is schematic diagram after pellet injection.
In figure, 1 first air accumulator, 2 fast valves, 3 pistons, 4 second air accumulators, 5 bullets, 6 accelerate gun barrel, 7 hydrogen or helium.
The specific embodiment
Below in conjunction with drawings and Examples, the present invention is described in detail:
Two-stage list high speed piston Pellet Injection System mainly comprises the first air accumulator 1, the second air accumulator 4, piston 3, fast valve 2, accelerates gun barrel 6.
As shown in Figure 1, the first air accumulator 1 is communicated with the second air accumulator 4, fast valve 2 and piston 3, the second air accumulators 4 is installed successively in the second air accumulator 4 and is communicated with acceleration gun barrel 6, accelerates to lay bullet 5 in gun barrel 6.
The gas adiabatic compression principle that native system adopts improves the second air accumulator pressure, its structure is equivalent to the series connection of two single-stage pneumatic gun, its air accumulator pressure can be up to hundreds of MPas, thereby energy is ACCELERATING PROJECTILE rapidly, emission process: according to time command, the first step is opened fast valve, gases at high pressure moment in the first air accumulator enters the second air accumulator, promote rapidly the piston advances forward in the second air accumulator, compress the low-pressure gas in the second air accumulator, during pressure hundred MPa that the pressure sensor in air accumulator obtains, second step is opened the second fast valve, now the instantaneous promotion bullet of gases at high pressure travels forward, accelerated in gun barrel, the 3rd step, open vacuum-pumping system, extract unnecessary gas.
The operation of two-stage list piston emission system is as follows:
1, the about 4L of the first air accumulator volume, 0.1MPa< pressure <0.5MPa, generally adopts high-purity helium;
2, the second air accumulator is about 1.2m, internal diameter 30mm, and the about 0.85L of volume, is filled with helium in tank, pressure <0.11MPa;
3, piston adopts high-strength elastic rubber to make, and the about 30mm of length is whole tapered, is easy to high-speed slide, and the about 30g of gross mass, and the tolerance fit <0.01mm between the second air accumulator, guarantee its sealing;
4, the about 1.2m of electron gun pipe range, internal diameter 4mm, is used for ACCELERATING PROJECTILE.
5, the main equation of analog computation has: the conservation of mass and the energy conservation equation of the first air accumulator and the second air accumulator, the equation of momentum of piston, characteristic of fluid line equation in the second air accumulator, bullet back pressure equation and the equation of momentum.
6, connection is separated above-mentioned 6 large equations, can calculate the pressure in each air accumulator and temperature rise in pellet injection process; Piston displacement and speed; The back pressure that bullet bears and the acceleration of acquisition, speed etc.
Claims (1)
1. two-stage list high speed piston Pellet Injection System, it is characterized in that: it comprises the first air accumulator (1), the second air accumulator (4), piston (3), fast valve (2), accelerates gun barrel (6), the first air accumulator (1) is communicated with the second air accumulator (4), in the second air accumulator (4), be provided with successively fast valve (2) and piston (3), the second air accumulator (4) is communicated with acceleration gun barrel (6), accelerates to lay bullet (5) in gun barrel (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320746757.6U CN203572314U (en) | 2013-11-22 | 2013-11-22 | Two-stage single-piston high-speed projectile launching system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320746757.6U CN203572314U (en) | 2013-11-22 | 2013-11-22 | Two-stage single-piston high-speed projectile launching system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203572314U true CN203572314U (en) | 2014-04-30 |
Family
ID=50540042
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320746757.6U Expired - Lifetime CN203572314U (en) | 2013-11-22 | 2013-11-22 | Two-stage single-piston high-speed projectile launching system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203572314U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104654916A (en) * | 2013-11-22 | 2015-05-27 | 核工业西南物理研究院 | Two-stage single-piston high-speed bullet launch system |
| CN112254572A (en) * | 2020-10-21 | 2021-01-22 | 中国科学院力学研究所 | Piston for gas detonation drive ultra-high-speed launch testing device |
-
2013
- 2013-11-22 CN CN201320746757.6U patent/CN203572314U/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104654916A (en) * | 2013-11-22 | 2015-05-27 | 核工业西南物理研究院 | Two-stage single-piston high-speed bullet launch system |
| CN112254572A (en) * | 2020-10-21 | 2021-01-22 | 中国科学院力学研究所 | Piston for gas detonation drive ultra-high-speed launch testing device |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104654916A (en) | Two-stage single-piston high-speed bullet launch system | |
| CN102778171B (en) | Three-level light-gas gun driven by compressed nitrogen | |
| CN109945740B (en) | Novel two-level light air gun driven by high-pressure air | |
| CN203572314U (en) | Two-stage single-piston high-speed projectile launching system | |
| CN101865760A (en) | Gas gun scheme experiment system of high-speed rain movable model | |
| CN109870069B (en) | Single-tube air cannon capable of continuously launching | |
| CN102921127B (en) | Gases at high pressure launch water cannon | |
| CN105351260B (en) | Gas-liquid mixed multistage high speed ejection device | |
| CN202124119U (en) | Steam ejection boosting device for taking off of airplane | |
| CN103007471B (en) | Air bag buffered high pressure gas water shell firing device | |
| CN202178066U (en) | Multilevel differential vacuum pumping system for propulsive gas of nuclear fusion projectile charging | |
| CN103057720A (en) | Gunpowder catapult | |
| CN202915827U (en) | Barrel recoil buffering mechanism | |
| CN103335559B (en) | Double sealing membrane breaking machine | |
| CN206160822U (en) | High -pressure gas big gun is sent out to wink | |
| CN109855471B (en) | Anti-recoil device of multistage air cannon | |
| CN202961611U (en) | High-pressure gas catapulting water gun | |
| CN102903399B (en) | Multistage differential vacuum pumping system for pellet charging propulsive gas in nuclear fusion | |
| CN109236761B (en) | Hydraulic energy storage control method and hydraulic energy storage device thereof | |
| CN103055457B (en) | High pressure gas water bomb launching device buffered by valve control airbag | |
| CN217520938U (en) | Hydraulic drive's second grade light gas superelevation strain rate loading drive arrangement | |
| CN202892736U (en) | Ultra-long-range high-pressure pulse water flushing gun | |
| CN108333040B (en) | Hopkinson pressure bar air cannon launching tube capable of automatically loading bullets | |
| CN104713771A (en) | Launcher of Hopkinson equipment | |
| CN203464850U (en) | Double sealing membrane breaking machine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term |
Granted publication date: 20140430 |
|
| CX01 | Expiry of patent term |