CN1687693A - Curve shaped bullet holder in autosegregation - Google Patents
Curve shaped bullet holder in autosegregation Download PDFInfo
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- CN1687693A CN1687693A CN 200510009959 CN200510009959A CN1687693A CN 1687693 A CN1687693 A CN 1687693A CN 200510009959 CN200510009959 CN 200510009959 CN 200510009959 A CN200510009959 A CN 200510009959A CN 1687693 A CN1687693 A CN 1687693A
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- bullet
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Abstract
The invention is the curved self-separating bullet pallet, and relates to the improvement of the pallet structure. The invention aims to solve the unstable separation of the straight bullet pallet. The sections of the left distinguish 1 and the right distinguish 2 are two corresponding semicircles; the upper part of one side of the inner face 11 of the left distinguish 1 opens the left bullet hole 3; the inner face 11 of the left distinguish 1 has left tooth profile 5; the upper part of one side of the inner face 12 of the right distinguish 2 opens the right bullet hole 4 that is corresponding to the left bullet hoe 3; the inner face 12 of the right distinguish 2 has the right tooth profile 6 that engages with the left tooth profile 5; the left distinguish 1 is the curved body 9 and the right distinguish 2 is the curved body 10 corresponding to the left distinguish. The invention improves the launching efficiency and lowers the cost.
Description
Technical field:
The present invention relates to a kind of improvement that plays holder structure.
Background technology:
The high speed light-gas gun is in " spacecraft space junk crash " research field, carries out the capital equipment of hypervelocity impact ground simulation test, is used for launching the projectile impact target plate of 3～7 kilometer per second speed, and target plate is pressed the material and the structure manufacturing of spacecraft bulkhead.Purpose is to explore the material and the structure of the spacecraft bulkhead that adapts to the long-life man-in-space flight.During high speed light-gas gun emission bullet,, need that bullet is put into the bullet holder and launch because of bullet has different shapes and diameter.The effect of bullet holder is to protect bullet not contact with HTHP driving gas in transmitting tube and the transmitting tube in accelerator, avoids transmitting tube and driving gas that bullet is caused damage.Also avoid simultaneously of the damage of metal bullet to transmitting tube.After leaving transmitting tube, the bullet holder needs to separate with bullet.Bullet continues to move along the central axis of transmitting tube and hits target plate.Need to adopt certain isolation technics on the target plate for avoiding the bullet holder to get to.Existing separation method is divided into two classes: pneumatic separation separates with additional separator.One, the problem of pneumatic isolation technics existence mainly contains: this specification requirement is inflated in the target cabin, utilizes air resistance that the bullet holder is separated.The volume density of inflating big more, bullet holder flying distance is far away more, bullet holder distance of separation is big more.But, after the inflation, reduced the vacuum requirement in target cabin, and increased the projectile flight resistance, reduced velocity of shot.How many separating resultings is subjected to aeration quantity, and the influence of bullet holder shape (aerodynamic configuration), causes the separating effect instability, and certain randomness is arranged.This technology can not be used under the target cabin requires to the condition of vacuum.Two, the problem of additional separator isolation technics existence mainly contains: additional separator is that mechanical device or aerodynamic drag device are set between transmitting tube and target plate, and the bullet holder is separated with bullet.This its center line of class matching requirements is accurately coaxial with launcher-tube line, and it is more to adjust the time spent.This class device generally all is provided with cracky spare, and the new fragment that cracky spare produced still might hit target plate, reduces separating effect.And each experiment all need be changed cracky spare, has increased launch cost.This class device itself occupies certain space, and other the use of observation test instrument and equipment is caused adverse effect.Two above-mentioned structure problems that problem is the bullet holder after all, no matter existing bullet holder is made up of two lobes still is to be made up of pintongs, the monnolithic case of its bullet holder all is a stretched shape, after transmitting tube is left in the bullet holder, himself can not initiatively open, full resistance or other device by gas opens with bullet the bullet holder to separate, so cause the appearance of above-mentioned two problems.
Summary of the invention:
The objective of the invention is for solve existing stretched shape bullet deposit the separating effect instability, increase the problem of launch cost, a kind of curve shaped bullet holder in autosegregation is provided.The present invention has under the condition that keeps target cabin vacuum, does not increase any device the bullet holder is separated with bullet, improves emission effciency, reduces the characteristics of launch cost.The present invention is made up of left split 1 and right split 2; The horizontal cross-section of left split 1 and right split 2 is two corresponding semicircles, the top of inner face 11 1 sides of left split 1 has left half bullet hole 3, the inner face 11 of left split 1 is provided with left profile of tooth body 5, the top of inner face 12 1 sides of right split 2 has right half bullet hole 4, half bullet hole 3, a left side on the left split 1 is corresponding with the half bullet hole 4, the right side on the right split 2, the inner face 12 of right split 2 is provided with the right tooth shape body 6 that is meshed with left profile of tooth body 5 on the left split 1, left split 1 is a curve shaped 9, and right split 2 is curve shapeds 10 symmetrical with left split 1.The present invention is designed to the holder of bent body bullet with the holder of existing stretched bullet.After bent body bullet support was gone into the transmitting tube of high speed light-gas gun, being subjected to the restrained deformation of transmitting tube tube wall was stretched, and remained stretched move along launcher-tube line in transmitting tube in emission process.At the moment tube wall that breaks away from the transmitting tube mouth of pipe constraint of bullet holder is disappeared, bullet holder meeting reverts to bent body, and the bullet holder can produce in reverting to the process of bent body along perpendicular to the moving of launcher-tube line direction, thereby, bullet holder and bullet are separated.Just be equivalent to add between the bullet holder spring that the bullet holder is separated, only this spring is exactly bullet holder itself.Under the gas effect after the bullet holder separately in transmitting tube, can rotate, proal speed is reduced, further improve separating effect around barycenter.The present invention has under the condition that keeps target cabin vacuum, does not increase any device the bullet holder is separated with bullet, improves emission effciency, reduces the advantage of launch cost.
Description of drawings:
Fig. 1 is the front view after bullet holder left split 1 of the present invention and right split 2 separate, Fig. 2 is the perspective view after bullet holder left split 1 of the present invention and right split 2 separate, Fig. 3 is that the schematic diagram that bullet moves is carried in the bullet holder in transmitting tube, Fig. 4 is the bullet holder part of stretching out transmitting tube under self elastic reaction, the schematic diagram that reverts to bent body and separate, Fig. 5 is the moment of all leaving transmitting tube in the bullet holder, and the schematic diagram the when flexural deformation of bullet holder distinguish launches fully, Fig. 6 are that the A of Fig. 3 is to view.In the Reference numeral of Fig. 3～Fig. 5,15 is bullet, and 16 is transmitting tube, and 17 is high drive gas.
The specific embodiment:
The specific embodiment one: (referring to Fig. 1, Fig. 2) present embodiment is made up of left split 1 and right split 2; The horizontal cross-section of left split 1 and right split 2 is two corresponding semicircles, the top of inner face 11 1 sides of left split 1 has left half bullet hole 3, the inner face 11 of left split 1 is provided with left profile of tooth body 5, the top of inner face 12 1 sides of right split 2 has right half bullet hole 4, half bullet hole 3, a left side on the left split 1 is corresponding with the half bullet hole 4, the right side on the right split 2, the inner face 12 of right split 2 is provided with the right tooth shape body 6 that is meshed with left profile of tooth body 5 on the left split 1, left split 1 is a curve shaped 9, and right split 2 is curve shapeds 10 symmetrical with left split 1.The material of described left split 1 and right split 2 is Merlon, polyethylene or nylon.
The specific embodiment two: the difference of (referring to Fig. 1, Fig. 2) present embodiment and the specific embodiment one is that the upper surface of left split 1 is plane 7, and the upper surface of right split 2 is plane 8.Other composition is identical with the specific embodiment one with annexation.The upper surface of left split 1 and right split 2 is designed to planar structure, can increases the resistance of motion of bullet holder, enable better to separate with bullet.
Operation principle: when the bullet support was gone into transmitting tube, it is cylindrical that available anchor clamps become the bullet holder, pushes in the transmitting tube again, and the bullet holder is subjected to the effect of high drive gas in the bottom, and under high drive gas promoted, the bullet holder was carried bullet and moved in transmitting tube, as shown in Figure 3.When bullet holder front end stretched out transmitting tube, owing to no longer be subjected to the constraint of transmitting tube, the part that transmitting tube is stretched out in the bullet holder was separated because of reverting to curved shape, as shown in Figure 4 under self elastic reaction.All leave the moment of transmitting tube in the bullet holder, when the flexural deformation of bullet holder distinguish launches fully, drive two distinguish along moving perpendicular to the direction of launcher-tube line, the barycenter that makes two distinguish mutually away from, forms the bigger angle of departure (angle between direction and the launcher-tube line is moved in bullet delivery).As shown in Figure 5.Under the high drive gas effect in transmitting tube, bullet holder distinguish can rotate around barycenter, and proal speed is reduced, and has further improved separating effect.
Claims (3)
1, curve shaped bullet holder in autosegregation, it is made up of left split (1) and right split (2); The horizontal cross-section of left split (1) and right split (2) is two corresponding semicircles, the top of inner face (11) one sides of left split (1) has left half bullet hole (3), the inner face (11) of left split (1) is provided with left profile of tooth body (5), the top of inner face (12) one sides of right split (2) has right half bullet hole (4), half bullet hole (3), a left side on the left split (1) is corresponding with the half bullet hole (4), the right side on the right split (2), the inner face (12) of right split (2) is provided with the right tooth shape body (6) that is meshed with left profile of tooth body (5) on the left split (1), it is characterized in that left split (1) is a curve shaped (9), right split (2) is the curve shaped (10) symmetrical with left split (1).
2, curve shaped bullet holder in autosegregation according to claim 1, the upper surface that it is characterized in that left split (1) are plane (7), and the upper surface of right split (2) is plane (8).
3, curve shaped bullet holder in autosegregation according to claim 1 and 2 is characterized in that the material of described left split (1) and right split (2) is Merlon, polyethylene or nylon.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2005100099592A CN100370214C (en) | 2005-04-29 | 2005-04-29 | Curve shaped bullet holder in autosegregation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2005100099592A CN100370214C (en) | 2005-04-29 | 2005-04-29 | Curve shaped bullet holder in autosegregation |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1687693A true CN1687693A (en) | 2005-10-26 |
| CN100370214C CN100370214C (en) | 2008-02-20 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNB2005100099592A Expired - Fee Related CN100370214C (en) | 2005-04-29 | 2005-04-29 | Curve shaped bullet holder in autosegregation |
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| CN (1) | CN100370214C (en) |
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101839672A (en) * | 2010-04-29 | 2010-09-22 | 中国工程物理研究院流体物理研究所 | Ultra-high-speed gram-magnitude spherical projectile transmitting device |
| CN102062565A (en) * | 2010-11-08 | 2011-05-18 | 西安近代化学研究所 | Separator for preventing sabot from following |
| CN102297640A (en) * | 2011-08-24 | 2011-12-28 | 西安近代化学研究所 | Device for separating bullet and bullet support |
| CN105222659A (en) * | 2015-09-18 | 2016-01-06 | 西北核技术研究所 | Centring type angle of attack bullet holder before and after a kind of Balance Gun |
| CN105547806A (en) * | 2015-12-14 | 2016-05-04 | 北京理工大学 | Accelerating sabot and method for cylindrical fragment of 20-40g accelerated to speed of 200-1100m/s |
| CN105547059A (en) * | 2015-12-16 | 2016-05-04 | 哈尔滨工业大学 | Sabot capable of realizing pneumatic separation through muzzle cutters |
| CN105547058A (en) * | 2015-12-16 | 2016-05-04 | 哈尔滨工业大学 | Projectile holder separating system based on momentum theorem |
| CN105571936A (en) * | 2015-12-14 | 2016-05-11 | 北京理工大学 | 30-40g cylindrical fragment 1100-1700m/s acceleration bullet support and method |
| CN108895932A (en) * | 2018-05-10 | 2018-11-27 | 西南科技大学 | For impacting the bullet of the experiment of machanics of gas big gun and testing the device of the velocity of shot |
| CN108955371A (en) * | 2018-07-25 | 2018-12-07 | 北京理工大学 | A kind of bullet support electromagnetic separation of light-gas gun |
| CN113108655A (en) * | 2021-03-22 | 2021-07-13 | 北京理工大学 | Self-separating bullet holder for bullet body with elliptical section |
| CN112504008B (en) * | 2020-11-27 | 2022-07-01 | 江苏科技大学 | Multi-fragment synchronous launching bullet holder device and assembling method thereof |
| CN115235289A (en) * | 2022-06-30 | 2022-10-25 | 江苏恒神股份有限公司 | Composite material bullet holder and forming method |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104729364B (en) * | 2015-03-27 | 2016-07-06 | 西北核技术研究所 | A kind of pneumatic separation bullet holder of light-gas gun |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2445509A1 (en) * | 1978-12-28 | 1980-07-25 | Thomson Brandt | LAUNCHING MECHANISM OF A SUB-CALIBER PROJECTILE |
| US4827847A (en) * | 1985-05-30 | 1989-05-09 | Her Majesty The Queen In Right Of Canada | Short range tubular projectile |
| DE3625730A1 (en) * | 1986-08-04 | 1988-02-18 | Rheinmetall Gmbh | DRIVING CAGE WITH A MATERIAL COMPOSITE FOR A LOW-LENGTH / DIAMETER RATIO UNDER-CALIBRATION RIFLE STOCK |
| US5473989A (en) * | 1995-02-24 | 1995-12-12 | Buc; Steven M. | Fin-stabilized discarding sabot projectile |
| US6186094B1 (en) * | 1998-08-26 | 2001-02-13 | Alliant Techsystems Inc. | Sabot anti-splitting ring |
| CN2575597Y (en) * | 2002-09-13 | 2003-09-24 | 黄一兵 | Polymer optical fiber on-line measuring diameter instrument |
-
2005
- 2005-04-29 CN CNB2005100099592A patent/CN100370214C/en not_active Expired - Fee Related
Cited By (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101839672A (en) * | 2010-04-29 | 2010-09-22 | 中国工程物理研究院流体物理研究所 | Ultra-high-speed gram-magnitude spherical projectile transmitting device |
| CN101839672B (en) * | 2010-04-29 | 2012-10-03 | 中国工程物理研究院流体物理研究所 | Ultra-high-speed gram-magnitude spherical projectile transmitting device |
| CN102062565A (en) * | 2010-11-08 | 2011-05-18 | 西安近代化学研究所 | Separator for preventing sabot from following |
| CN102062565B (en) * | 2010-11-08 | 2013-04-03 | 西安近代化学研究所 | Separator for preventing sabot from following |
| CN102297640A (en) * | 2011-08-24 | 2011-12-28 | 西安近代化学研究所 | Device for separating bullet and bullet support |
| CN102297640B (en) * | 2011-08-24 | 2013-08-28 | 西安近代化学研究所 | Device for separating bullet and bullet support |
| CN105222659A (en) * | 2015-09-18 | 2016-01-06 | 西北核技术研究所 | Centring type angle of attack bullet holder before and after a kind of Balance Gun |
| CN105571936B (en) * | 2015-12-14 | 2018-07-13 | 北京理工大学 | Cylindric 1100~the 1700m/s of fragmentation of 30~40g accelerate bullet support and method |
| CN105571936A (en) * | 2015-12-14 | 2016-05-11 | 北京理工大学 | 30-40g cylindrical fragment 1100-1700m/s acceleration bullet support and method |
| CN105547806A (en) * | 2015-12-14 | 2016-05-04 | 北京理工大学 | Accelerating sabot and method for cylindrical fragment of 20-40g accelerated to speed of 200-1100m/s |
| CN105547059A (en) * | 2015-12-16 | 2016-05-04 | 哈尔滨工业大学 | Sabot capable of realizing pneumatic separation through muzzle cutters |
| CN105547058A (en) * | 2015-12-16 | 2016-05-04 | 哈尔滨工业大学 | Projectile holder separating system based on momentum theorem |
| CN105547058B (en) * | 2015-12-16 | 2017-03-22 | 哈尔滨工业大学 | Projectile holder separating system based on momentum theorem |
| CN108895932A (en) * | 2018-05-10 | 2018-11-27 | 西南科技大学 | For impacting the bullet of the experiment of machanics of gas big gun and testing the device of the velocity of shot |
| CN108955371A (en) * | 2018-07-25 | 2018-12-07 | 北京理工大学 | A kind of bullet support electromagnetic separation of light-gas gun |
| CN112504008B (en) * | 2020-11-27 | 2022-07-01 | 江苏科技大学 | Multi-fragment synchronous launching bullet holder device and assembling method thereof |
| CN113108655A (en) * | 2021-03-22 | 2021-07-13 | 北京理工大学 | Self-separating bullet holder for bullet body with elliptical section |
| CN115235289A (en) * | 2022-06-30 | 2022-10-25 | 江苏恒神股份有限公司 | Composite material bullet holder and forming method |
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|---|---|
| CN100370214C (en) | 2008-02-20 |
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Granted publication date: 20080220 Termination date: 20110429 |