CN102706216A - Connection structure for speed measurement device of gun muzzle of antiaircraft gun - Google Patents
Connection structure for speed measurement device of gun muzzle of antiaircraft gun Download PDFInfo
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- CN102706216A CN102706216A CN2012100910421A CN201210091042A CN102706216A CN 102706216 A CN102706216 A CN 102706216A CN 2012100910421 A CN2012100910421 A CN 2012100910421A CN 201210091042 A CN201210091042 A CN 201210091042A CN 102706216 A CN102706216 A CN 102706216A
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- gun
- antiaircraft
- measurement device
- muzzle
- speed measurement
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Abstract
The invention discloses an antiaircraft gun accessory, and particularly discloses a connection structure for a speed measurement device of a gun muzzle of an antiaircraft gun. The connection structure comprises a gun muzzle brake and a speed measurement device, wherein the speed measurement device and the front end surface of the gun muzzle brake are fixed in a threaded connection mode by bolts. The connection structure for the speed measurement device of the gun muzzle of the antiaircraft gun has the advantage of being simple in structure and firm in installation; and with the adoption of the connection structure, the speed measurement device and the gun muzzle brake can be conveniently connected into a whole, so that precise measurement of the initial speed of the antiaircraft gun is realized, and meanwhile, the shooting performance of the gun is not affected.
Description
(1) technical field
The present invention relates to antiaircraft antiaircraft gun field, particularly a kind of antiaircraft antiaircraft gun gun muzzle speed measuring device syndeton.
(2) background technology
Present antiaircraft antiaircraft gun is not all installed speed measuring device on the muzzle brake, cause the fried eye-distance that can not accurately control shell to leave, and can not accurately control the distance of detonating between shell and the target, and it is low that target is hit rate, influences antiaircraft effect.
(3) summary of the invention
The present invention for remedy on the existing antiaircraft gun not should technology blank, provide that a kind of high temperature resistant, high pressure, height wash away antiaircraft antiaircraft gun gun muzzle speed measuring device syndeton.
The present invention realizes through following technical scheme:
A kind of antiaircraft antiaircraft gun gun muzzle speed measuring device syndeton is characterized in that: comprise muzzle brake and speed measuring device, be threaded fixing with the front end face of muzzle brake speed measuring device through bolt.
The invention has the beneficial effects as follows: this air defense antiaircraft gun gun muzzle speed measuring device syndeton; Simple in structure; Install firmly, be suitable for the adverse circumstances of the powder gases effect that high temperature, high pressure, height washes away, can be easy speed measuring device and muzzle brake are linked into an integrated entity; Realization is accurately measured shell initial velocity, does not influence the shooting performance of antiaircraft gun self simultaneously.
(4) description of drawings
Below in conjunction with accompanying drawing the present invention is further described.
Accompanying drawing 1 is the structural representation of the present invention's air defense antiaircraft gun gun muzzle speed measuring device syndeton.
Among the figure, 1 muzzle brake, 2 speed measuring devices, 3 bolts.
(5) specific embodiment
Accompanying drawing is a kind of specific embodiment of the present invention.This air defense antiaircraft gun gun muzzle speed measuring device syndeton comprises muzzle brake 1 and speed measuring device 2, is threaded fixing with the front end face of muzzle brake 1 speed measuring device 2 through bolt 3.Earlier the front end face of muzzle brake 1 is processed when mounted and offered screwed hole; Bolt 3 through 8 M6 is threaded fixing with muzzle brake 1 speed measuring device 2 then; Install firmly simply, speed measuring device 2 is installed the device that a kind of bullet tests the speed for antiaircraft antiaircraft gun automatic machine barrel end, through two electromagnetic induction coils the shell that flies through the center is carried out timing; The used unit interval of shell through two electromagnetic induction coil mating reactions will be flown through the center calculates; Resolve the moment flying speed of shell, realize that each bullet of firing through gun muzzle is carried out initial velocity accurately to be measured, realize increasing function and the shooting performance that do not influence antiaircraft gun self.
Claims (1)
1. antiaircraft antiaircraft gun gun muzzle speed measuring device syndeton is characterized in that: comprise muzzle brake (1) and speed measuring device (2), be threaded fixing with the front end face of muzzle brake (1) speed measuring device (2) through bolt (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012100910421A CN102706216A (en) | 2012-03-31 | 2012-03-31 | Connection structure for speed measurement device of gun muzzle of antiaircraft gun |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012100910421A CN102706216A (en) | 2012-03-31 | 2012-03-31 | Connection structure for speed measurement device of gun muzzle of antiaircraft gun |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102706216A true CN102706216A (en) | 2012-10-03 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012100910421A Pending CN102706216A (en) | 2012-03-31 | 2012-03-31 | Connection structure for speed measurement device of gun muzzle of antiaircraft gun |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102706216A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103090722A (en) * | 2013-01-08 | 2013-05-08 | 中国人民解放军海军工程大学 | Installation structure of gyroscope muzzle |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4342961A (en) * | 1980-03-11 | 1982-08-03 | Werkzeugmaschinenfabrik Oerlikon-Buhrle Ag | Apparatus for measuring the muzzle velocity V-null of a projectile fired from a weapon |
| WO1984001224A1 (en) * | 1982-09-24 | 1984-03-29 | Fmc Corp | Muzzle velocimeter |
| US4677376A (en) * | 1982-11-10 | 1987-06-30 | Werkzeugmaschinenfabrik Oerlikon-Buhrle Ag | Apparatus for measuring the muzzle velocity of a projectile fired from a weapon |
| CN2303297Y (en) * | 1997-06-12 | 1999-01-06 | 南京理工大学 | Portable non-target type laser instrument for measuring speed of bullet |
| CN101589289A (en) * | 2006-12-08 | 2009-11-25 | 莱茵金属防空股份公司 | Method for measurement of the muzzle velocity of a projectile or the like |
| CN202547504U (en) * | 2012-03-31 | 2012-11-21 | 中国人民解放军济南军区72465部队 | Connecting structure of air-defense antiaircraft gun muzzle speed measuring device |
-
2012
- 2012-03-31 CN CN2012100910421A patent/CN102706216A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4342961A (en) * | 1980-03-11 | 1982-08-03 | Werkzeugmaschinenfabrik Oerlikon-Buhrle Ag | Apparatus for measuring the muzzle velocity V-null of a projectile fired from a weapon |
| WO1984001224A1 (en) * | 1982-09-24 | 1984-03-29 | Fmc Corp | Muzzle velocimeter |
| US4677376A (en) * | 1982-11-10 | 1987-06-30 | Werkzeugmaschinenfabrik Oerlikon-Buhrle Ag | Apparatus for measuring the muzzle velocity of a projectile fired from a weapon |
| CN2303297Y (en) * | 1997-06-12 | 1999-01-06 | 南京理工大学 | Portable non-target type laser instrument for measuring speed of bullet |
| CN101589289A (en) * | 2006-12-08 | 2009-11-25 | 莱茵金属防空股份公司 | Method for measurement of the muzzle velocity of a projectile or the like |
| CN202547504U (en) * | 2012-03-31 | 2012-11-21 | 中国人民解放军济南军区72465部队 | Connecting structure of air-defense antiaircraft gun muzzle speed measuring device |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103090722A (en) * | 2013-01-08 | 2013-05-08 | 中国人民解放军海军工程大学 | Installation structure of gyroscope muzzle |
| CN103090722B (en) * | 2013-01-08 | 2015-03-25 | 中国人民解放军海军工程大学 | Installation structure of gyroscope muzzle |
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Application publication date: 20121003 |