CN102620603A - Installation structure of initial-speed measuring coils and time setting coil of air-defense antiaircraft gun muzzle - Google Patents
Installation structure of initial-speed measuring coils and time setting coil of air-defense antiaircraft gun muzzle Download PDFInfo
- Publication number
- CN102620603A CN102620603A CN2012100947303A CN201210094730A CN102620603A CN 102620603 A CN102620603 A CN 102620603A CN 2012100947303 A CN2012100947303 A CN 2012100947303A CN 201210094730 A CN201210094730 A CN 201210094730A CN 102620603 A CN102620603 A CN 102620603A
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- coil
- initial
- time setting
- speed measuring
- initial velocity
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- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The invention relates to the field of air-defense antiaircraft guns, in particular to an installation structure of initial-speed measuring coils and a time setting coil of an air-defense antiaircraft gun muzzle. The installation structure comprises a coil skeleton, wherein the outer-side surface of the coil skeleton is provided with the initial-speed measuring coil A, the initial-speed measuring coil B and the time setting coil in sequence from near to far from a muzzle brake; the initial-speed measuring coil A and the time setting coil are positioned at two ends of the coil skeleton; and the initial-speed measuring coil B is positioned at the middle part of the coil skeleton. The installation structure has the advantages that since the two initial-speed measuring coils and the time setting coil are combined on a same coil supporting body, the appearance size of the whole device is reduced and the structure is more reasonable.
Description
(1) technical field
The present invention relates to antiaircraft antiaircraft gun field, particularly a kind of antiaircraft antiaircraft gun gun muzzle initial velocity is measured coil and is set the coil mounting structure in time.
(2) background technology
Present antiaircraft antiaircraft gun when gun muzzle is installed initial speed measuring device and time faze setting device, need realize that the mounting means that sets coil between initial velocity measurement coil is timely directly has influence on the performance of whole device through electromagnetic induction coil is installed.
(3) summary of the invention
The present invention provides a kind of antiaircraft antiaircraft gun gun muzzle initial velocity measurement coil that three grades of coils are wound on the same body each other to set the coil mounting structure in time in order to remedy the defective of prior art.
The present invention realizes through following technical scheme:
A kind of antiaircraft antiaircraft gun gun muzzle initial velocity is measured coil and is set the coil mounting structure in time; It is characterized in that: comprise coil rack; The coil rack outer surface from the close-by examples to those far off is equipped with initial velocity successively apart from muzzle brake and measures loop A, initial velocity measurement coil B and time setting coil; Initial velocity is measured loop A and the time setting coil is positioned at the coil rack two ends, and initial velocity is measured coil B and is positioned at the coil rack middle part.
The invention has the beneficial effects as follows: this air defense antiaircraft gun gun muzzle initial velocity is measured coil and is set the coil mounting structure in time; Two coils and time setting coil through initial velocity is measured are combined on the same coil support; Whole device appearance and size is reduced, and structure is more reasonable.
(4) description of drawings
Below in conjunction with accompanying drawing the present invention is further described.
Among the figure, 1 initial velocity is measured loop A, and 2 initial velocity are measured coil B, 3 time setting coils, 4 coil racks.
(5) specific embodiment
Accompanying drawing is a kind of specific embodiment of the present invention.
Among Fig. 1; This air defense antiaircraft gun gun muzzle initial velocity is measured coil and is set the coil mounting structure in time; Be that antiaircraft antiaircraft gun carries out a develop skill core component of fire accuracy of technological improvement, comprise coil rack 4, coil rack 4 outer surfaces are equipped with successively from the close-by examples to those far off apart from muzzle brake that initial velocity is measured coil A1, initial velocity is measured coil B2 and time setting coil 3; Initial velocity is measured coil A1 and time setting coil 3 is positioned at coil rack 4 two ends, and initial velocity is measured coil B2 and is positioned at coil rack 4 middle parts.Initial velocity is measured between coil A1 and the initial velocity measurement coil B2 has certain intervals, calculates through the time of the two with bullet, can accurately measure the initial velocity of bullet.Initial velocity is measured between coil B2 and the time setting coil 3 has certain intervals, flies through the two required time as the required time of information processing with bullet, confirms the fuse time installation site.This three coils are installed in the technology on the same supporter, whole device profile is reduced as far as possible, the miniaturization lightweight is installed on existing antiaircraft antiaircraft gun, keeps structure more reasonable.
Claims (1)
1. antiaircraft antiaircraft gun gun muzzle initial velocity is measured coil and is set the coil mounting structure in time; It is characterized in that: comprise coil rack (4); Coil rack (4) outer surface from the close-by examples to those far off is equipped with initial velocity successively apart from muzzle brake and measures loop A (1), initial velocity measurement coil B (2) and time setting coil (3); Initial velocity is measured loop A (1) and time setting coil (3) is positioned at coil rack (4) two ends, and initial velocity is measured coil B (2) and is positioned at coil rack (4) middle part.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012100947303A CN102620603A (en) | 2012-03-31 | 2012-03-31 | Installation structure of initial-speed measuring coils and time setting coil of air-defense antiaircraft gun muzzle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012100947303A CN102620603A (en) | 2012-03-31 | 2012-03-31 | Installation structure of initial-speed measuring coils and time setting coil of air-defense antiaircraft gun muzzle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102620603A true CN102620603A (en) | 2012-08-01 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012100947303A Pending CN102620603A (en) | 2012-03-31 | 2012-03-31 | Installation structure of initial-speed measuring coils and time setting coil of air-defense antiaircraft gun muzzle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102620603A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4672316A (en) * | 1983-08-19 | 1987-06-09 | Werkzeugmaschinenfabrik Oerlikon-Buhrle Ag | Method for calibrating a muzzle velocity measuring device |
| CN1030825A (en) * | 1987-07-20 | 1989-02-01 | 奥拉恩-博勒机械工具公司 | The device of counter in the timing ignition device in the adjusting triggering projectile |
| US6170377B1 (en) * | 1996-04-18 | 2001-01-09 | Bofors Ab | Method and arrangement for programming shells |
| CN2766244Y (en) * | 2005-08-30 | 2006-03-22 | 郦龙 | Device for measuring muzzle projectile velocity |
| US20070074625A1 (en) * | 2005-05-23 | 2007-04-05 | Jens Seidensticker | Method and device for setting the fuse and/or correcting the ignition time of a projectile |
| CN101363699A (en) * | 2007-08-06 | 2009-02-11 | 孙再庸 | Spinning stability fire-fighting rocket bomb, launching set thereof and system |
-
2012
- 2012-03-31 CN CN2012100947303A patent/CN102620603A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4672316A (en) * | 1983-08-19 | 1987-06-09 | Werkzeugmaschinenfabrik Oerlikon-Buhrle Ag | Method for calibrating a muzzle velocity measuring device |
| CN1030825A (en) * | 1987-07-20 | 1989-02-01 | 奥拉恩-博勒机械工具公司 | The device of counter in the timing ignition device in the adjusting triggering projectile |
| US6170377B1 (en) * | 1996-04-18 | 2001-01-09 | Bofors Ab | Method and arrangement for programming shells |
| US20070074625A1 (en) * | 2005-05-23 | 2007-04-05 | Jens Seidensticker | Method and device for setting the fuse and/or correcting the ignition time of a projectile |
| CN2766244Y (en) * | 2005-08-30 | 2006-03-22 | 郦龙 | Device for measuring muzzle projectile velocity |
| CN101363699A (en) * | 2007-08-06 | 2009-02-11 | 孙再庸 | Spinning stability fire-fighting rocket bomb, launching set thereof and system |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C12 | Rejection of a patent application after its publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20120801 |