CN101900512B - Artillery angle control mechanism - Google Patents
Artillery angle control mechanism Download PDFInfo
- Publication number
- CN101900512B CN101900512B CN 200910013227 CN200910013227A CN101900512B CN 101900512 B CN101900512 B CN 101900512B CN 200910013227 CN200910013227 CN 200910013227 CN 200910013227 A CN200910013227 A CN 200910013227A CN 101900512 B CN101900512 B CN 101900512B
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- China
- Prior art keywords
- chute
- control mechanism
- dial
- angle control
- magnetic induction
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Abstract
The invention relates to an artillery angle control mechanism comprising a directional angle control mechanism and a high-low angle control mechanism. The artillery angle control mechanism is characterized in that a dial of the directional angle control mechanism is fixed on a support, two inductive indicators are slidably assembled on a chute of the dial and can arbitrarily slide in the chute, a passive magnetic induction switch is fixed on a supporting board, and a certain distance is kept between the passive magnetic induction switch and the heads of the inductive indicators; and a dial of the high-low angle control mechanism is connected to a fixed sleeve, a chute is arranged on the dial, two inductive indicators are slidably assembled in the chute and can arbitrarily slide in the chute, a passive magnetic induction switch is fixed on the support, and a certain distance is kept between the passive magnetic induction switch and the heads of the inductive indicators. The artillery angle control mechanism has the advantages of simple structure, accurate angle adjustment and sensitive reaction and can avoid wrong launch caused by artillery angle adjusting deviation. The whole device is manually installed, thereby having convenient installation and disassembly.
Description
Technical field
The invention belongs to a kind of safety device of conventional weapon, particularly a kind of artillery angle control mechanism.
Background technology
In traditional cannon training emission process, because the angle adjustment of cannon is the mode by the general orientation adjustment of range estimation mostly, cause the problem that mistakenly launches so often can occur to adjust deviation because of artillery angle.Cannon mistakenly launches the effect that does not only reach training, and can increase training cost.There is no at present the control device that the control artillery angle is adjusted.
Summary of the invention
The objective of the invention is the problem for above-mentioned existence, a kind of artillery angle control mechanism is provided, simple in structure, easy for installation, adjust angle accurate, be quick on the draw, avoid because of mistakenly launching that artillery angle adjustment deviation causes.
In order to realize above-mentioned purpose, the invention provides following technical scheme: it comprises orientation angle controlling organization and high and low angle controlling organization, it is characterized in that: the dial of orientation angle controlling organization is fixed on the support, two inductions of slidingly assemble pointer on the chute of dial, the induction pointer can slide arbitrarily in chute, the passive magnetic induction switch is fixed on the gripper shoe, and passive magnetic induction switch and induction pointer head keep certain distance.The dial of high and low angle controlling organization is connected on the fixed cover, and with chute, two inductions of slidingly assemble pointer in the chute is responded to pointer and can be slided arbitrarily in chute on the dial.The passive magnetic induction switch is fixed on the support, support by up and down two be fixedly set on the height rotating shaft, between passive magnetic induction switch and the induction pointer head certain distance is arranged.
Advantage of the present invention is: simple in structure, adjust angle accurate, and be quick on the draw, can avoid because of mistakenly launching that artillery angle adjustment deviation causes.Whole device all is manual installation, and it is extremely convenient to mount and dismount.
Description of drawings
Fig. 1 is horizontal direction angle control mechanism front view.
Fig. 2 is the top view of Fig. 1.
Fig. 3 is induction pointer schematic diagram.
Fig. 4 is passive magnetic induction switch schematic diagram.
Fig. 5 is high and low angle controlling organization front view.
Fig. 6 is the A-A cutaway view of Fig. 5.
The specific embodiment
The present invention includes orientation angle controlling organization and high and low angle controlling organization two parts, see Fig. 1-4, the orientation angle controlling organization is as follows: dial 2 is fixed on the support 1, two inductions of slidingly assemble pointer 5 on the chute 6 of dial 2, induction pointer 5 adopts existing product, and induction pointer 5 is to be combined by pointer segment 5-1 and permanent magnets 5-2.Induction pointer 5 can be in chute 6 interior any slips.Dial 2 fixedly is assembled on the rotation barrel by attachment screw 8,9.Passive magnetic induction switch 3 is fixed on the gripper shoe 4, gripper shoe 4 is fixed on the barrel pedestal by screw 7, passive magnetic induction switch 3 is existing products, and passive magnetic induction switch 3 is that the magnetic reed switch 3-1 switch housing 3-2 that packs into is formed with switch pedestal 3-3 encapsulation again.Permanent magnets 5-2 end face central alignment on passive magnetic induction switch 3 end faces and the induction pointer 5 also keeps certain distance.See Fig. 5,6, the high and low angle controlling organization is as follows: the dial 11 of high and low angle controlling organization is connected on the fixed cover 10, and with chute 12, two of chute 12 interior slidingly assembles are responded to pointer 5 on the dial 11, and induction pointer 5 can be in chute 12 interior any slips.Dial 11 is by fixed cover 10, attachment screw 15 and be connected folder and 14 fixedly be assembled on the cannon standing part.Passive magnetic induction switch 3 is fixed on the support 13, and support 13 is connected on the rotating part of barrel.Passive magnetic induction switch 3 and induction pointer 5 heads keep certain distance.
Operation principle of the present invention: two precalculated positions fix about first two induction pointers 5 being adjusted to by scale when adjusting gun muzzle horizontal direction angle, driving dial 2 during horizontal direction rotation barrel rotates together with induction pointer 5, turn to precalculated position induction pointer 5 and trigger passive magnetic induction switch 3, passive magnetic induction switch 3 sends alarm signal immediately, by wire alarm signal is reached alarm.Adjusting to up and down by scale two induction pointers 5 first when adjusting gun muzzle high and low angle, two precalculated positions fix, driving passive magnetic induction switch 3 when height rotates barrel rotates together, turn to precalculated position induction pointer 5 and trigger passive magnetic induction switch 3, passive magnetic induction switch 3 sends alarm signal immediately, by wire alarm signal is reached alarm.Claims
Claims (1)
1. artillery angle control mechanism, it comprises orientation angle controlling organization and high and low angle controlling organization, it is characterized in that: the dial of orientation angle controlling organization is fixed on the support, two inductions of slidingly assemble pointer on the chute of dial, the induction pointer can slide arbitrarily in chute, the passive magnetic induction switch is fixed on the gripper shoe, and passive magnetic induction switch and induction pointer head have certain distance; The dial of high and low angle controlling organization is connected on the fixed cover, with chute, two inductions of slidingly assemble pointer in the chute is responded to pointer and can be slided arbitrarily in chute on the dial, the passive magnetic induction switch is fixed on the support, and passive magnetic induction switch and induction pointer head have certain distance.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200910013227 CN101900512B (en) | 2009-08-18 | 2009-08-18 | Artillery angle control mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200910013227 CN101900512B (en) | 2009-08-18 | 2009-08-18 | Artillery angle control mechanism |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN101900512A CN101900512A (en) | 2010-12-01 |
| CN101900512B true CN101900512B (en) | 2013-01-23 |
Family
ID=43226267
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200910013227 Expired - Fee Related CN101900512B (en) | 2009-08-18 | 2009-08-18 | Artillery angle control mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN101900512B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114152140B (en) * | 2021-12-07 | 2023-05-12 | 西安昆仑工业（集团）有限责任公司 | Barrel angle adjusting bracket for fire-proof gun |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2404099Y (en) * | 2000-01-14 | 2000-11-01 | 中国人民解放军55064部队 | Position indicator |
| CN201449217U (en) * | 2009-08-18 | 2010-05-05 | 沈阳重工电器制造有限公司 | Cannon angle control mechanism |
-
2009
- 2009-08-18 CN CN 200910013227 patent/CN101900512B/en not_active Expired - Fee Related
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2404099Y (en) * | 2000-01-14 | 2000-11-01 | 中国人民解放军55064部队 | Position indicator |
| CN201449217U (en) * | 2009-08-18 | 2010-05-05 | 沈阳重工电器制造有限公司 | Cannon angle control mechanism |
Also Published As
| Publication number | Publication date |
|---|---|
| CN101900512A (en) | 2010-12-01 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130123 Termination date: 20130818 |