CN216245844U - Steering and deviation rectifying mechanism for plate spring removing front reticle of sighting telescope - Google Patents
Steering and deviation rectifying mechanism for plate spring removing front reticle of sighting telescope Download PDFInfo
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- CN216245844U CN216245844U CN202122927477.2U CN202122927477U CN216245844U CN 216245844 U CN216245844 U CN 216245844U CN 202122927477 U CN202122927477 U CN 202122927477U CN 216245844 U CN216245844 U CN 216245844U
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Abstract
The utility model relates to the field of sighting telescope, in particular to a steering and deviation rectifying mechanism for a front reticle of a sighting telescope without a leaf spring, which comprises a reticle frame, the dividing frame is of a cylindrical structure, a dividing plate is inserted into one side of the dividing frame, a stabilizing component is arranged on one side of the dividing frame, the device improves the installation stability of the reticle by adding the limiting component on the stabilizing component and in the installation and use process of the reticle, and the installation efficiency, avoids the swinging and the deviation or the damage of the installation of the reticle caused by improper installation force, by arranging the deviation rectifying component on one side of the stabilizing component, when the reticle deviates due to various reasons along with the time, under the effect of inflation gasbag, strengthen the contact between stabilizing ring and the reticle and be connected, cooperate the spacing ring to correct the skew, easy operation, convenient to use is swift.
Description
Technical Field
The utility model relates to the field of sighting telescope, in particular to a steering and deviation rectifying mechanism for a front reticle of a sighting telescope without a leaf spring.
Background
The sighting telescope leaf spring is installed and is used for assisting the accessory of observation angle direction regulation inside the mirror body, the reticle is the thin glass who is carved with the secret line of division on the surface of installing an inside polar book of mirror body, in order to reduce the leading occupation space's of leaf spring problem among the prior art, there is the leading rearmounted auxiliary structure that turns to of leaf spring, because reticle structure itself is thinner, probably take place to exert oneself improper the problem that leads to the reticle installation stable inadequately or damage when the installation, and then under long-time service action, the reticle probably appears becoming flexible, cause the phenomenon of reticle position and the skew of the secret line of division.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a steering deviation correcting mechanism of a front reticle of a sighting telescope without a leaf spring, which aims to solve the problems in the prior art.
In order to achieve the purpose, the utility model provides the following technical scheme: the utility model provides a gun sight removes leading reticle of leaf spring and turns to mechanism of rectifying, the mechanism of rectifying includes:
the dividing frame is of a cylindrical structure;
the reticle is inserted into one side of the inside of the reticle frame;
the stabilizing assembly is arranged on one side in the dividing frame, and one side of the stabilizing assembly is in contact with one side of the dividing plate;
the deviation rectifying assembly is arranged on one side in the dividing frame, and one side of the deviation rectifying assembly is connected with one side of the stabilizing assembly;
and the limiting assembly is sleeved on one side of the dividing frame.
Preferably, the center of the dividing frame is provided with a through hole in a penetrating way, one side in the through hole of the dividing frame is provided with a mounting groove, and the dividing plate is vertically inserted in the mounting groove.
Preferably, the stabilizing component comprises a stabilizing ring, a circular groove is formed in one side of the mounting groove, a plurality of sleeves are symmetrically arranged in the circular groove in a horizontal mode, a plurality of inserting rods are symmetrically arranged on one side of the stabilizing ring, and one sides of the inserting rods are respectively inserted into the sleeves in a splicing mode.
Preferably, the inserted bar is inserted and arranged in the intraductal one side of cover all an organic whole of being equipped with the anticreep board, all cup joints on the sleeve pipe and is equipped with the spring, and spring one side contacts with stabilizer ring one side.
Preferably, the deviation rectifying assembly comprises a transfer air bag and a plurality of expansion air bags, an annular cavity is formed in one side of an annular groove in the dividing frame, the transfer air bag is inserted in the annular cavity, the expansion air bags are respectively inserted in the sleeve and contacted with one side of the inserted rod, and a first vent pipe is connected and arranged between the expansion air bags and the transfer air bag and penetrates through one side of the dividing frame respectively.
Preferably, an air inlet valve is vertically arranged on one side of the upper end of the dividing frame, and a second vent pipe is connected between the air inlet valve and the expansion air bag.
Preferably, spacing subassembly includes the spacing ring, and the spacing ring cup joints reticle frame one side through the screw thread, and just spacing ring one side is pegged graft and is arranged in the mounting groove and contact through gasket and reticle one side.
Compared with the prior art, the utility model has the beneficial effects that:
1. the device improves the mounting stability and mounting efficiency of the reticle and avoids the mounting shaking deviation or damage of the reticle caused by improper mounting force by adding the limiting component on the stabilizing component in the mounting and using process of the reticle;
2. through setting up the subassembly of rectifying on one side of stabilizing the subassembly, when along with the lapse of time, the reticle leads to when squinting because of various reasons, under the effect of inflation gasbag, strengthen the contact between stabilizing ring and the reticle and be connected, the cooperation spacing ring corrects the skew, easy operation, convenient to use is swift.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of portion A of FIG. 1 according to the present invention;
FIG. 3 is a schematic view of the portion B of FIG. 2 according to the present invention.
In the figure: the device comprises a dividing frame 1, a dividing plate 2, a stabilizing ring 3, an annular groove 4, a sleeve 5, an inserted rod 6, an anti-drop plate 7, a spring 8, a transfer air bag 9, an expansion air bag 10, an air inlet valve 11, a limiting ring 12 and a gasket 13.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below. The embodiments of the present invention, and all other embodiments obtained by a person of ordinary skill in the art without any inventive work, belong to the scope of protection of the present invention.
Referring to fig. 1-3, the present invention provides a steering deviation correcting mechanism for a front reticle of a telescope with a leaf spring removed: the mechanism of rectifying includes:
the dividing frame 1 is of a cylindrical structure, a through hole is formed in the center of the dividing frame 1 in a penetrating mode, a mounting groove is formed in one side in the through hole of the dividing frame 1, a dividing plate 2 is vertically inserted into the mounting groove, the dividing plate 2 is inserted into one side in the dividing frame 1, a stabilizing component is arranged on one side in the dividing frame 1, one side of the stabilizing component is in contact with one side of the dividing plate 2 and comprises a stabilizing ring 3, an annular groove 4 is formed in one side in the mounting groove, a plurality of sleeves 5 are horizontally and symmetrically arranged in the annular groove 4, a plurality of inserting rods 6 are symmetrically arranged on one side of the stabilizing ring 3, one sides of the inserting rods 6 are respectively inserted into the sleeves 5, the inserting rods 6 are integrally arranged on one side in the sleeves 5 in an inserting mode, springs 8 are sleeved on the sleeves 5, one side of each spring 8 is in contact with one side of the stabilizing ring 3, and the dividing plate 2 is convenient to mount and dismount, and stability;
the correcting component is arranged on one side in the dividing frame 1, one side of the correcting component is connected with one side of the stabilizing component, the correcting component comprises a transfer air bag 9 and a plurality of expansion air bags 10, an annular cavity is formed in one side of an annular groove 4 in the dividing frame 1, the transfer air bag 9 is inserted in the annular cavity, the expansion air bags 10 are respectively inserted in a sleeve 5 and are contacted with one side of an inserted link 6, a first vent pipe is respectively arranged between the expansion air bags 10 and the transfer air bag 9 and penetrates through one side of the dividing frame 1, an air inlet valve 11 is vertically arranged on one side of the upper end of the dividing frame 1, a second vent pipe is arranged between the air inlet valve 11 and the expansion air bags 10, the limiting component is sleeved on one side of the dividing frame 1 and comprises a limiting ring 12, the limiting ring 12 is sleeved on one side of the dividing frame 1 through threads, one side of the limiting ring 12 is inserted in a mounting groove and is contacted with one side of the dividing plate 2 through a gasket 13, and (5) quickly correcting the deviation of the dividing and dividing plate 2.
The working principle is as follows: during the use, the reticle 2 and the gasket 13 are sequentially inserted into the mounting groove, then the spring 8 clamps the reticle 2 under the rebound effect of the stabilizing ring 3 and under the fixed connection effect of the limiting ring 12, and under the effect of the springs 8, the installation is more stable, the operation is more convenient, when the device is used for a long time, the limiting ring 12 is loosened or the springs 8 are elastically deformed, the centering air bag 9 is inflated through the air inlet valve 11 of a common one-way valve in the prior art, then the air is fed to the expansion air bags 10 in the sleeves 5 through the first air pipes, the expansion is carried out simultaneously, the inserting rod 6 is supported, and then the deviation of the reticle 2 is corrected through the stabilizing ring 3 and the gasket 13, and the stable use state in normal use is kept.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. The utility model provides a gun sight removes leading reticle of leaf spring and turns to mechanism of rectifying which characterized in that: the mechanism of rectifying includes:
the dividing frame (1), the dividing frame (1) is of a cylindrical structure;
the dividing plate (2) is inserted into one side of the dividing frame (1);
the stabilizing assembly is arranged on one side in the dividing frame (1), and one side of the stabilizing assembly is in contact with one side of the dividing plate (2);
the deviation rectifying assembly is arranged on one side in the dividing frame (1), and one side of the deviation rectifying assembly is connected with one side of the stabilizing assembly;
the limiting component is sleeved on one side of the dividing frame (1).
2. The sighting telescope deleading front reticle steering correction mechanism of claim 1, wherein: the center of the dividing frame (1) is penetrated and provided with a through hole, one side in the through hole of the dividing frame (1) is provided with a mounting groove, and the dividing plate (2) is vertically inserted and arranged in the mounting groove.
3. The sighting telescope deleading front reticle steering correction mechanism of claim 2, wherein: the stabilizing component comprises a stabilizing ring (3), a ring groove (4) is formed in one side of the mounting groove, a plurality of sleeves (5) are symmetrically arranged in the ring groove (4) in a horizontal mode, a plurality of inserting rods (6) are symmetrically arranged on one side of the stabilizing ring (3), and one sides of the inserting rods (6) are respectively inserted into the sleeves (5).
4. The sighting telescope deleading front reticle steering correction mechanism of claim 3, wherein: inserted bar (6) are pegged graft and are arranged in equal an organic whole of one side and be equipped with anticreep board (7) in sleeve pipe (5), all cup joint on sleeve pipe (5) and are equipped with spring (8), and spring (8) one side contacts with stabilizing ring (3) one side.
5. The sighting telescope deleading front reticle steering correction mechanism of claim 4, wherein: the deviation rectifying assembly comprises a transfer air bag (9) and a plurality of expansion air bags (10), an annular cavity is formed in one side of an annular groove (4) in the dividing frame (1), the transfer air bag (9) is inserted into the annular cavity, the expansion air bags (10) are inserted into the sleeve (5) respectively and are contacted with one side of an inserted bar (6), and a first vent pipe is connected and arranged between the expansion air bags (10) and the transfer air bag (9) in a penetrating mode and on one side of the dividing frame (1).
6. The sighting telescope deleading front reticle steering correction mechanism of claim 5, wherein: an air inlet valve (11) is vertically arranged on one side of the upper end of the dividing frame (1), and a second vent pipe is connected between the air inlet valve (11) and the expansion air bag (10).
7. The sighting telescope deleading front reticle steering correction mechanism of claim 6, wherein: the limiting assembly comprises a limiting ring (12), the limiting ring (12) is sleeved on one side of the reticle frame (1) through threads, and one side of the limiting ring (12) is inserted into the mounting groove and is contacted with one side of the reticle (2) through a gasket (13).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122927477.2U CN216245844U (en) | 2021-11-25 | 2021-11-25 | Steering and deviation rectifying mechanism for plate spring removing front reticle of sighting telescope |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122927477.2U CN216245844U (en) | 2021-11-25 | 2021-11-25 | Steering and deviation rectifying mechanism for plate spring removing front reticle of sighting telescope |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216245844U true CN216245844U (en) | 2022-04-08 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122927477.2U Active CN216245844U (en) | 2021-11-25 | 2021-11-25 | Steering and deviation rectifying mechanism for plate spring removing front reticle of sighting telescope |
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| CN (1) | CN216245844U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115327760A (en) * | 2022-10-11 | 2022-11-11 | 南通腾峰光学仪器有限公司 | Optical assembly suitable for sighting telescope |
| CN115540688A (en) * | 2022-11-29 | 2022-12-30 | 南通腾峰光学仪器有限公司 | Optical assembly for sighting telescope |
-
2021
- 2021-11-25 CN CN202122927477.2U patent/CN216245844U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115327760A (en) * | 2022-10-11 | 2022-11-11 | 南通腾峰光学仪器有限公司 | Optical assembly suitable for sighting telescope |
| CN115540688A (en) * | 2022-11-29 | 2022-12-30 | 南通腾峰光学仪器有限公司 | Optical assembly for sighting telescope |
| CN115540688B (en) * | 2022-11-29 | 2023-10-20 | 南通腾峰光学仪器有限公司 | Optical assembly for sighting telescope |
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