CN215639054U - High-precision vibration reduction buffering connecting seat for sighting telescope - Google Patents
High-precision vibration reduction buffering connecting seat for sighting telescope Download PDFInfo
- Publication number
- CN215639054U CN215639054U CN202121130426.0U CN202121130426U CN215639054U CN 215639054 U CN215639054 U CN 215639054U CN 202121130426 U CN202121130426 U CN 202121130426U CN 215639054 U CN215639054 U CN 215639054U
- Authority
- CN
- China
- Prior art keywords
- connecting seat
- wall
- elastic piece
- damping
- buffer
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Landscapes
- Telescopes (AREA)
Abstract
The utility model discloses a high-precision vibration-damping buffering connecting seat for a sighting telescope, which comprises a telescope body, a first connecting seat and a second connecting seat, wherein positioning grooves are formed in the outer walls of the two sides of the bottom end of the second connecting seat and the outer walls of the two sides of the top end of the first connecting seat, spring plate assemblies are inserted into the inner walls of the positioning grooves, positioning pins are arranged on the outer walls of the top and the bottom of each spring plate assembly, and the positioning pins are connected with the positioning grooves. The multi-layer vertical elastic piece assembly has the advantages that the front and rear groups of elastic pieces bend after swinging back and forth under the impact, and restore the vertical state to buffer the structure, the multi-layer vertical elastic piece assembly structure is not easy to deform, the zero position is stable and reliable, the buffering effect is improved, the anti-bending capacity of the buffering elastic pieces is strong, the deformation is not easy, the zero position stability of the sighting telescope is good, the sighting precision is high, in addition, the multi-layer elastic pieces have better restoring force and better buffering effect compared with single-layer elastic pieces, the generated zero position walking amount is smaller, and the damping and buffering efficiency of the connecting seat is improved.
Description
Technical Field
The utility model relates to the technical field of sighting telescope, in particular to a high-precision vibration-damping buffer connecting seat for a sighting telescope.
Background
Be equipped with photoelectric conversion device in the gun sight that the individual soldier used, photoelectric conversion device's shock resistance is relatively poor, for this reason, need increase buffer in the gun sight, cushion photoelectric conversion device, the buffer gear that sets up on the mirror gun connecting seat of this patent, the gun sight dress is on the rifle, the gun sight can receive the impact at the shooting in-process, the dividing point in the mirror body can change for the optical axis before and after the gun sight strikes, this change volume is called zero-bit walking volume, the zero-bit walking volume is less, the gun sight precision of gun sight is higher.
Some individual soldier gun sight chooses for use photoelectric conversion device shock resistance relatively poor, need utilize buffer gear to cushion the buffer device, at present, present gun sight gun connecting seat adopts the shell fragment of U type to cushion, this structure takes place the swing in front and back direction, the height direction also can produce the swing, the U-shaped shell fragment swings along the height fore-and-aft direction, can produce unrecoverable deformation, so, can all produce the displacement in two directions of the interior partition of mirror, cause gun sight partition point and initial condition's gun sight partition point to have taken place great change, the zero-position of production is walked about the volume great, the shock attenuation buffer efficiency of connecting seat has been reduced.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a high-precision vibration-damping buffer connecting seat for an aiming lens, which aims to solve the problems in the prior art.
In order to achieve the purpose, the utility model adopts the following technical scheme:
the utility model provides a high accuracy damping buffering connecting seat for gun sight, includes the mirror body, connecting seat one and connecting seat two, the constant head tank has all been seted up to the both sides outer wall of two bottom ends of connecting seat and the both sides outer wall on a connecting seat top, the inner wall of constant head tank has all been pegged graft and has had the shell fragment subassembly, the top and the bottom outer wall of shell fragment subassembly all are provided with the locating pin, the locating pin all is connected with the constant head tank, the locating pin all with the size looks adaptation of constant head tank.
As a further improvement scheme of the technical scheme: circular ports are formed in the outer walls of the two sides of the bottom ends of the connecting seats, and screws are connected to the inner walls of the circular ports through threads.
As a further improvement scheme of the technical scheme: threaded holes are formed in the outer walls of the two sides of the bottom end of the mirror body, and the threaded holes are matched with the size of the screws.
As a further improvement scheme of the technical scheme: the elastic piece assembly comprises an elastic piece I and an elastic piece II, and the elastic piece I and the elastic piece II are made of stainless steel materials.
As a further improvement scheme of the technical scheme: the outer shell is installed to the top outer wall of the mirror body, the top of shell is the arc setting, the size looks adaptation of shell and mirror body.
As a further improvement scheme of the technical scheme: and a bottom plate is fixedly connected to the outer wall of the bottom end of the second connecting seat, and mounting holes are formed in the bottom plate and the outer wall of one side of the second connecting seat.
As a further improvement scheme of the technical scheme: the bottom outer wall of bottom plate is provided with the buffer board, the inner wall packing of buffer board has buffer material.
As a further improvement scheme of the technical scheme: and the connecting seat is positioned right below the connecting seat II, and the outer wall of the top of the screw is sleeved with a sealing plate.
Compared with the prior art, the utility model has the beneficial effects that:
1. the high-precision vibration-damping buffering connecting seat for the sighting telescope is provided with a first connecting seat, a second connecting seat, a spring plate assembly, a telescope body and a positioning pin, wherein the spring plate assembly is connected between the first connecting seat and the second connecting seat through the positioning pin, the second connecting seat is connected at the bottom of the telescope body through a screw, the telescope body is arranged on the telescope body, the telescope body is driven by the vibration of the telescope body when the telescope is started to vibrate and is buffered and absorbed by the multi-layer spring plate assembly serving as a buffering material, the front and rear two groups of spring plates bend after being impacted and swing back and forth and restore the upright state to buffer the structure, the multi-layer upright spring plate assembly is not easy to deform, the zero position is stable and reliable, the buffering effect is increased, the anti-bending capacity of the buffering spring plate is strong, the deformation is not easy, the zero position stability of the sighting telescope is good, the sighting telescope is high in aiming precision, besides, the multi-layer spring plate has better restoring force compared with a single-layer spring plate, and is better in buffering effect, the zero position walking amount of production is less, has improved the shock attenuation buffer efficiency of connecting seat.
2. This be used for gun sight to cushion high accuracy damping connecting seat, through being provided with the mirror body and shell, the shell effectively prevents the entering of outside dust, and protects the inside part, improves the safeguard effect.
3. This be used for gun sight to cushion high accuracy damping connecting seat, through being provided with bottom plate and buffer board, the bottom plate and the buffer board cooperation shell fragment subassembly of a connecting seat bottom further cushion the protection to the structure, improve the buffering effect of connecting seat.
The foregoing description is only an overview of the technical solutions of the present invention, and in order to make the technical solutions of the present invention more clearly understood and to implement them in accordance with the contents of the description, the following detailed description is given with reference to the preferred embodiments of the present invention and the accompanying drawings. The detailed description of the present invention is given in detail by the following examples and the accompanying drawings.
Drawings
The accompanying drawings, which are included to provide a further understanding of the utility model and are incorporated in and constitute a part of this application, illustrate embodiment(s) of the utility model and together with the description serve to explain the utility model without limiting the utility model. In the drawings:
fig. 1 is a cross-sectional front view of the whole structure of a high-precision vibration-damping buffer connecting seat for a sighting telescope, which is provided by the utility model;
FIG. 2 is an enlarged schematic view of the structure A of the high-precision vibration-damping buffer connecting seat for the sighting telescope according to the present invention;
fig. 3 is a front view of the spring assembly structure of the high-precision vibration-damping buffer connecting seat for the sighting telescope.
In the drawings, the components represented by the respective reference numerals are listed below:
1. a mirror body; 2. a housing; 3. positioning pins; 4. a spring plate assembly; 5. positioning a groove; 6. a first connecting seat; 7. a buffer plate; 8. mounting holes; 9. a screw; 10. a threaded hole; 11. a first elastic sheet; 12. a second elastic sheet; 13. and a second connecting seat.
Detailed Description
The principles and features of this invention are described below in conjunction with the following drawings, which are set forth by way of illustration only and are not intended to limit the scope of the utility model. The utility model is described in more detail in the following paragraphs by way of example with reference to the accompanying drawings. Advantages and features of the present invention will become apparent from the following description and from the claims. It is to be noted that the drawings are in a very simplified form and are not to precise scale, which is merely for the purpose of facilitating and distinctly claiming the embodiments of the present invention.
It will be understood that when an element is referred to as being "secured to" another element, it can be directly on the other element or intervening elements may also be present. When a component is referred to as being "connected" to another component, it can be directly connected to the other component or intervening components may also be present. When a component is referred to as being "disposed on" another component, it can be directly on the other component or intervening components may also be present. The terms "vertical," "horizontal," "left," "right," and the like as used herein are for illustrative purposes only.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. The terminology used in the description of the utility model herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the utility model. As used herein, the term "and/or" includes any and all combinations of one or more of the associated listed items.
Referring to fig. 1 to 3, in an embodiment of the present invention, a high-precision vibration damping buffer connection seat for a sighting telescope includes a telescope body 1, a connection seat one 6 and a connection seat two 13, positioning grooves 5 are respectively formed on two outer walls of a bottom end of the connection seat two 13 and two outer walls of a top end of the connection seat one 6, elastic sheet assemblies 4 are respectively inserted into inner walls of the positioning grooves 5, positioning pins 3 are respectively arranged on top and bottom outer walls of the elastic sheet assemblies 4, the positioning pins 3 are respectively connected with the positioning grooves 5, and the positioning pins 3 are respectively matched with sizes of the positioning grooves 5.
Referring to fig. 2, the outer walls of the two sides of the bottom end of the second connecting seat 13 are both provided with circular holes, and the inner walls of the circular holes are both connected with screws 9 through threads.
Referring to fig. 2, the outer walls of the two sides of the bottom end of the mirror body 1 are both provided with threaded holes 10, and the threaded holes 10 are both matched with the size of the screws 9.
Referring to fig. 3, the elastic piece assembly 4 includes an elastic piece one 11 and an elastic piece two 12, and both the elastic piece one 11 and the elastic piece two 12 are made of stainless steel.
Referring to fig. 1, a housing 2 is mounted on the outer wall of the top end of the mirror body 1, the top of the housing 2 is arc-shaped, and the housing 2 is matched with the mirror body 1 in size.
Referring to fig. 1, a bottom plate is fixedly connected to an outer wall of a bottom end of the second connecting seat 13, and mounting holes 8 are formed in the bottom plate and an outer wall of one side of the second connecting seat 13.
Referring to fig. 1, the outer wall of the bottom end of the bottom plate is provided with a buffer plate 7, and the inner wall of the buffer plate 7 is filled with a buffer material, so as to further improve the buffering effect.
Referring to fig. 1, the first connecting seat 6 is located right below the second connecting seat 13, and the top outer wall of the screw 9 is sleeved with the sealing plate.
The working principle of the utility model is as follows: when the high-precision vibration reduction buffering connecting seat for the sighting telescope is required to be used, the elastic piece component 4 is connected between the first connecting seat 6 and the second connecting seat 13 through the positioning pin 3, the second connecting seat 13 is connected to the bottom of the telescope body 1 through the screw 9, the telescope body 1 is installed on the gun, the telescope body 1 is driven to vibrate by the vibration of the telescope body during the gun opening process and is buffered and absorbed by the multilayer elastic piece component 4 serving as a buffering material, the front and the rear two groups of elastic pieces bend after swinging back and forth under the impact and restore the upright state to buffer the structure, the multilayer upright elastic piece component 4 is not easy to deform in structure, the zero position is stable and reliable, the buffering effect is increased, the shell 2 effectively prevents the entering of external dust, and protect internal part, the bottom plate and the buffer board 7 cooperation shell fragment subassembly 4 of 6 bottoms of connecting seat further cushion the protection to the structure, accomplish the use of high accuracy damping buffering connecting seat for gun sight.
Although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that various changes in the embodiments and/or modifications of the utility model can be made, and equivalents and modifications of some features of the utility model can be made without departing from the spirit and scope of the utility model.
Claims (8)
1. The utility model provides a high accuracy damping buffering connecting seat for gun sight, includes the mirror body (1), connecting seat (6) and connecting seat two (13), its characterized in that, constant head tank (5) have all been seted up to the both sides outer wall of connecting seat two (13) bottom and the both sides outer wall on connecting seat (6) top, the inner wall of constant head tank (5) is all pegged graft and is had elastic piece subassembly (4), the top and the bottom outer wall of elastic piece subassembly (4) all are provided with locating pin (3), locating pin (3) all are connected with constant head tank (5), locating pin (3) all with the size looks adaptation of constant head tank (5).
2. The high-precision vibration-damping buffering connecting seat for the sighting telescope according to claim 1, wherein circular holes are formed in the outer walls of the two sides of the bottom end of the second connecting seat (13), and screws (9) are connected to the inner walls of the circular holes through threads.
3. The high-precision vibration-damping buffer connecting seat for the sighting telescope according to claim 1, wherein threaded holes (10) are formed in the outer walls of two sides of the bottom end of the telescope body (1), and the threaded holes (10) are matched with the size of the screws (9).
4. The high-precision vibration-damping buffering connecting seat for the sighting telescope according to claim 1, wherein the elastic piece assembly (4) comprises a first elastic piece (11) and a second elastic piece (12), and the first elastic piece (11) and the second elastic piece (12) are made of stainless steel materials.
5. The high-precision vibration-damping buffer connecting seat for the sighting telescope according to claim 1, wherein a shell (2) is mounted on the outer wall of the top end of the telescope body (1), the top of the shell (2) is arranged in an arc shape, and the shell (2) is matched with the size of the telescope body (1).
6. The high-precision vibration-damping buffering connecting seat for the sighting telescope according to claim 1, wherein a bottom plate is fixedly connected to the outer wall of the bottom end of the second connecting seat (13), and mounting holes (8) are formed in the bottom plate and the outer wall of one side of the second connecting seat (13).
7. A high-precision vibration-damping buffer connecting seat for an aiming telescope according to claim 6, characterized in that the outer wall of the bottom end of the bottom plate is provided with a buffer plate (7), and the inner wall of the buffer plate (7) is filled with buffer material.
8. The high-precision vibration-damping buffer connecting seat for the sighting telescope is characterized in that the first connecting seat (6) is located right below the second connecting seat (13), and a sealing plate is sleeved on the outer wall of the top of each screw (9).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202121130426.0U CN215639054U (en) | 2021-05-25 | 2021-05-25 | High-precision vibration reduction buffering connecting seat for sighting telescope |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202121130426.0U CN215639054U (en) | 2021-05-25 | 2021-05-25 | High-precision vibration reduction buffering connecting seat for sighting telescope |
Publications (1)
Publication Number | Publication Date |
---|---|
CN215639054U true CN215639054U (en) | 2022-01-25 |
Family
ID=79939392
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202121130426.0U Active CN215639054U (en) | 2021-05-25 | 2021-05-25 | High-precision vibration reduction buffering connecting seat for sighting telescope |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN215639054U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113137889A (en) * | 2021-05-25 | 2021-07-20 | 江苏北方湖光光电有限公司 | High-precision vibration reduction buffering connecting seat for sighting telescope |
-
2021
- 2021-05-25 CN CN202121130426.0U patent/CN215639054U/en active Active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113137889A (en) * | 2021-05-25 | 2021-07-20 | 江苏北方湖光光电有限公司 | High-precision vibration reduction buffering connecting seat for sighting telescope |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN215639054U (en) | High-precision vibration reduction buffering connecting seat for sighting telescope | |
CN103712521B (en) | Recoil damping device for firearms | |
CN212567128U (en) | High-efficient dual shock attenuation buffer gear | |
US11913755B2 (en) | Method for shock attenuation device using a pivot mechanism | |
CN113137889A (en) | High-precision vibration reduction buffering connecting seat for sighting telescope | |
CN109937314A (en) | Vibration isolating mechanism, the shooting robot with vibration isolation function | |
CN213599938U (en) | Embedded gun sighting telescope base convenient to install | |
CN107607255A (en) | It is provided with the crash-proof pressure gauge of bezel, cluster | |
CN218002560U (en) | Anti-impact device for cannon inertial navigation installation | |
CN108120342B (en) | Shock attenuation is aimed utensil | |
CN114718988B (en) | Satellite flywheel vibration isolator based on flexible frame body | |
CN107165981B (en) | A kind of dynamic vibration absorber | |
CN109974527A (en) | Explosion-proof energy absorption device | |
CN211059287U (en) | Spring vibration reduction mechanism with quick locking function | |
CN109236925B (en) | Gas linear damping type constant-rigidity vibration isolator | |
CN207984540U (en) | A kind of shock absorption suspension device sub-assembly | |
CN218995778U (en) | Telescope optical lens | |
CN217687249U (en) | Laser sighting device structure | |
CN218443529U (en) | Rotatable folding mechanical sighting device | |
CN111005982A (en) | Spring vibration reduction mechanism with quick locking function | |
CN219622828U (en) | Damping type air compressor | |
CN210036439U (en) | Civil gun aiming anti-seismic focusing mechanism | |
CN110058661A (en) | A kind of mounting structure of computer motherboard vibration-proof mounting | |
CN210397021U (en) | Air compressor with shock-absorbing function | |
US4893412A (en) | Weapon sighting structure |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant |