CN203224346U - Sighting telescope impact testboard - Google Patents
Sighting telescope impact testboard Download PDFInfo
- Publication number
- CN203224346U CN203224346U CN 201320078773 CN201320078773U CN203224346U CN 203224346 U CN203224346 U CN 203224346U CN 201320078773 CN201320078773 CN 201320078773 CN 201320078773 U CN201320078773 U CN 201320078773U CN 203224346 U CN203224346 U CN 203224346U
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- Prior art keywords
- shock
- gun sight
- slide block
- stationary installation
- impact
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Abstract
The utility model discloses a sighting telescope impact testboard. The sighting telescope impact testboard comprises an impact testboard body, and a numerical control device for controlling the impact testboard body to perform a drop test, wherein the impact testboard body comprises a base column, the front end surface of the base column is provided with a fixing device for fixing the sighting telescope, the fixing device is provided with a magnetic conductive block, a sliding block for magnetically connecting the magnetic conductive block is disposed over the fixing device, an impact base for receiving drop impact of the sighting telescope is disposed at the bottom part of the base column, a power device is disposed over the base column and used for controlling the height of the sliding block and controlling the magnetic switch of the sliding block, and the numerical control device is in connection with the power device and is used for issuing a test instruction to the power device. The sighting telescope impact testboard provides a sighting telescope test method with high efficiency and high precision.
Description
Technical field
The utility model relates to the gun sight technical field of measurement and test, relates in particular to a kind of gun sight shock-testing platform.
Background technology
Gun sight claims optical aiming device again, and gun sight mainly is divided into following three major types: the formula of looking in the distance gun sight, collimation formula gun sight, reflex sight are wherein popular with look in the distance formula gun sight and reflex sight again.Gun sight is when bringing great convenience to people, also some inconvenience because people often fall rifle on ground accidentally, has brought influence for the precision of gun sight inevitably, so need be to the gun sight test of falling, so that gun sight can also keep preferable quality, in the prior art behind certain number of times that falls, it mainly is the test of falling manually, this manual test method is poor accuracy not only, and efficient is extremely low, is difficult for promoting the use of.
Therefore, prior art has yet to be improved and developed.
The utility model content
In view of above-mentioned the deficiencies in the prior art, the purpose of this utility model is to provide a kind of gun sight shock-testing platform, is intended to solve that existing gun sight method of testing efficient is low, the problem of poor accuracy.
The technical solution of the utility model is as follows:
A kind of gun sight shock-testing platform, for test that gun sight is fallen, wherein, described gun sight shock-testing platform comprises a shock testing machine body and is used for the numerical control device that the described shock testing machine body of control falls and tests, described shock testing machine body comprises a matrix column, the front end face of described matrix column is provided with one and is used for the fixedly stationary installation of gun sight, described stationary installation is provided with a magnetic inductive block, above described stationary installation, be provided with the slide block that connects described magnetic inductive block for magnetic, be provided with an impact base for the shock of a fall that receives gun sight in the bottom of described matrix column, the top of described matrix column is provided with propulsion system, described propulsion system are used for the height of control slide block and the switch of controlling the magnetic of described slide block, described numerical control device is connected in described propulsion system, is used for sending test instruction to propulsion system.
Described gun sight shock-testing platform, wherein, the front end face of described shock testing machine body is provided with a guide rail, and described stationary installation and slide block are slidingly connected on the described guide rail, and on the vertical direction, the upper end of described guide rail is predetermined oblique angle inwards.
Described gun sight shock-testing platform, wherein, described predetermined angular is 5 degree ~ 10 degree.
Described gun sight shock-testing platform, wherein, upper end and lower end at described guide rail are respectively arranged with upper limit inductor and lower limit inductor, described upper limit inductor is arranged on the top of described slide block, described lower limit inductor is arranged on the below of described slide block, is used for the described slide block of control and moves between upper limit inductor and lower limit inductor.
Described gun sight shock-testing platform wherein, is provided with one and is used for storing the memory storage of shock-testing data in the described numerical control device.
Described gun sight shock-testing platform wherein, arranges a balancing weight that is used for the weight of model gun in the described stationary installation.
Described gun sight shock-testing platform, wherein in, described propulsion system connect described slide block by draught line, control rising and the whereabouts of described slide block by described draught line.
Beneficial effect: the utility model is by arranging a shock testing machine body, matrix column at this shock testing machine body arranges guide rail, pass through fixedly gun sight of a stationary installation then, hold or put down gun sight by numerical control device and propulsion system control magnetic slider, thereby to the gun sight test of falling, proving installation of the present utility model is simple in structure, the design is ingenious, practical, and, method of testing efficient height of the present utility model, accuracy height, can repeat multi-pass operations.
Description of drawings
Fig. 1 is the structural representation of the utility model gun sight shock-testing platform preferred embodiment.
Fig. 2 is the process flow diagram of the utility model gun sight impact test methods preferred embodiment.
Embodiment
The utility model provides a kind of gun sight shock-testing platform, and is clearer, clear and definite for making the purpose of this utility model, technical scheme and effect, below the utility model further described.Should be appreciated that specific embodiment described herein only in order to explaining the utility model, and be not used in restriction the utility model.
See also Fig. 1, Fig. 1 is the structural representation of the utility model gun sight shock-testing platform preferred embodiment, as shown in the figure, it comprises: a shock testing machine body and the numerical control device 100 that falls and test for the described shock testing machine body of control, described shock testing machine body comprises a matrix column 180, the front end face of described matrix column 180 is provided with one and is used for the fixedly stationary installation 150 of gun sight 140, described stationary installation 150 is provided with a magnetic inductive block, above described stationary installation 150, be provided with the slide block 160 that connects described magnetic inductive block for magnetic, be provided with an impact base 120 for the shock of a fall that receives gun sight 140 in the bottom of described matrix column 180, the top of described matrix column 180 is provided with propulsion system 190, described propulsion system 190 are used for the height of control slide block 160 and the switch of controlling the magnetic of described slide block 160, described numerical control device 100 is connected in described propulsion system 190, is used for sending test instruction to propulsion system 190.
Core part of the present utility model is, by the fixing gun sight 140 of stationary installation 150, in stationary installation 150, magnetic inductive block is set then, utilizes the controlled slide block of magnetic 160 to hold or put down stationary installation 150 then, thus the test of falling of the gun sight 140 that control stationary installation 150 is fixed.
The magnetic inductive block that arranges on the described stationary installation 150 can be to carry out the material that magnetic is connected with the slide block 160 of magnetic, and for example iron block etc. can certainly be other materials.Stationary installation 150 of the present utility model not only can play the fixedly effect of gun sight, can also play simultaneously the effect of counterweight, specifically can in described stationary installation 150, be provided for the balancing weight of the weight of model gun, perhaps the weight of direct stationary installation 150 is set to the weight of rifle, thereby be used for the weight of model gun, make the test of falling of gun sight 140 meet true environment more.
The front end face of shock testing machine body of the present utility model is provided with a guide rail 200, and this guide rail 200 is for arranging from top to bottom, and stationary installation 150 and slide block 160 are and are slidingly connected on the described guide rail 200, thereby stationary installation 150 and slide block 160 can be moved up and down.Further, in the vertical direction, the upper end of this guide rail 200 predetermined angular that namely slopes inwardly inwards, the benefit of this set is that stationary installation 150 and slide block 160 can be moved downward or upward along guide rail, and can vertically not drop, without any dependence, cause stationary installation 150, slide block 160, gun sight 140 positions own to change easily, test impacting to falling.Described predetermined angular is preferably 5 degree ~ 10 degree, and this angle can make positions such as stationary installation 150, slide block 160, gun sight 140 can not be shifted, rotation change, and can guarantee again can not impact the test of falling.Preferred, described predetermined angular is 5 degree.
In the utility model, be provided with upper limit inductor 170 and lower limit inductor 130 at described guide rail 200, as its name suggests, upper limit inductor 170 is arranged on the upper end of guide rail 200, lower limit inductor 130 is arranged on the lower end of guide rail 170, more specifically, described upper limit inductor 170 is arranged on the top of described slide block 160, described lower limit inductor 130 is arranged on the below of described slide block 160, described slide block 160 is provided with the slide block inductor, when upper limit inductor 170 and lower limit inductor 130 can be sensed described slide block inductor and move to corresponding position, send control signal to numerical control device 100, stop to provide power to slide block 160 by these numerical control device 200 control propulsion system 190, thereby make slide block 160 can not surpass the position of upper limit inductor 170 and lower limit inductor 130, this can guarantee that slide block 160 moves in predetermined scope, make the gun sight 140 at every turn can both be in the predetermined altitude test of falling.
Be provided with draught line in described propulsion system 190, described propulsion system 190 connect described slide block 160 by this draught line, control rising and the whereabouts of described slide block 160 by this draught line.
In described numerical control device 200, also be provided with memory storage, be used for storing the shock-testing data, described shock-testing data comprise balancing weight weight, testing time etc. falls.After each like this test of falling finished, the data before can also preserving were analyzed use for the user.Be provided with base 110 in the bottom of described matrix column 180, described impact base 120 is arranged on the described base 110.
Based on said apparatus, the utility model also provides a kind of method of testing, and as shown in Figure 2, it comprises step:
S1, numerical control device receive user's input, send the test instruction of the test of falling to propulsion system;
After S2, propulsion system receive described test instruction, control described slide block and move downward, control described slide block magnetic simultaneously and open to hold described stationary installation;
S3, after slide block holds described stationary installation, propulsion system are controlled described slide block and are moved up to predetermined altitude;
S4, propulsion system are controlled described slide block magnetic and are closed to put down described stationary installation, and stationary installation is fallen downwards, with to being fixed on the test of falling of gun sight on the described stationary installation.About existing detailed description the in detail in the concrete ins and outs device in front of described method, repeat no more.
In sum, the utility model is by arranging a shock testing machine body, matrix column at this shock testing machine body arranges guide rail, pass through fixedly gun sight of a stationary installation then, hold or put down gun sight by numerical control device and propulsion system control magnetic slider, thereby to the gun sight test of falling, proving installation of the present utility model is simple in structure, it is ingenious, practical to design, and, method of testing efficient height of the present utility model, accuracy height, can repeat multi-pass operations.
Should be understood that; application of the present utility model is not limited to above-mentioned giving an example; for those of ordinary skills, can be improved according to the above description or conversion, all these improvement and conversion all should belong to the protection domain of the utility model claims.
Claims (7)
1. gun sight shock-testing platform, for test that gun sight is fallen, it is characterized in that, described gun sight shock-testing platform comprises a shock testing machine body and is used for the numerical control device that the described shock testing machine body of control falls and tests, described shock testing machine body comprises a matrix column, the front end face of described matrix column is provided with one and is used for the fixedly stationary installation of gun sight, described stationary installation is provided with a magnetic inductive block, above described stationary installation, be provided with the slide block that connects described magnetic inductive block for magnetic, be provided with an impact base for the shock of a fall that receives gun sight in the bottom of described matrix column, the top of described matrix column is provided with propulsion system, described propulsion system are used for the height of control slide block and the switch of controlling the magnetic of described slide block, described numerical control device is connected in described propulsion system, is used for sending test instruction to propulsion system.
2. gun sight shock-testing platform according to claim 1, it is characterized in that the front end face of described shock testing machine body is provided with a guide rail, described stationary installation and slide block are slidingly connected on the described guide rail, on the vertical direction, the upper end of described guide rail is predetermined oblique angle inwards.
3. gun sight shock-testing platform according to claim 2 is characterized in that, described predetermined angular is 5 degree ~ 10 degree.
4. gun sight shock-testing platform according to claim 2, it is characterized in that, upper end and lower end at described guide rail are respectively arranged with upper limit inductor and lower limit inductor, described upper limit inductor is arranged on the top of described slide block, described lower limit inductor is arranged on the below of described slide block, is used for the described slide block of control and moves between upper limit inductor and lower limit inductor.
5. gun sight shock-testing platform according to claim 1 is characterized in that, is provided with one in the described numerical control device and is used for storing the memory storage of shock-testing data.
6. gun sight shock-testing platform according to claim 1 is characterized in that, a balancing weight that is used for the weight of model gun is set in the described stationary installation.
7. gun sight shock-testing platform according to claim 1 is characterized in that described propulsion system connect described slide block by draught line, controls rising and the whereabouts of described slide block by described draught line.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320078773 CN203224346U (en) | 2013-02-20 | 2013-02-20 | Sighting telescope impact testboard |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320078773 CN203224346U (en) | 2013-02-20 | 2013-02-20 | Sighting telescope impact testboard |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203224346U true CN203224346U (en) | 2013-10-02 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201320078773 Expired - Fee Related CN203224346U (en) | 2013-02-20 | 2013-02-20 | Sighting telescope impact testboard |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203224346U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103134656A (en) * | 2013-02-20 | 2013-06-05 | 深圳市金凯进光电仪器有限公司 | Telescopic sight impact test board and test method |
-
2013
- 2013-02-20 CN CN 201320078773 patent/CN203224346U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103134656A (en) * | 2013-02-20 | 2013-06-05 | 深圳市金凯进光电仪器有限公司 | Telescopic sight impact test board and test method |
| CN103134656B (en) * | 2013-02-20 | 2016-01-20 | 武汉高明兰光电科技有限公司 | A kind of gun sight shock-testing platform and method of testing |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 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: 20131002 Termination date: 20140220 |