CN211085311U - Survey chartered plane with shock attenuation safeguard function - Google Patents

Survey chartered plane with shock attenuation safeguard function Download PDF

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Publication number
CN211085311U
CN211085311U CN201922158912.2U CN201922158912U CN211085311U CN 211085311 U CN211085311 U CN 211085311U CN 201922158912 U CN201922158912 U CN 201922158912U CN 211085311 U CN211085311 U CN 211085311U
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China
Prior art keywords
shock attenuation
fixedly connected
plate
chartered plane
shock
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CN201922158912.2U
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Chinese (zh)
Inventor
吴刚
林明高
苏敬森
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Kunshan Junyucheng Precision Mould Co ltd
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Kunshan Junyucheng Precision Mould Co ltd
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Priority to CN201922158912.2U priority Critical patent/CN211085311U/en
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Abstract

The utility model discloses a survey chartered plane with shock attenuation safeguard function, including the shock attenuation seat, the below of shock attenuation seat is equipped with the shock attenuation board, symmetrical through-hole has been seted up to the upper surface of shock attenuation board, the symmetrical support column of bottom surface fixedly connected with of shock attenuation seat, every the bottom of support column all runs through the through-hole and extends to the below of shock attenuation board, the symmetrical bumper shock absorber of last fixed surface fixedly connected with of shock attenuation board, the top of bumper shock absorber and the bottom surface fixed connection of shock attenuation seat, the inside of shock attenuation seat is equipped with the fixed plate, the equal fixedly connected with sliding plate of the left and right sides face of fixed plate. This survey chartered plane with shock attenuation protect function utilizes vertical shock-absorbing structure and horizontal shock-absorbing structure to combine together, and the effectual vibration range of surveying chartered plane body at the during operation that has reduced has improved the shock attenuation effect, has solved present survey chartered plane and has not had the function of shock attenuation protection, long-time being in under the vibration power work, will damage the problem of equipment.

Description

Survey chartered plane with shock attenuation safeguard function
Technical Field
The utility model belongs to the electronics field of making especially relates to a survey chartered plane with shock attenuation safeguard function.
Background
The electronic manufacturing adopts advanced electronic technology to carry out production and processing flow, survey the chartered plane that will use usually in the electronic manufacturing, survey the chartered plane and be used for detecting and encapsulating electronic component, in electronic component's production, survey the chartered plane and because the operation of machine will produce very big vibration in the use, influence the device's stability, lead to when detecting and encapsulating, it is inaccurate to detect data, but present survey chartered plane does not have the function of shock attenuation protection yet, long-time being in under the vibration power work, will damage equipment, consequently for solving above problem, we provide a survey chartered plane with shock attenuation protect function.
SUMMERY OF THE UTILITY MODEL
The utility model provides a, aim at solving above-mentioned current survey chartered plane and do not have the function of shock attenuation protection, long-time being in under the vibration power work, will damage the problem of equipment.
The utility model is realized in such a way, a survey chartered plane with shock attenuation safeguard function, including the cushion socket, the below of cushion socket is equipped with the shock attenuation board, the upper surface of shock attenuation board has seted up symmetrical through-hole, the bottom surface of cushion socket is fixedly connected with symmetrical support column, the bottom of each support column all runs through the through-hole and extends to the below of shock attenuation board, the upper surface of cushion socket is fixedly connected with symmetrical bumper shock absorber, the top of bumper shock absorber is fixedly connected with the bottom surface of cushion socket, the inside of cushion socket is equipped with the fixed plate, the left and right sides face of fixed plate all is fixedly connected with the sliding plate, two sides face that the sliding plate kept away from each other all is fixedly connected with the shell fragment, two sides face that the shell fragment kept away from each other all is fixedly connected with the inside wall of cushion socket, the upper surface of fixed plate, the upper surface fixed connection of backup pad has the buffer board, the upper surface fixed connection of buffer board has the mounting panel, the bottom surface fixedly connected with symmetrical hydraulic damper of mounting panel, every the bottom of hydraulic damper all is connected with the upper surface fixed connection of shock attenuation seat, the top of mounting panel is equipped with surveys chartered plane body.
Every the equal fixedly connected with universal wheel in bottom of support column, every the surface of support column all is equipped with damping spring.
The bottom surface fixedly connected with buffer spring of shock attenuation seat, buffer spring's bottom and the last fixed surface of shock attenuation board are connected.
Symmetrical chutes are formed in the inner bottom wall of the shock absorption seat and the inner top wall of the shock absorption seat, sliding blocks matched with the chutes are clamped in the chutes, and the top end of each sliding plate and the bottom end of each sliding plate are fixedly connected with one side face, close to the two sliding blocks, of each sliding plate.
Symmetrical threaded holes are formed in the front face of the mounting plate, and the bag measuring machine body is fixedly connected with the mounting plate through bolts.
The front of the shock absorption seat is fixedly connected with a cover plate through screws, and the front of the cover plate is provided with air holes which are arranged at equal intervals.
Compared with the prior art, the beneficial effects of the utility model are that: the shock absorber and the buffer spring are arranged below the shock absorption seat, the shock absorption plate can be matched to buffer vertical vibration force, the shock absorption plate can transmit the vibration force to the fixed plate in the moving process through the action of the support column, the through hole and the shock absorption spring, the vibration force generated in the moving process of the device is reduced by the matching of the shock absorption spring, the universal wheel is arranged at the bottom end of the support column, the pushing device can be conveniently pushed to move, the use flexibility is improved, the elastic piece is arranged in the shock absorption seat, the transverse shock absorption effect is realized by the elastic piece matched with the sliding plate and the fixed plate, meanwhile, the stability of the shock absorption structure is ensured by the matching of the sliding groove and the sliding block, the stability of the device is improved, the support plate is connected with the mounting plate through the buffer plate, and the mounting plate further buffers the vibration force by the action of, the amplitude of vibrations has been reduced, and the device utilizes vertical shock-absorbing structure and horizontal shock-absorbing structure to combine together, and the effectual vibration amplitude of surveying chartered plane body at the during operation that has reduced has improved the shock attenuation effect, has solved present survey chartered plane and has not had the function of shock attenuation protection, long-time being in under the vibration power work, will damage the problem of equipment.
Drawings
Fig. 1 is a sectional view of the front view of the shock-absorbing seat of the present invention;
FIG. 2 is a front view of the shock mount of the present invention;
fig. 3 is a top view of the mounting plate of the present invention.
In the figure: 1. a damper plate; 2. a shock absorbing seat; 3. a slider; 4. a fixing plate; 5. a chute; 6. a support plate; 7. a buffer plate; 8. a bag measuring machine body; 9. a bolt; 10. mounting a plate; 11. a hydraulic damper; 12. a sliding plate; 13. a spring plate; 14. a support pillar; 15. a through hole; 16. a damping spring; 17. a universal wheel; 18. a buffer spring; 19. a shock absorber; 20. air holes are formed; 21. a screw; 22. a cover plate; 23. a threaded bore.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more clearly understood, the present invention is further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
In the description of the present invention, it is to be understood that the terms "length", "width", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on those shown in the drawings, and are merely for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention. In addition, in the description of the present invention, "a plurality" means two or more unless specifically limited otherwise.
Referring to fig. 1-3, a bag measuring machine with shock absorption and protection functions comprises a shock absorption seat 2, a shock absorption plate 1 is arranged below the shock absorption seat 2, symmetrical through holes 15 are formed in the upper surface of the shock absorption plate 1, symmetrical support columns 14 are fixedly connected to the bottom surface of the shock absorption seat 2, the bottom end of each support column 14 penetrates through the through hole 15 and extends to the lower side of the shock absorption plate 1, symmetrical shock absorbers 19 are fixedly connected to the upper surface of the shock absorption plate 1, the top ends of the shock absorbers 19 are fixedly connected to the bottom surface of the shock absorption seat 2, a fixed plate 4 is arranged inside the shock absorption seat 2, sliding plates 12 are fixedly connected to the left side surface and the right side surface of the fixed plate 4, elastic pieces 13 are fixedly connected to one side surface far away from each other of the two sliding plates 12, one side surface far away from each other of the two elastic pieces 13 is fixedly connected to, fixed surface is connected with buffer board 7 for backup pad 6, and fixed surface is connected with mounting panel 10 for buffer board 7, and the symmetrical hydraulic damper 11 of bottom surface fixedly connected with of mounting panel 10, the bottom of every hydraulic damper 11 all with the last fixed surface of cushion socket 2 be connected, the top of mounting panel 10 is equipped with surveys chartered plane body 8.
The utility model discloses in, the equal fixedly connected with universal wheel 17 in bottom of every support column 14, the surface of every support column 14 all overlaps and is equipped with damping spring 16, can make things convenient for the device to remove, reduce the vibrational force of removal in-process, the bottom surface fixedly connected with buffer spring 18 of cushion socket 2, buffer spring 18's bottom and damping plate 1's last fixed surface are connected, can further improve buffering effect, symmetrical spout 5 has all been seted up to the inner bottom wall of cushion socket 2 and the interior roof of cushion socket 2, the equal joint in inside of every spout 5 has the slider 3 with 5 looks adaptations of spout, a side fixed connection that the top of every sliding plate 12 and the bottom of sliding plate 12 are close to each other with two sliders 3 respectively, damping device's stability can be guaranteed.
Symmetrical screw hole 23 is seted up in the front of mounting panel 10, surveys chartered plane body 8 and passes through bolt 9 and mounting panel 10 fixed connection, can be convenient for install and fix, convenient dismantlement, and screw 21 fixedly connected with apron 21 is passed through in the front of cushion socket 2, and the bleeder vent 20 that the equidistance was arranged is seted up in the front of apron 21, can realize the ventilative effect of ventilating.
The utility model discloses a theory of operation is: when in use, the bag measuring machine body 8 is fixedly arranged on the mounting plate 10 through the threaded hole 23 and the bolt 9, then the bag measuring machine body 8 is connected with a power supply, the bag measuring machine body 8 is started, the bag measuring machine body 8 vibrates during working, the vibration force is primarily buffered through a hydraulic damper 11, meanwhile, the buffer plate 7 and the supporting plate 6 are connected with the fixed plate 4, the fixed plate 4 counteracts and weakens the transverse vibration force through the sliding plate 12 under the matching of the sliding chute 5 and the sliding block 3 by using the elastic sheet 13, the shock absorber 19 and the buffer spring 18 are arranged below the shock absorption seat 2, and can be matched with the shock absorption plate 1 to realize the buffer of vertical vibration force, through the effect of support column 14, through-hole 15 and damping spring 16, can guarantee to survey chartered plane body 8 and on removing in-process support column 14 transmission vibrations power to damper plate 1, utilize damping spring 16's cooperation, reduced the vibrational force that the device produced at the removal in-process.
The above description is only exemplary of the present invention and should not be construed as limiting the present invention, and any modifications, equivalents and improvements made within the spirit and principles of the present invention are intended to be included within the scope of the present invention.

Claims (6)

1. The utility model provides a survey chartered plane with shock attenuation safeguard function, includes cushion socket (2), its characterized in that: a damping plate (1) is arranged below the damping seat (2), symmetrical through holes (15) are formed in the upper surface of the damping plate (1), symmetrical supporting columns (14) are fixedly connected to the bottom surface of the damping seat (2), the bottom end of each supporting column (14) penetrates through the through hole (15) and extends to the lower portion of the damping plate (1), symmetrical dampers (19) are fixedly connected to the upper surface of the damping plate (1), the top ends of the dampers (19) are fixedly connected with the bottom surface of the damping seat (2), a fixed plate (4) is arranged inside the damping seat (2), sliding plates (12) are fixedly connected to the left side surface and the right side surface of the fixed plate (4), elastic pieces (13) are fixedly connected to one side surface, far away from each other, of the two elastic pieces (13) are fixedly connected to the inner side wall of the damping seat (2), the upper surface fixed connection of fixed plate (4) has backup pad (6), the upper surface fixed connection of backup pad (6) has buffer board (7), the upper surface fixed connection of buffer board (7) has mounting panel (10), the symmetrical hydraulic damper (11) of bottom surface fixedly connected with of mounting panel (10), every the bottom of hydraulic damper (11) all is connected with the upper surface fixed connection of vibration damping seat (2), the top of mounting panel (10) is equipped with surveys chartered plane body (8).
2. The chartered plane of surveying with shock attenuation safeguard function of claim 1 characterized in that: the bottom of every support column (14) all fixedly connected with universal wheel (17), every the surface of support column (14) all overlaps and is equipped with damping spring (16).
3. The chartered plane of surveying with shock attenuation safeguard function of claim 1 characterized in that: the damping plate is characterized in that a buffering spring (18) is fixedly connected to the bottom surface of the damping seat (2), and the bottom end of the buffering spring (18) is fixedly connected with the upper surface of the damping plate (1).
4. The chartered plane of surveying with shock attenuation safeguard function of claim 1 characterized in that: symmetrical sliding grooves (5) are formed in the inner bottom wall of the shock absorption seat (2) and the inner top wall of the shock absorption seat (2), sliding blocks (3) matched with the sliding grooves (5) are clamped in the sliding grooves (5), and the top end of each sliding plate (12) and the bottom end of each sliding plate (12) are fixedly connected with one side face, close to the two sliding blocks (3), of each sliding plate.
5. The chartered plane of surveying with shock attenuation safeguard function of claim 1 characterized in that: symmetrical threaded holes (23) are formed in the front face of the mounting plate (10), and the bag measuring machine body (8) is fixedly connected with the mounting plate (10) through bolts (9).
6. The chartered plane of surveying with shock attenuation safeguard function of claim 1 characterized in that: the front surface of the shock absorption seat (2) is fixedly connected with a cover plate (22) through screws (21), and the front surface of the cover plate (22) is provided with air holes (20) which are arranged at equal intervals.
CN201922158912.2U 2019-12-05 2019-12-05 Survey chartered plane with shock attenuation safeguard function Active CN211085311U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201922158912.2U CN211085311U (en) 2019-12-05 2019-12-05 Survey chartered plane with shock attenuation safeguard function

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201922158912.2U CN211085311U (en) 2019-12-05 2019-12-05 Survey chartered plane with shock attenuation safeguard function

Publications (1)

Publication Number Publication Date
CN211085311U true CN211085311U (en) 2020-07-24

Family

ID=71644004

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201922158912.2U Active CN211085311U (en) 2019-12-05 2019-12-05 Survey chartered plane with shock attenuation safeguard function

Country Status (1)

Country Link
CN (1) CN211085311U (en)

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