CN210293515U - Turbine shell rocker arm elastic sheet residual force detection tool - Google Patents
Turbine shell rocker arm elastic sheet residual force detection tool Download PDFInfo
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- CN210293515U CN210293515U CN201921509981.7U CN201921509981U CN210293515U CN 210293515 U CN210293515 U CN 210293515U CN 201921509981 U CN201921509981 U CN 201921509981U CN 210293515 U CN210293515 U CN 210293515U
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- turbine shell
- platform
- frock
- force detection
- slide rail
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Abstract
The utility model discloses a turbine shell rocking arm shell fragment residual power detects frock. The utility model discloses in, a turbine shell rocking arm shell fragment residual power detects frock, including controlling the platform, control the right wall mounting of platform and have controlled the ware, the upper surface mounting who controls the platform has the frock platform, the location frock is installed to the upper surface middle part of frock platform, the top of location frock is provided with the turbine shell, the installation section of thick bamboo has all been welded to the upper surface left and right sides of frock platform, install the support pillar in the inner chamber of installation section of thick bamboo, the top welding of two sets of support pillars has the motor installation base, no oil bearing two and no oil bearing one are installed respectively to the upper surface of motor installation base, be provided with guide arm one in the no oil bearing one, the slide rail mount pad is installed to servo motor's drive end, the electric cylinder connector is installed to the upper surface middle part of slide rail mount pad, place the turbine shell cooperation at frock bench surface on the detecting head displacement downwards, and extrude the.
Description
Technical Field
The utility model belongs to the technical field of turbine shell scope, specifically be a turbine shell rocking arm shell fragment residual power detects frock.
Background
The automobile industry is very competitive in machining parts. The demand for large batches of typical products has multiplied, which means that any new advantage will bring a huge return;
taking a turbine shell of the turbocharger as an example, the pressure shell is taken as an important component of the turbocharger, and due to the characteristic that the aluminum part is easy to deform, the accurate detection and reasonable judgment of the contour of the pressure shell profile become problems to be considered in the detection process.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a: in order to solve the problem provided above, a turbine shell rocker arm elastic sheet residual force detection tool is provided.
The utility model adopts the technical scheme as follows:
a turbine shell rocker arm elastic sheet residual force detection tool comprises a control platform, wherein a controller is installed on the right wall of the control platform, a tool platform is installed on the upper surface of the control platform, a positioning tool is installed in the middle of the upper surface of the tool platform, a turbine shell is arranged above the positioning tool, installation cylinders are welded on the left side and the right side of the upper surface of the tool platform, supporting pillars are installed in the inner cavity of the installation cylinders, motor installation bases are welded at the top ends of the two groups of supporting pillars, oil-free bearings II and oil-free bearings I are installed on the upper surface of the motor installation bases respectively, a servo motor is installed in the middle of the upper surface of the motor installation bases, a guide rod I is arranged in each oil-free bearing I, a slide rail installation base is installed at the driving end of the servo motor, and an electric cylinder connector is installed in the middle, and a detection head is arranged below the electric cylinder connector.
And a second guide rod is arranged in a notch of the second oilless bearing, and the bottom of the second guide rod penetrates through the inner cavity of the second oilless bearing and is fixedly connected with the upper surface of the slide rail mounting seat.
The back bottom of the turbine shell is provided with an extrusion plate, the right side of the extrusion plate is provided with a pneumatic rod, the bottom of the pneumatic rod is provided with a pneumatic cavity door, the back of the pneumatic cavity door is provided with a speed regulating valve, and the front vertical face of the pneumatic cavity door is provided with a supporting workpiece.
The soft block is installed at the top end of the supporting workpiece, the bottom end of the supporting workpiece is welded to the upper surface of the tool table, and the soft block is fixedly connected with the bottom end of the extrusion plate.
The supporting legs are installed at the bottom end of the sliding rail installation seat, and the controller is installed on the right wall of the sliding rail installation seat.
The bottom of the guide rod I penetrates through an inner cavity of the oilless bearing I and is fixedly connected with the upper surface of the sliding rail mounting seat.
To sum up, owing to adopted above-mentioned technical scheme, the beneficial effects of the utility model are that:
1. the utility model discloses in, control servo motor's actuating lever downward displacement, and then promote the detecting head downward displacement, wherein guide arm one is used for connecting with the fixed plate of turbine shell top, realizes wholly carrying out downward displacement to fixed plate and detecting head and does control, places detecting head downward displacement on the turbine shell cooperation of frock bench surface to extrude the turbine shell, can do the detection to the pressure of turbine shell.
2. The utility model discloses in, through the support work piece of installation on the back at location frock to the soft piece that connects in the top of supporting the work piece is used for cooperating the stripper plate and connects, installs at the pneumatic chamber door at the support work piece back, receiving the governing valve back of admitting air, will promote pneumatic stem displacement upwards, and promote the stripper plate also displacement upwards, realize the extrusion at the turbine shell back, and the soft piece is a set of hose form, after receiving the pneumatic stem dynamics of upwards, the flexible phenomenon will appear.
Drawings
FIG. 1 is a schematic diagram of the structure of the present invention;
FIG. 2 is a left side view of the present invention;
fig. 3 is a top view of the present invention.
The labels in the figure are: 1. a console; 2. positioning a tool; 3. a slide rail mounting seat; 4. a turbine shell; 5. a probe head; 6. a support pillar; 7. mounting the cylinder; 8. a tooling table; 9. a manipulator; 10. an electric cylinder connector; 11. an oilless bearing I; 12. a servo motor; 13. a first guide rod; 14. a second guide rod; 15. an oilless bearing II; 16. supporting legs; 17. a motor mounting base; 18. a pressing plate; 19. a pneumatic rod; 20. a pneumatic chamber door; 21. a speed regulating valve; 22. supporting a workpiece; 23. and (4) soft blocks.
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 for purposes of illustration only and are not intended to limit the invention.
Referring to fig. 1-3, a turbine shell rocker arm elastic sheet residual force detection tool comprises a control platform 1, a controller 9 is installed on the right wall of the control platform 1, a tool platform 8 is installed on the upper surface of the control platform 1, a positioning tool 2 is installed in the middle of the upper surface of the tool platform 8, a turbine shell 4 is arranged above the positioning tool 2, an extrusion plate 18 is installed at the bottom of the back of the turbine shell 4, a pneumatic rod 19 is installed on the right side of the extrusion plate 18, a pneumatic cavity door 20 is installed at the bottom end of the pneumatic rod 19, a speed regulating valve 21 is installed on the back of the pneumatic cavity door 20, a supporting workpiece 22 is installed on the front vertical surface of the pneumatic cavity door 20, a soft block 23 is installed at the top end of the supporting workpiece 22, the bottom end of the supporting workpiece 22 is welded with the upper surface of the tool platform 8, the soft block 23 is fixedly connected with the bottom end of the extrusion plate 18, the inner cavity of the installation cylinder 7 is internally provided with support pillars 6, the top ends of two groups of support pillars 6 are welded with a motor installation base 17, the upper surface of the motor installation base 17 is respectively provided with an oilless bearing II 15 and an oilless bearing I11, a guide rod II 14 is arranged in a notch of the oilless bearing II 15, the bottom of the guide rod II 14 penetrates through the inner cavity of the oilless bearing II 15 and is fixedly connected with the upper surface of the slide rail installation base 3, the middle part of the upper surface of the motor installation base 17 is provided with a servo motor 12, the guide rod I11 is internally provided with a guide rod I13, the bottom of the guide rod I13 penetrates through the inner cavity of the oilless bearing I11 and is fixedly connected with the upper surface of the slide rail installation base 3, the drive end of the servo motor 12 is provided with the slide rail installation base 3, the bottom end of the slide rail installation base 3 is provided with support legs 16, the right wall, a probe 5 is arranged below the electric cylinder connector 10.
The working principle is as follows: when the detection device is used, the driving rod of the servo motor 12 is controlled to move downwards, the detection head 5 is further pushed to move downwards, the guide rod I13 is used for being connected with the fixing plate above the turbine shell 4, the fixing plate and the detection head 5 are integrally controlled to move downwards, the turbine shell 4 placed on the upper surface of the tooling table 8 is matched with the upper detection head 5 to move downwards, the turbine shell 4 is extruded, and then the pressure of the turbine shell 4 can be detected;
the positioning tools 2 arranged on the left side and the right side of the turbine shell 4 are used for clamping the turbine shell 4;
the method comprises the following specific operations: through the supporting workpiece 22 installed on the back surface of the positioning tool 2, and the soft block 23 connected above the supporting workpiece 22 is used for being matched with the upper extrusion plate 18 to be connected, the pneumatic cavity door 20 installed on the back surface of the supporting workpiece 22 pushes the pneumatic rod 19 to move upwards after being subjected to air inlet by the speed regulating valve 21, and pushes the extrusion plate 18 to move upwards, so that extrusion on the back surface of the turbine shell 4 is realized, and the soft block 23 is in a group of soft pipe shapes, and can stretch out and draw back after being subjected to upward force of the pneumatic rod 19.
The above description is only exemplary of the present invention and should not be taken as limiting the scope of the present invention, as any modifications, equivalents, improvements and the like 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 residual frock of turbine shell rocking arm shell fragment, includes and controls platform (1), its characterized in that: a controller (9) is installed on the right wall of the control platform (1), a tooling platform (8) is installed on the upper surface of the control platform (1), a positioning tool (2) is arranged in the middle of the upper surface of the tool table (8), a turbine shell (4) is arranged above the positioning tool (2), mounting cylinders (7) are welded on the left side and the right side of the upper surface of the tool table (8), supporting struts (6) are arranged in the inner cavity of the mounting cylinder (7), motor mounting bases (17) are welded at the top ends of the two groups of supporting struts (6), the upper surface of the motor mounting base (17) is respectively provided with an oilless bearing II (15) and an oilless bearing I (11), a servo motor (12) is installed in the middle of the upper surface of the motor installation base (17), and a guide rod I (13) is arranged in the oilless bearing I (11);
slide rail mount pad (3) are installed to the drive end of servo motor (12), electric cylinder connector (10) are installed to the upper surface middle part of slide rail mount pad (3), the below of electric cylinder connector (10) is provided with detecting head (5).
2. The turbine shell rocker spring piece residual force detection tool of claim 1, characterized in that: a second guide rod (14) is arranged in a groove opening of the second oilless bearing (15), and the bottom of the second guide rod (14) penetrates through an inner cavity of the second oilless bearing (15) and is fixedly connected with the upper surface of the sliding rail mounting seat (3).
3. The turbine shell rocker spring piece residual force detection tool of claim 1, characterized in that: stripper plate (18) are installed to the back bottom of turbine shell (4), pneumatic rod (19) are installed on the right side of stripper plate (18), pneumatic chamber door (20) are installed to the bottom of pneumatic rod (19), install governing valve (21) on the back of pneumatic chamber door (20), support work piece (22) are installed to the preceding facade of pneumatic chamber door (20).
4. The turbine shell rocker arm elastic piece residual force detection tool of claim 3, characterized in that: soft blocks (23) are installed at the top ends of the supporting workpieces (22), the bottom ends of the supporting workpieces (22) are welded with the upper surface of the tooling table (8), and the soft blocks (23) are fixedly connected with the bottom ends of the extrusion plates (18).
5. The turbine shell rocker spring piece residual force detection tool of claim 1, characterized in that: supporting legs (16) are installed to the bottom of slide rail mount pad (3), install controller (9) on the right wall of slide rail mount pad (3).
6. The turbine shell rocker spring piece residual force detection tool of claim 1, characterized in that: the bottom of the guide rod I (13) penetrates through the inner cavity of the oilless bearing I (11) and is fixedly connected with the upper surface of the sliding rail mounting seat (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921509981.7U CN210293515U (en) | 2019-09-11 | 2019-09-11 | Turbine shell rocker arm elastic sheet residual force detection tool |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921509981.7U CN210293515U (en) | 2019-09-11 | 2019-09-11 | Turbine shell rocker arm elastic sheet residual force detection tool |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210293515U true CN210293515U (en) | 2020-04-10 |
Family
ID=70064618
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921509981.7U Active CN210293515U (en) | 2019-09-11 | 2019-09-11 | Turbine shell rocker arm elastic sheet residual force detection tool |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210293515U (en) |
-
2019
- 2019-09-11 CN CN201921509981.7U patent/CN210293515U/en active Active
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