CN219768040U - Machining and positioning jig for middle shell of automobile turbine - Google Patents
Machining and positioning jig for middle shell of automobile turbine Download PDFInfo
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- CN219768040U CN219768040U CN202321191553.0U CN202321191553U CN219768040U CN 219768040 U CN219768040 U CN 219768040U CN 202321191553 U CN202321191553 U CN 202321191553U CN 219768040 U CN219768040 U CN 219768040U
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- positioning
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- 238000003754 machining Methods 0.000 title claims description 9
- 230000002457 bidirectional effect Effects 0.000 abstract description 15
- 238000010586 diagram Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model relates to the technical field of positioning jigs, in particular to a processing and positioning jig for an automobile turbine intermediate shell, wherein a vertical plate is connected with a positioning mechanism for positioning and fixing the turbine intermediate shell, and is connected with a limiting mechanism for limiting the turbine intermediate shell; one end rotatable being connected to the inside bottom of spout frame of bi-directional screw, the other end fixed connection of bi-directional screw is in the pivot, and the pivot passes the spout frame, and two parallel arrangement's mounting slidable is connected to on the spout frame, has seted up first screw hole on two parallel arrangement's the mounting. According to the utility model, the two fixing pieces are driven to move backwards after the bidirectional screw rod rotates, the two fixing pieces are in contact with the turbine intermediate shell, the two fixing pieces extrude and fix the turbine intermediate shell, and the turbine intermediate shell with different sizes can be positioned and fixed through the two fixing pieces under the limit of the limit mechanism to the turbine intermediate shell.
Description
Technical Field
The utility model relates to the technical field of positioning jigs, in particular to a machining positioning jig for an automobile turbine middle shell.
Background
The jig is a large tool for woodworking, ironwork and other handicraft articles, is mainly used as a tool for assisting in controlling position or action, and in the production and processing process of the middle turbine shell of the automobile, the middle turbine shell needs to be positioned and fixed by adopting the positioning jig, and the existing positioning jig can only fix the middle turbine shell with a single size and cannot be suitable for middle turbine shells with various sizes.
Disclosure of Invention
The utility model aims to solve the defect that the middle turbine shell with various sizes cannot be applied in the prior art, and provides a processing and positioning jig for the middle turbine shell of an automobile.
In order to achieve the above purpose, the present utility model adopts the following technical scheme:
the utility model provides a shell processing location tool in middle of car turbine, includes bottom plate, riser, support piece, positioning mechanism, stop gear and turbine intermediate housing, wherein:
the vertical plate is fixedly connected to the bottom plate, the supporting piece is slidably connected to the bottom plate, the turbine middle shell is arranged on the supporting piece, the vertical plate is connected with the positioning mechanism for positioning and fixing the turbine middle shell, and the vertical plate is connected with the limiting mechanism for limiting the turbine middle shell;
the positioning mechanism comprises a chute frame, two bidirectional screws, a rotating shaft and two fixing pieces which are arranged in parallel, wherein the chute frame is fixedly connected to the vertical plate, one end of each bidirectional screw is rotatably connected to the inner bottom end of the chute frame, the other end of each bidirectional screw is fixedly connected to the corresponding rotating shaft, the rotating shaft penetrates through the chute frame, the two fixing pieces which are arranged in parallel are slidably connected to the chute frame, and the two fixing pieces which are arranged in parallel are provided with first threaded holes which are matched with the corresponding bidirectional screws.
Preferably, the bottom end of the bottom plate is fixedly connected with anti-skid patterns.
Preferably, the support piece comprises a movable block, a connecting plate and a support block, wherein the movable block is slidably connected to the bottom plate, one end of the connecting plate is fixedly connected to the movable block, the other end of the connecting plate is fixedly connected to the support block, and the support block supports the turbine intermediate shell.
Preferably, the fixing piece comprises a moving plate and a protruding block, the moving plate is slidably connected to the chute frame, the moving plate is provided with the first threaded hole, and the protruding block is fixedly connected to the moving plate.
Preferably, the stop gear includes limiting plate, threaded rod and handle, the limiting plate passes on the riser, the rotatable connection of one end of threaded rod to on the riser, the second screw hole has been seted up on the limiting plate, the threaded rod with the second screw hole cooperatees, the other end fixed connection of threaded rod to on the handle.
The utility model provides a processing and positioning jig for an intermediate shell of an automobile turbine, which has the beneficial effects that:
the two fixing pieces are driven to move backwards after the bidirectional screw rod rotates, the two fixing pieces are in contact with the middle turbine shell, the two fixing pieces extrude and fix the middle turbine shell, and the middle turbine shell with different sizes can be positioned and fixed through the two fixing pieces under the limit of the middle turbine shell by the limit mechanism.
Drawings
Fig. 1 is a schematic structural diagram of a positioning fixture for machining an intermediate shell of an automobile turbine;
fig. 2 is a schematic structural diagram of a support member in an automobile turbine intermediate shell processing and positioning jig according to the present utility model;
fig. 3 is a schematic structural diagram of a positioning mechanism in an automobile turbine middle shell processing positioning jig according to the present utility model.
In the figure: the turbine comprises a bottom plate 1, a vertical plate 2, a supporting piece 3, a positioning mechanism 4, a limiting mechanism 5, a turbine middle shell 6, a movable block 31, a connecting plate 32, a supporting block 33, a chute frame 41, a bidirectional screw rod 42, a rotating shaft 43, a fixing piece 44, a moving plate 441, a protruding block 442, a limiting plate 51, a threaded rod 52 and a handle 53.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments.
Example 1
Referring to fig. 1-3, a positioning jig for machining an intermediate shell of an automobile turbine comprises a bottom plate 1, a vertical plate 2, a supporting piece 3, a positioning mechanism 4, a limiting mechanism 5 and an intermediate shell 6 of the turbine, wherein:
the vertical plate 2 is fixedly connected to the bottom plate 1, the vertical plate 2 is used for connecting the positioning mechanism 4, the bottom end of the bottom plate 1 is fixedly connected with anti-skid patterns, the anti-skid patterns are used for increasing friction between the bottom plate 1 and a contact surface, the supporting piece 3 is slidably connected to the bottom plate 1, the supporting piece 3 is used for supporting a turbine intermediate shell 6 which needs to be positioned, the turbine intermediate shell 6 is arranged on the supporting piece 3, the vertical plate 2 is connected with the positioning mechanism 4 which is used for positioning and fixing the turbine intermediate shell 6, and the vertical plate 2 is connected with the limiting mechanism 5 which is used for limiting the turbine intermediate shell 6;
the positioning mechanism 4 comprises a chute frame 41, a bidirectional screw rod 42, a rotating shaft 43 and two fixing pieces 44 which are arranged in parallel, wherein the chute frame 41 is fixedly connected to the vertical plate 2, the chute frame 41 is used for connecting the fixing pieces 44, one end of the bidirectional screw rod 42 is rotatably connected to the inner bottom end of the chute frame 41, the distance between the two fixing pieces 44 is adjusted after the bidirectional screw rod 42 rotates, the other end of the bidirectional screw rod 42 is fixedly connected to the rotating shaft 43, the rotating shaft 43 is used for driving the bidirectional screw rod 42 to rotate, the rotating shaft 43 penetrates through the chute frame 41, the two fixing pieces 44 which are arranged in parallel are slidably connected to the chute frame 41, the fixing pieces 44 are used for fixing the turbine intermediate shell 6, and first threaded holes are formed in the two fixing pieces 44 which are arranged in parallel and are matched with the bidirectional screw rod 42.
The working process comprises the following steps: the turbine intermediate shell 6 is placed on the supporting piece 3, the turbine intermediate shell 6 is driven to move through the supporting piece 3, the turbine intermediate shell 6 of the supporting piece 3 is positioned in front of the positioning mechanism 4, the turbine intermediate shell 6 of the supporting piece 3 is taken down and placed on the fixing piece 44, the turbine intermediate shell 6 is limited through the limiting mechanism 5, the rotating shaft 43 drives the bidirectional screw rod 42 to rotate, the bidirectional screw rod 42 drives the two fixing pieces 44 to move back after rotating, the two fixing pieces 44 are in contact with the turbine intermediate shell 6, the two fixing pieces 44 extrude and fix the turbine intermediate shell 6, the turbine intermediate shell 6 is extruded and fixed through the two fixing pieces 44 under the limit of the turbine intermediate shell 6 by the limiting mechanism 5, and the turbine intermediate shell 6 with different sizes can be positioned and fixed.
Example 2
Referring to fig. 1 to 3, as another preferred embodiment of the present utility model, the difference from embodiment 1 is that the support 3 includes a movable block 31, a connection plate 32 and a support block 33, the movable block 31 is slidably connected to the base plate 1, the movable block 31 is used to move the connection plate 32, one end of the connection plate 32 is fixedly connected to the movable block 31, the connection plate 32 is used to fix the support block 33, the other end of the connection plate 32 is fixedly connected to the support block 33, and the support block 33 supports the turbine intermediate housing 6.
Example 3
Referring to fig. 1 to 3, as another preferred embodiment of the present utility model, the difference from embodiment 1 is that the fixing member 44 includes a moving plate 441 and a protruding block 442, the moving plate 441 is slidably connected to the chute frame 41, the moving plate 441 is used for driving the protruding block 442 to move in a vertical direction, a first threaded hole is formed in the moving plate 441, the protruding block 442 is fixedly connected to the moving plate 441, and the protruding block 442 performs compression fixation on the turbine intermediate shell 6.
Example 4
Referring to fig. 1 to 3, as another preferred embodiment of the present utility model, the difference from embodiment 1 is that the limit mechanism 5 includes a limit plate 51, a threaded rod 52 and a handle 53, the limit plate 51 passes through the riser 2, one end of the threaded rod 52 is rotatably connected to the riser 2, a second threaded hole is formed in the limit plate 51, the threaded rod 52 is matched with the second threaded hole, and the other end of the threaded rod 52 is fixedly connected to the handle 53.
The foregoing is only a preferred embodiment of the present utility model, but the scope of the present utility model is not limited thereto, and any person skilled in the art, who is within the scope of the present utility model, should make equivalent substitutions or modifications according to the technical scheme of the present utility model and the inventive concept thereof, and should be covered by the scope of the present utility model.
Claims (5)
1. The utility model provides a shell processing location tool in middle of car turbine, its characterized in that, including bottom plate (1), riser (2), support piece (3), positioning mechanism (4), stop gear (5) and turbine intermediate casing (6), wherein:
the vertical plate (2) is fixedly connected to the bottom plate (1), the supporting piece (3) is slidably connected to the bottom plate (1), the turbine middle shell (6) is arranged on the supporting piece (3), the vertical plate (2) is connected with the positioning mechanism (4) for positioning and fixing the turbine middle shell (6), and the vertical plate (2) is connected with the limiting mechanism (5) for limiting the turbine middle shell (6);
positioning mechanism (4) include spout frame (41), bi-directional screw (42), pivot (43) and two parallel arrangement's mounting (44), spout frame (41) fixed connection to on riser (2), the rotatable one end of bi-directional screw (42) is connected to the inside bottom of spout frame (41), the other end fixed connection of bi-directional screw (42) is to on pivot (43), pivot (43) pass spout frame (41), two parallel arrangement's mounting (44) slidable connection to on spout frame (41), two parallel arrangement offer first screw hole on mounting (44), first screw hole with bi-directional screw (42) cooperate.
2. The machining and positioning jig for the middle shell of the automobile turbine according to claim 1, wherein the bottom end of the bottom plate (1) is fixedly connected with anti-skid patterns.
3. The machining positioning jig for the middle shell of the automobile turbine according to claim 1, wherein the supporting piece (3) comprises a movable block (31), a connecting plate (32) and a supporting block (33), the movable block (31) is slidably connected to the bottom plate (1), one end of the connecting plate (32) is fixedly connected to the movable block (31), the other end of the connecting plate (32) is fixedly connected to the supporting block (33), and the supporting block (33) supports the middle shell (6) of the turbine.
4. The machining positioning jig for the middle shell of the automobile turbine according to claim 1, wherein the fixing piece (44) comprises a moving plate (441) and a protruding block (442), the moving plate (441) is slidably connected to the chute frame (41), the moving plate (441) is provided with the first threaded hole, and the protruding block (442) is fixedly connected to the moving plate (441).
5. The machining positioning jig for the middle shell of the automobile turbine according to claim 1, wherein the limiting mechanism (5) comprises a limiting plate (51), a threaded rod (52) and a handle (53), the limiting plate (51) penetrates through the vertical plate (2), one end of the threaded rod (52) is rotatably connected to the vertical plate (2), a second threaded hole is formed in the limiting plate (51), the threaded rod (52) is matched with the second threaded hole, and the other end of the threaded rod (52) is fixedly connected to the handle (53).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202321191553.0U CN219768040U (en) | 2023-05-17 | 2023-05-17 | Machining and positioning jig for middle shell of automobile turbine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202321191553.0U CN219768040U (en) | 2023-05-17 | 2023-05-17 | Machining and positioning jig for middle shell of automobile turbine |
Publications (1)
Publication Number | Publication Date |
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CN219768040U true CN219768040U (en) | 2023-09-29 |
Family
ID=88110249
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN202321191553.0U Active CN219768040U (en) | 2023-05-17 | 2023-05-17 | Machining and positioning jig for middle shell of automobile turbine |
Country Status (1)
Country | Link |
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CN (1) | CN219768040U (en) |
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2023
- 2023-05-17 CN CN202321191553.0U patent/CN219768040U/en active Active
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