CN211681977U - Aircraft special-shaped part centre gripping frock - Google Patents
Aircraft special-shaped part centre gripping frock Download PDFInfo
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- CN211681977U CN211681977U CN201922489501.1U CN201922489501U CN211681977U CN 211681977 U CN211681977 U CN 211681977U CN 201922489501 U CN201922489501 U CN 201922489501U CN 211681977 U CN211681977 U CN 211681977U
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Abstract
The utility model provides an aircraft special-shaped part centre gripping frock, belongs to the fixed technical field of aircraft opposite sex part, including PMKD, fixing hole, adjusting device, activity piece, elevating gear, fixed bolster, clamping device, its characterized in that: the middle of the left edge and the right edge of the upper top end surface of the fixed bottom plate is provided with a fixed through hole, each fixed through hole is connected with an adjusting device in the middle of the front top end surface inside, a movable support block is inserted in the top end surface of the side of the adjusting device, a lifting device is inserted in the middle of the top end surface of the left side of the movable support block, a fixed support is fixedly connected to the right side of the upper top end surface of the lifting device, a clamping device is inserted in the middle of the left edge of the upper top end surface of the fixed support block, a worker can adjust the front position and the rear position of the fixator at any time according to the position.
Description
The technical field is as follows:
the utility model belongs to the technical field of the fixed apparatus of aircraft special-shaped part, concretely relates to aircraft special-shaped part centre gripping frock.
Background art:
in long-term work practice, during the staff fixes the workstation with special-shaped part, current fixer need be installed on the processing platform according to the circular arc position to the work piece of co-altitude need select the fixer that is fit for the height after measuring the height, inconvenient staff's operation use and reduction work efficiency.
The utility model has the following contents:
the utility model aims at: in order to solve the staff with special-shaped part fixed work platform in-process, the staff can adjust fixer front and back position at any time according to the circular arc position to the staff can be quick regulation fixer height at any time, makes things convenient for the staff to operate and use and improves work efficiency, its technical scheme as follows:
the utility model provides an aircraft special-shaped part centre gripping frock, it includes PMKD 1, fixing hole 2, adjusting device 3, activity piece 4, elevating gear 5, fixed bolster 6, clamping device 7, its characterized in that: the middle of the left edge and the right edge of the top end surface of the fixed bottom plate 1 is respectively provided with a fixed through hole 2, the middle of the front top end surface inside each fixed through hole 2 is connected with an adjusting device 3, the top end surface of the side of the adjusting device 3 is inserted with a movable support block 4, the middle of the top end surface of the left side of the movable support block 4 is inserted with a lifting device 5, the right side of the top end surface of the lifting device 5 is fixedly connected with a fixed support 6, the middle of the left edge of the top end surface of the fixed support 6 is inserted with a clamping device 7, the adjusting device 3 comprises a lead screw 3-1, a bearing 3-2 and a rotary table 3-3, the front edge and the rear part of the top end surface of the lead screw 3-1 are symmetrically inserted with the bearing 3-2 respectively, and the circle center of the top end surface, the screw rod 3-1 penetrates through the rear top end surface of the fixed bottom plate 1 to be inserted into the fixed through hole 2 and is inserted into the middle of the front top end surface in the fixed through hole 2, the movable support block 4 comprises an upright post 4-1, a threaded hole 4-2, a sliding hole 4-3, a threaded post 4-4 and an adjusting disc 4-5, the threaded hole 4-2 is arranged in the middle of the lower edge of the top end surface on the left side of the upright post 4-1, the sliding hole 4-3 is arranged in the middle above the front top end surface of the upright post 4-1, the threaded post 4-4 is inserted into the middle of the top end surface on the upright post 4-1, the adjusting disc 4-5 is fixedly connected to the circle center of the top end surface on the threaded post 4-4, and the threaded hole 4-2 is inserted into the side surface of, the threaded column 4-4 penetrates through the upper surface of the upright column 4-1 and is inserted into the lower top end surface inside the sliding hole 4-3, the lifting device 5 comprises a support block 5-1, a sliding block 5-2 and an insertion hole 5-3, the sliding block 5-2 is fixedly connected to the middle of the top end surface of the rear side of the support block 5-1, the insertion hole 5-3 is arranged in the middle of the right edge of the top end surface of the sliding block 5-2, the insertion hole 5-3 is inserted into the side surface of the threaded column 4-4, internal threads are arranged on the inner side surface of the insertion hole 5-3, the upper surface of the support block 5-1 is in an arc shape, the clamping device 7 comprises a lifting column 7-1, a rotating block 7-2 and a pressing block 7-3, the rotating block 7-2 is fixedly connected to the circle center of the top end surface of the lifting column 7, a pressing block 7-3 is fixedly connected to the circle center of the surface of the lower top end of the lifting column 7-1, and the lifting column 7-1 is inserted in the middle of the left edge of the surface of the upper top end of the fixed support 6.
The utility model has the advantages that: in order to solve the problem that a worker fixes a special-shaped part on a workbench, the worker can adjust the front position and the rear position of a fixer at any time according to the arc position, the height of the fixer can be adjusted quickly by the worker at any time, and the worker can operate and use the fixer conveniently and improve the working efficiency.
Description of the drawings:
fig. 1 is a schematic view of the overall structure of the present invention;
fig. 2 is a schematic structural diagram of the adjusting device 3 of the present invention;
fig. 3 is a schematic structural view of the movable supporting block 4 of the present invention;
fig. 4 is a schematic structural view of the lifting device 5 of the present invention;
fig. 5 is a schematic structural view of the clamping device 7 of the present invention.
The specific implementation mode is as follows:
referring to fig. 1, fig. 2, fig. 3, fig. 4, fig. 5, an aircraft special-shaped part clamping tool includes a fixed base plate 1, a fixed through hole 2, an adjusting device 3, a movable support block 4, a lifting device 5, a fixed support 6, and a clamping device 7, and is characterized in that: the middle of the left edge and the right edge of the top end surface of the fixed bottom plate 1 is respectively provided with a fixed through hole 2, the middle of the front top end surface inside each fixed through hole 2 is connected with an adjusting device 3, the top end surface of the side of the adjusting device 3 is inserted with a movable support block 4, the middle of the top end surface of the left side of the movable support block 4 is inserted with a lifting device 5, the right side of the top end surface of the lifting device 5 is fixedly connected with a fixed support 6, the middle of the left edge of the top end surface of the fixed support 6 is inserted with a clamping device 7, the adjusting device 3 comprises a lead screw 3-1, a bearing 3-2 and a rotary table 3-3, the front edge and the rear part of the top end surface of the lead screw 3-1 are symmetrically inserted with the bearing 3-2, the rotary table 3-3 is fixedly connected with the center of the top end surface of the rear end of the lead screw 3-, the movable support block 4 comprises an upright post 4-1, a threaded hole 4-2, a sliding hole 4-3, a threaded post 4-4 and an adjusting disc 4-5, the threaded hole 4-2 is arranged in the middle of the lower edge of the top end surface of the left side of the upright post 4-1, the sliding hole 4-3 is arranged in the middle of the upper portion of the top end surface of the front side of the upright post 4-1, the threaded post 4-4 is inserted in the middle of the top end surface of the upright post 4-1, the adjusting disc 4-5 is fixedly connected to the circle center of the top end surface of the upper portion of the threaded post 4-4, the threaded hole 4-2 is inserted in the side surface of the screw rod 3-1, and the threaded post 4-4 penetrates through the upper surface of the upright post 4-1 and is inserted in the lower top end surface of the sliding hole 4-3, the lifting device 5 comprises a support block 5-1, a sliding block 5-2 and an insertion hole 5-3, the sliding block 5-2 is fixedly connected to the middle of the top end surface of the rear side of the support block 5-1, the insertion hole 5-3 is arranged in the middle of the right edge of the top end surface of the sliding block 5-2, the insertion hole 5-3 is inserted into the side surface of the threaded column 4-4, internal threads are arranged on the inner side surface of the insertion hole 5-3, the upper surface of the support block 5-1 is in a circular arc shape, the clamping device 7 comprises a lifting column 7-1, a rotating block 7-2 and a pressing block 7-3, the rotating block 7-2 is fixedly connected to the center of the top end surface of the lifting column 7-1, the pressing block 7-3 is fixedly connected to the center of the bottom end surface of the lifting column 7-1, the lifting column 7-1 is inserted in the middle of the left edge of the top surface of the fixed bracket 6.
When the device is used, firstly, the fixed base plate 1 is placed on a workbench, then the turntable 3-3 on the adjusting device 3 is held and rotated, meanwhile, the screw rod 3-1 rotates in the bearing 3-2, meanwhile, the screw rod 3-1 rotates in the threaded hole 4-2 on the movable supporting block 4, meanwhile, the upright post 4-1 moves back and forth and is adjusted to a proper position, then the adjusting disc 4-5 is rotated to enable the threaded post 4-4 to rotate in the sliding hole 4-3, meanwhile, the threaded post 4-4 rotates in the inserting hole 5-3 on the lifting device 5 and drives the sliding block 5-2 to move up and down in the sliding hole 4-3, then, after the proper height is adjusted, a workpiece is placed on the upper surface of the supporting block 5-1, then the rotating block 7-2 on the clamping device 7 is held and rotates, meanwhile, the lifting post 7-1 moves up and down, and finally, the pressing block 7-3 is contacted with the upper surface of the workpiece and is pressed tightly.
Of course, the above description is not intended to limit the present invention, and the present invention is not limited to the above examples, and the changes, modifications, additions or substitutions made by those skilled in the art within the scope of the present invention should also belong to the protection scope of the present invention.
Claims (5)
1. The utility model provides an aircraft special-shaped part centre gripping frock, includes PMKD (1), fixing hole (2), adjusting device (3), activity piece (4), elevating gear (5), fixed bolster (6), clamping device (7), its characterized in that: the utility model discloses a fixed baseplate (1) is characterized in that fixed through hole (2) respectively are equipped with in the middle of the edge about the top surface on PMKD (1), every the top surface middle department is connected with adjusting device (3) before fixed through hole (2) is inside, adjusting device (3) side top surface cartridge has a movable piece (4), the middle cartridge of locating of movable piece (4) left side top surface has elevating gear (5), top surface right side fixedly connected with fixed bolster (6) on elevating gear (5), top surface left edge middle cartridge has clamping device (7) on fixed bolster (6).
2. The special-shaped part clamping tool for the airplane as claimed in claim 1, wherein the special-shaped part clamping tool comprises: the adjusting device (3) comprises a lead screw (3-1), bearings (3-2) and a rotary table (3-3), the bearings (3-2) are symmetrically inserted into the front edge and the rear part of the side top end surface of the lead screw (3-1), the rotary table (3-3) is fixedly connected to the circle center of the rear top end surface of the lead screw (3-1), and the lead screw (3-1) penetrates through the rear top end surface of the fixing bottom plate (1) to be inserted into the fixing through hole (2) and is inserted into the middle of the front top end surface inside the fixing through hole (2).
3. The special-shaped part clamping tool for the airplane as claimed in claim 2, wherein the special-shaped part clamping tool comprises: the movable supporting block (4) comprises an upright post (4-1), a threaded hole (4-2), a sliding hole (4-3), a threaded post (4-4) and an adjusting disc (4-5), the middle of the lower edge of the top surface of the left side of the upright post (4-1) is provided with a threaded hole (4-2), a sliding hole (4-3) is arranged in the middle of the upper part of the front top end surface of the upright post (4-1), a threaded post (4-4) is inserted in the middle of the upper top end surface of the upright post (4-1), the circle center of the surface of the upper top end of the threaded column (4-4) is fixedly connected with an adjusting disc (4-5), the threaded hole (4-2) is inserted into the side surface of the screw rod (3-1), and the threaded column (4-4) penetrates through the upper surface of the upright column (4-1) and is inserted into the lower top end surface inside the sliding hole (4-3).
4. The special-shaped part clamping tool for the airplane as claimed in claim 3, wherein the special-shaped part clamping tool comprises: the lifting device (5) comprises a support block (5-1), a sliding block (5-2) and an insertion hole (5-3), the sliding block (5-2) is fixedly connected to the middle of the top end surface of the rear side of the support block (5-1), the insertion hole (5-3) is formed in the middle of the right edge of the top end surface of the sliding block (5-2), the insertion hole (5-3) is inserted into the side surface of the threaded column (4-4), internal threads are formed in the inner side surface of the insertion hole (5-3), and the upper surface of the support block (5-1) is in an arc shape.
5. The special-shaped part clamping tool for the airplane as claimed in claim 1, wherein the special-shaped part clamping tool comprises: the clamping device (7) comprises a lifting column (7-1), a rotating block (7-2) and a pressing block (7-3), the circle center of the upper top end surface of the lifting column (7-1) is fixedly connected with the rotating block (7-2), the circle center of the lower top end surface of the lifting column (7-1) is fixedly connected with the pressing block (7-3), and the lifting column (7-1) is inserted in the middle of the left edge of the upper top end surface of the fixed support (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922489501.1U CN211681977U (en) | 2019-12-30 | 2019-12-30 | Aircraft special-shaped part centre gripping frock |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922489501.1U CN211681977U (en) | 2019-12-30 | 2019-12-30 | Aircraft special-shaped part centre gripping frock |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211681977U true CN211681977U (en) | 2020-10-16 |
Family
ID=72798167
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922489501.1U Active CN211681977U (en) | 2019-12-30 | 2019-12-30 | Aircraft special-shaped part centre gripping frock |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211681977U (en) |
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2019
- 2019-12-30 CN CN201922489501.1U patent/CN211681977U/en active Active
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