CN215470735U - Clamping support for aviation lifting lug product - Google Patents
Clamping support for aviation lifting lug product Download PDFInfo
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- CN215470735U CN215470735U CN202122092578.2U CN202122092578U CN215470735U CN 215470735 U CN215470735 U CN 215470735U CN 202122092578 U CN202122092578 U CN 202122092578U CN 215470735 U CN215470735 U CN 215470735U
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Abstract
The utility model relates to a clamping support for an aviation lifting lug product, which comprises a base, a front side pressure plate seat side surface supporting head, a front side pressure plate top surface compression screw, a front side left side fixing supporting seat, a front side left side bottom surface supporting head, a front side right side fixing supporting seat, a front side right side bottom surface supporting head, a limiting seat, a limiting column, a jacking seat, a jacking screw, a middle compression seat side surface compression screw, a rear end middle fixing supporting seat, a rear end middle bottom surface supporting head, a rear side pressure plate seat, a rear side pressure plate top surface compression screw, a compression adjusting seat, a top surface compression adjusting screw, a rear end left side floating supporting seat, a rear end left side floating supporting head, a rear end right side floating supporting seat and a rear end right side floating supporting head. The utility model can automatically adapt to the height of a product and prevent irregular castings from vibrating and swinging left and right in the processing process, thereby improving the production efficiency and reducing the reject ratio of the product.
Description
Technical Field
The utility model relates to a fixing device for an aviation lifting lug product, in particular to a clamping support for the aviation lifting lug product.
Background
When the aviation lug product is processed, the product is fixed on the clamp. However, in the existing production process, the product clamping time is long, the processing efficiency is low, the working strength of operators is high, and time and labor are wasted. And the clamp for fixing the product is inconvenient to operate and inaccurate in positioning the product, so that the processing efficiency of the product is low.
Disclosure of Invention
The utility model aims to overcome the defects in the prior art and provide the clamping support for the aviation lifting lug product, which is convenient to operate, accurate in product positioning, capable of improving the production rate and reducing the reject ratio of the product.
According to the technical scheme provided by the utility model, the clamping support for the aviation lifting lug product comprises a base, a front side pressure plate seat, a side surface supporting head of the front side pressure plate seat, a front side pressure plate, a top surface compression screw of the front side pressure plate, a front side left fixing supporting seat, a front side left bottom surface supporting head, a front side right fixing supporting seat, a front side right bottom surface supporting head, a limiting seat, a limiting column, a top pressing seat, a top pressing screw, a middle pressing seat side compression screw, a rear end middle fixing supporting seat, a rear end middle bottom surface supporting head, a rear side pressure plate seat, a rear side pressure plate top surface compression screw, a compression adjusting seat, a top surface compression adjusting screw, a rear side floating supporting seat, a rear side supporting floating head, a rear side floating supporting seat and a rear side floating supporting head;
a front side platen seat is fixed on the upper surface of the base, front side platen seat side supporting heads are fixed on the left side and the right side of the front side platen seat, a front side platen is fixed on the upper end surface of the front side platen seat, the length of the front side platen in the left-right direction is larger than that of the front side platen seat in the left-right direction, front side platen top surface compression screws are fixed on the lower surface of the front side platen corresponding to the left end surface left side and the right end surface right side of the front side platen seat, a front side left side fixing supporting seat is fixed on the upper surface of the base corresponding to the left side of the front side platen seat, and a front side left side bottom surface supporting head is fixed on the upper end surface of the front side left side fixing supporting seat;
a front-end right-side fixed support seat is fixed on the upper surface of the base corresponding to the right side of the front-end pressure plate seat, a front-end right-side bottom support head is fixed on the upper end surface of the front-end right-side fixed support seat, a limit seat is fixed on the upper surface of the base corresponding to the rear side of the front-end left-side fixed support seat, a limit column is fixed on the upper end surface of the limit seat, a jacking seat is fixed on the upper surface of the base corresponding to the rear side of the front-end right-side fixed support seat, a jacking screw is installed on the right side of the jacking seat, a middle pressing seat is fixed on the upper surface of the base corresponding to the rear side between the limit seat and the jacking seat, a middle pressing seat side pressing screw is installed on the right side surface of the middle pressing seat, a rear-end middle fixed support seat is fixed on the upper surface of the base corresponding to the rear side of the middle pressing seat, a rear-end middle bottom support head is fixed on the upper surface of the rear-end middle fixed support seat, a rear-end pressure plate seat is fixed on the upper surface of the base corresponding to the rear side of the rear-end middle fixed support seat, a rear side pressure plate is fixed on the upper end surface of the rear side pressure plate seat, the length of the rear side pressure plate in the left-right direction is greater than that of the rear side pressure plate seat in the left-right direction, and rear side pressure plate top surface compression screws are arranged on the rear side pressure plate corresponding to the left side of the left side surface of the rear side pressure plate seat and the rear side pressure plate corresponding to the right side of the right side surface of the rear side pressure plate seat;
the front side of the rear pressure plate seat corresponding to the upper part of the rear middle fixed support seat is fixed with a compression adjusting seat, the compression adjusting seat is provided with a top surface compression adjusting screw, the upper surface of the base corresponding to the left side of the rear pressure plate seat is fixed with a rear left floating support seat, the upper end surface of the rear left floating support seat is provided with a rear left floating support head, the upper surface of the base corresponding to the right side of the rear pressure plate seat is fixed with a rear right floating support seat, and the upper end surface of the rear right floating support seat is provided with a rear right floating support head.
Preferably, a baffle is fixed to a front wall surface of the front platen base.
Preferably, a front platen positioning pin is fixed to an upper end surface of the front platen, a front platen positioning pin groove is formed in a lower end surface of the front platen, and the front platen positioning pin groove is engaged with the front platen positioning pin.
The utility model can automatically adapt to the height of a product and prevent irregular castings from vibrating and swinging left and right in the processing process, thereby improving the production efficiency and reducing the reject ratio of the product.
Drawings
Fig. 1 is a schematic view of the overall structure of the present invention.
Fig. 2 is an exploded view of the present invention.
Fig. 3 is a schematic structural diagram of an aviation lifting lug product.
Detailed Description
The present invention will be further described with reference to the following specific examples.
The clamping support for the aviation lifting lug product is shown in figures 1 and 2, the device comprises a base 1, a front side pressure plate seat 2, a front side pressure plate seat side surface supporting head 2.1, a front side pressure plate 3, a front side pressure plate top surface compression screw 3.1, a front side left side fixed supporting seat 4, a front side left side bottom surface supporting head 4.1, a front side right side fixed supporting seat, a front side right side bottom surface supporting head 5.1, a limiting seat 6, a limiting column 6.1, a jacking seat 7, a jacking screw 7.1, a middle jacking seat 8, a middle jacking seat side surface compression screw 8.1, a rear end middle fixed supporting seat 9, a rear end middle bottom surface supporting head 9.1, a rear side pressure plate seat 10, a rear side pressure plate 11, a rear side pressure plate top surface compression screw 11.1, a compression adjusting seat 12, a top surface compression adjusting screw 12.1, a rear end left side floating supporting seat 13, a rear end left side floating supporting head 13.1, a rear end right side floating supporting seat 14 and a rear end right side floating supporting head 14.1;
a front platen base 2 is fixed on the upper surface of the base 1, front platen base side supporting heads 2.1 are fixed on the left side and the right side of the front platen base 2, a front platen 3 is fixed on the upper end surface of the front platen base 2, the length of the front platen 3 in the left-right direction is larger than that of the front platen base 2 in the left-right direction, front platen top surface compression screws 3.1 are fixed on the lower surfaces of the front platens 3 corresponding to the left end surface left side and the right end surface right side of the front platen base 2, a front left side fixed supporting base 4 is fixed on the upper surface of the base 1 corresponding to the left side of the front platen base 2, and a front left side bottom surface supporting head 4.1 is fixed on the upper end surface of the front left side fixed supporting base 4;
a front-end right-side fixed supporting seat is fixed on the upper surface of the base 1 corresponding to the right side of the front-end pressure plate seat 2, a front-end right-side bottom supporting head 5.1 is fixed on the upper end surface of the front-end right-side fixed supporting seat, a limiting seat 6 is fixed on the upper surface of the base 1 corresponding to the back of the front-end left-side fixed supporting seat 4, a limiting column 6.1 is fixed on the upper end surface of the limiting seat 6, a jacking seat 7 is fixed on the upper surface of the base 1 corresponding to the back of the front-end right-side fixed supporting seat, a jacking screw 7.1 is installed on the right side of the jacking seat 7, a middle pressing seat 8 is fixed on the upper surface of the base 1 corresponding to the back between the limiting seat 6 and the jacking seat 7, a middle pressing seat 8 is installed on the right side surface of the middle pressing seat 8, a back-end middle fixed supporting seat 9 is fixed on the upper surface of the base 1 corresponding to the back of the middle pressing seat 8, a back-end middle supporting seat 9 is fixed on the upper end bottom surface of the back-end middle supporting seat 9, a rear platen seat 10 is fixed on the upper surface of the base 1 corresponding to the rear middle fixed support seat 9, a rear platen 11 is fixed on the upper end surface of the rear platen seat 10, the length of the rear platen 11 in the left-right direction is greater than that of the rear platen seat 10 in the left-right direction, and rear platen top surface compression screws 11.1 are installed on the rear platen 11 corresponding to the left side of the left side surface of the rear platen seat 10 and the rear platen 11 corresponding to the right side of the right side surface of the rear platen seat 10;
a pressing adjusting seat 12 is fixed on the front side of the rear platen seat 10 above the corresponding rear middle fixing support seat 9, a top surface pressing adjusting screw 12.1 is installed on the pressing adjusting seat, a rear left floating support seat 13 is fixed on the upper surface of the base 1 corresponding to the left side of the rear platen seat 10, a rear left floating support head 13.1 is installed on the upper end surface of the rear left floating support seat 13, a rear right floating support seat 14 is fixed on the upper surface of the base 1 corresponding to the right side of the rear platen seat 10, and a rear right floating support head 14.1 is installed on the upper end surface of the rear right floating support seat 14.
In the utility model, a self-adaptive sleeve, a spring and a transverse locking screw are arranged in a rear-end left floating support seat 13, a rear-end left floating support head 13.1 is arranged at the upper end part of the self-adaptive sleeve, and the spring is arranged between the self-adaptive sleeve and the transverse locking screw; a self-adaptive sleeve, a spring and a transverse locking screw are arranged in the rear-end right floating support seat 14, a rear-end right floating support head 14.1 is arranged at the upper end part of the self-adaptive sleeve, and the spring is arranged between the self-adaptive sleeve and the transverse locking screw.
The working principle of the utility model is as follows:
the utility model uses a front end left side bottom surface support head 4.1 and a front end right side bottom surface support head 5.1 to fix the front end of the lower beam surface of an aviation lug product 20, uses a rear end middle bottom surface support head 9.1 to fix the middle rear end of the lower beam surface of the aviation lug product 20, uses a jacking screw 7.1 and a middle pressing seat side pressing screw 8.1 to tightly lock the side surface of the aviation lug product 20, uses a spacing column 6.1 to jack the middle part of the lower beam surface of the aviation lug product 20 to prevent the aviation lug product from moving forwards and backwards, uses a front side pressure plate top surface pressing screw 3.1 to tightly press and fix the front end (namely a narrower end) of the upper beam surface of the aviation lug product 20, uses a rear side pressure plate top surface pressing screw 11.1 to tightly press and fix the rear end (namely a wider end) of the upper beam surface of the aviation lug product 20, uses a top surface pressing adjusting screw 12.1 to fix the rear end middle rear end of the upper beam surface of the aviation lug product 20, uses a rear end left side floating support head 13.1 and a rear end right side floating support head 14.1 to form a floating support system, the rear end (namely the wider end) of the lower beam surface of the aviation lifting lug product 20 is supported in a self-adaptive mode, so that the height of the aviation lifting lug product 20 is supported in a self-adaptive mode in the machining process, a vibration resisting effect is achieved, and the aviation lifting lug product 20 is prevented from swinging left and right in the production process.
The baffle plate 15 is fixed on the front wall surface of the front side pressure plate seat 2, and the front end surface of the front side pressure plate 3 is abutted against the rear end surface of the baffle plate 15 during installation, so that the front side pressure plate 3 can be conveniently installed on the pressure plate seat 2.
The upper end surface of the front side press plate seat 2 is fixed with a front side press plate seat positioning pin 2.2, the lower end surface of the front side press plate 3 is provided with a front side press plate positioning pin groove 3.2, and the front side press plate positioning pin groove 3.2 is matched with the front side press plate seat positioning pin 2.2. When the front pressing plate 3 is installed, the front pressing plate 3 can be accurately installed at the corresponding position of the upper end surface of the front pressing plate seat 2 only by aligning the front pressing plate locating pin groove 3.2 with the front pressing plate seat locating pin 2.2 and pressing the front pressing plate 3 against the baffle plate 15, namely aligning and then screwing the screw for fixing the front pressing plate 3 with the screw hole arranged on the upper end surface of the front pressing plate seat 2.
Claims (3)
1. The utility model provides a clamping support of aviation lug product, characterized by: the device comprises a base (1), a front side pressure plate seat (2), a front side pressure plate seat side supporting head (2.1), a front side pressure plate (3), a front side pressure plate top surface compression screw (3.1), a front side left side fixed support seat (4), a front side left side bottom surface supporting head (4.1), a front side right side fixed support seat, a front side right side bottom surface supporting head (5.1), a limiting seat (6), a limiting column (6.1), a jacking seat (7), a jacking screw (7.1), a middle compression seat (8), a middle compression seat side compression screw (8.1), a rear end middle fixed support seat (9), a rear end middle bottom surface supporting head (9.1), a rear side pressure plate seat (10), a rear side pressure plate (11), a rear side pressure plate top surface compression screw (11.1), a compression adjusting seat (12), a top surface compression adjusting screw (12.1), a rear end left side floating support seat (13), a rear end left side floating support head (13.1), A rear right floating support seat (14) and a rear right floating support head (14.1);
a front side platen seat (2) is fixed on the upper surface of the base (1), front side platen seat side supporting heads (2.1) are fixed on the left side surface and the right side surface of the front side platen seat (2), a front side platen (3) is fixed on the upper end surface of the front side platen seat (2), the lengths of the front side platen (3) in the left direction and the right direction are greater than the lengths of the front side platen seat (2) in the left direction and the right direction, front side platen top surface compression screws (3.1) are fixed on the lower surfaces of the front side platens (3) corresponding to the left end surface left side and the right end surface right side of the front side platen seat (2), a front side left side fixing supporting seat (4) is fixed on the upper surface of the base (1) corresponding to the left side platen seat (2), and a front side left side bottom surface supporting head (4.1) is fixed on the upper end surface of the front side fixing supporting seat (4);
the upper surface of a base (1) corresponding to the right side of a front side pressure plate seat (2) is fixed with a front side right side fixed support seat, the upper end surface of the front side right side fixed support seat is fixed with a front side right side bottom surface support head (5.1), the upper surface of the base (1) corresponding to the rear side of a front side left side fixed support seat (4) is fixed with a limiting seat (6), the upper end surface of the limiting seat (6) is fixed with a limiting column (6.1), the upper surface of the base (1) corresponding to the rear side of the front side right side fixed support seat is fixed with a jacking seat (7), the right side of the jacking seat (7) is provided with a jacking screw (7.1), the upper surface of the base (1) corresponding to the rear side between the limiting seat (6) and the jacking seat (7) is fixed with a middle compression seat (8), the right side surface of the middle compression seat (8) is provided with a middle compression seat side compression screw (8.1), the middle part of the base (1) corresponding to the rear side of the middle compression seat (8) is fixed with a rear middle support seat (9) ) A rear end middle bottom surface supporting head (9.1) is fixed on the upper end surface of the rear end middle fixing supporting seat (9), a rear side pressure plate seat (10) is fixed on the upper surface of the base (1) corresponding to the rear of the rear end middle fixing supporting seat (9), a rear side pressure plate (11) is fixed on the upper end surface of the rear side pressure plate seat (10), the length of the rear side pressure plate (11) in the left-right direction is greater than that of the rear side pressure plate seat (10) in the left-right direction, and rear side pressure plate top surface compression screws (11.1) are installed on the rear side pressure plate (11) corresponding to the left side surface of the rear side pressure plate seat (10) and the rear side pressure plate (11) corresponding to the right side surface of the rear side pressure plate seat (10);
a pressing adjusting seat (12) is fixed on the front side face of a rear pressure plate seat (10) above a corresponding rear-end middle fixed supporting seat (9), a top-face pressing adjusting screw (12.1) is installed on the pressing adjusting seat, a rear-end left floating supporting seat (13) is fixed on the upper surface of a base (1) on the left side of the corresponding rear pressure plate seat (10), a rear-end left floating supporting head (13.1) is installed on the upper end face of the rear-end left floating supporting seat (13), a rear-end right floating supporting seat (14) is fixed on the upper surface of the base (1) on the right side of the corresponding rear pressure plate seat (10), and a rear-end right floating supporting head (14.1) is installed on the upper end face of the rear-end right floating supporting seat (14).
2. A clamping support for an aviation lifting lug product according to claim 1, wherein: a baffle (15) is fixed on the front wall surface of the front side pressure plate seat (2).
3. A clamping support for an aviation lifting lug product according to claim 1, wherein: the upper end surface of the front side pressure plate seat (2) is fixed with a front side pressure plate seat positioning pin (2.2), the lower end surface of the front side pressure plate (3) is provided with a front side pressure plate positioning pin groove (3.2), and the front side pressure plate positioning pin groove (3.2) is matched with the front side pressure plate seat positioning pin (2.2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122092578.2U CN215470735U (en) | 2021-08-31 | 2021-08-31 | Clamping support for aviation lifting lug product |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122092578.2U CN215470735U (en) | 2021-08-31 | 2021-08-31 | Clamping support for aviation lifting lug product |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215470735U true CN215470735U (en) | 2022-01-11 |
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ID=79766850
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122092578.2U Active CN215470735U (en) | 2021-08-31 | 2021-08-31 | Clamping support for aviation lifting lug product |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215470735U (en) |
-
2021
- 2021-08-31 CN CN202122092578.2U patent/CN215470735U/en active Active
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