CN213256560U - Spacer punching device for aerospace machinery - Google Patents
Spacer punching device for aerospace machinery Download PDFInfo
- Publication number
- CN213256560U CN213256560U CN202022179627.1U CN202022179627U CN213256560U CN 213256560 U CN213256560 U CN 213256560U CN 202022179627 U CN202022179627 U CN 202022179627U CN 213256560 U CN213256560 U CN 213256560U
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- CN
- China
- Prior art keywords
- fixedly connected
- rod
- hole
- cylinder
- connecting rod
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Links
- 238000004080 punching Methods 0.000 title claims abstract description 16
- 238000003825 pressing Methods 0.000 claims description 10
- 230000003014 reinforcing Effects 0.000 claims description 2
- 230000002146 bilateral Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006011 modification reaction Methods 0.000 description 1
- 239000003351 stiffener Substances 0.000 description 1
Abstract
The utility model discloses an adjusting shim punching device for aerospace machinery, the on-line screen storage device comprises a base, the one end fixedly connected with fixed column at base top, the top fixedly connected with diaphragm of fixed column, fixedly connected with cylinder on the bottom surface of diaphragm, the through-hole has been seted up to the bottom of cylinder, the inside of through-hole is provided with the connecting rod, the bottom fixedly connected with drift of connecting rod, the both sides of connecting rod and the outside symmetry fixedly connected with dead lever that is located the through-hole, fixedly connected with locating lever on the side of cylinder bottom, the bottom of locating lever is rotated and is connected with the horizontal pole, is provided with the gag lever post on the bottom. This spacer adjusting punching device for aerospace machinery, through setting up the linkage relation between dead lever, locating lever, horizontal pole, gag lever post and the spring, conveniently changes the drift, is convenient for adjust different drift sizes, fixes the gasket through setting up the hold-down mechanism convenience, and easy operation is convenient, convenient to use.
Description
Technical Field
The utility model belongs to the technical field of the adjusting shim punches a hole, concretely relates to adjusting shim punching device for aerospace machinery.
Background
In the punching process, due to the fact that the punching holes are different in size, the punching heads with different sizes need to be replaced, operation is troublesome, and fixing is inconvenient, so that the problem that the spacer adjusting punching device for the aerospace machinery needs to be designed is solved.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an adjusting shim punching device for aerospace machinery to solve the problem that proposes among the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: an adjusting gasket punching device for aerospace machinery comprises a base, wherein one end of the top of the base is fixedly connected with a fixing column, the top end of the fixed column is fixedly connected with a transverse plate, the bottom surface of the transverse plate is fixedly connected with a cylinder, the bottom end of the cylinder is provided with a through hole, a connecting rod is arranged in the through hole, the bottom end of the connecting rod is fixedly connected with a punch, the two sides of the connecting rod and the outer part of the through hole are symmetrically and fixedly connected with a fixed rod, the side surface of the bottom end of the cylinder is fixedly connected with a positioning rod, the bottom end of the positioning rod is rotatably connected with a cross rod, the bottom surface of the cross rod is provided with a limiting rod, springs are symmetrically and fixedly connected with both sides of the limiting rod, a supporting table is fixedly connected on the top surface of the base and below the cylinder, the top surface of the supporting table is provided with a punched hole, and the two sides of the punched hole on the top surface of the supporting table are symmetrically and fixedly connected with pressing mechanisms;
the pressing mechanism comprises a supporting rod, a positioning plate is fixedly connected to the top end of the supporting rod, a screw rod is arranged on the positioning plate through threads, and a pressing block is arranged at the bottom end of the screw rod.
Preferably, a collecting tank is arranged on the top surface of the base and below the supporting table.
Preferably, the bottom surface of the pressing block is fixedly connected with an anti-skid bulge.
Preferably, the side surface of the supporting rod is provided with a limiting sliding groove, and the limiting sliding groove is matched with a limiting sliding rod fixedly connected with the side surface of the pressing block for use.
Preferably, a reinforcing rod is fixedly connected between the positioning plate and the supporting rod.
The utility model discloses a technological effect and advantage: this spacer adjusting punching device for aerospace machinery, through setting up the linkage relation between dead lever, locating lever, horizontal pole, gag lever post and the spring, conveniently changes the drift, is convenient for adjust different drift sizes, fixes the gasket through setting up the hold-down mechanism convenience, and easy operation is convenient, convenient to use.
Drawings
Fig. 1 is a schematic structural view of the present invention;
fig. 2 is a schematic structural view of the pressing mechanism of the present invention;
fig. 3 is an enlarged schematic view of a structure shown in fig. 1 according to the present invention.
In the figure: 1. a base; 2. fixing a column; 3. a transverse plate; 4. a cylinder; 5. a through hole; 6. a connecting rod; 7. a punch; 8. collecting tank; 9. fixing the rod; 10. positioning a rod; 11. a cross bar; 12. a limiting rod; 13. a spring; 14. a support table; 15. punching; 16. a hold-down mechanism 1601, a support rod; 1602. positioning a plate; 1603. a screw; 1604. briquetting; 1605. and (4) anti-skid bulges.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
The utility model provides a space machinery is with adjustment gasket punching device as shown in fig. 1-3, the on-line screen storage device comprises a base 1, the one end fixedly connected with fixed column 2 at base 1 top, the top fixedly connected with diaphragm 3 of fixed column 2, fixedly connected with cylinder 4 on the bottom surface of diaphragm 3, through-hole 5 has been seted up to cylinder 4's bottom, the inside of through-hole 5 is provided with connecting rod 6, the bottom fixedly connected with drift 7 of connecting rod 6, the both sides of connecting rod 6 just are located the outside symmetry fixedly connected with dead lever 9 of through-hole 5, fixedly connected with locating lever 10 on the side of cylinder 4 bottom, the bottom of locating lever 10 is rotated and is connected with horizontal pole 11, be provided with gag lever post 12 on the bottom surface of horizontal pole 11, the bilateral symmetry fixedly connected with spring 13 of gag lever post 12 is through setting up dead, The linkage relation among the positioning rod, the cross rod, the limiting rod and the spring facilitates the replacement of the punch 7, and different sizes of the punch 7 are used;
a supporting table 14 is fixedly connected to the top surface of the base 1 and located below the air cylinder 4, a punched hole 15 is formed in the top surface of the supporting table 14, pressing mechanisms 16 are symmetrically and fixedly connected to the top surface of the supporting table 14 and located on two sides of the punched hole 15, and a collecting tank 8 is arranged on the top surface of the base 1 and located below the supporting table 14;
hold-down mechanism 16 includes bracing piece 1601, the top fixedly connected with locating plate 1602 of bracing piece 1601, be provided with screw rod 1603 through the screw thread on the locating plate 1602, the bottom of screw rod 1603 is provided with briquetting 1604, fixedly connected with anti-skidding arch 1605 on the bottom surface of briquetting 1604, spacing spout has been seted up on the side of bracing piece 1601, and spacing spout uses with briquetting 1604 side fixed connection's spacing slide bar cooperation, fixedly connected with stiffener between locating plate 1602 and the bracing piece 1601 fixes the gasket through hold-down mechanism 16, and easy operation is convenient.
This spacer adjustment punching device for aerospace machinery, when using, place the gasket on a supporting bench 14, rotate screw rod 1603 and compress tightly the gasket, start cylinder 4 and drive drift 7 and descend, punch a hole to the gasket, when other size drift 7 need be changed, pulling gag lever post 12 separates with dead lever 9, then rotatory horizontal pole 11 to take connecting rod 6 out through-hole 5, thereby separate it and cylinder 4, and easy operation is convenient, convenient to use.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications and variations can be made in the embodiments or in part of the technical features of the embodiments without departing from the spirit and the scope of the invention.
Claims (5)
1. The utility model provides an adjusting shim punching device for aerospace machinery, includes base (1), its characterized in that: one end of the top of the base (1) is fixedly connected with a fixed column (2), the top end of the fixed column (2) is fixedly connected with a transverse plate (3), the bottom surface of the transverse plate (3) is fixedly connected with a cylinder (4), the bottom end of the cylinder (4) is provided with a through hole (5), the inside of the through hole (5) is provided with a connecting rod (6), the bottom end of the connecting rod (6) is fixedly connected with a punch (7), fixing rods (9) are symmetrically and fixedly connected with the two sides of the connecting rod (6) and positioned outside the through hole (5), a positioning rod (10) is fixedly connected with the side surface of the bottom end of the cylinder (4), the bottom end of the positioning rod (10) is rotatably connected with a transverse rod (11), the bottom surface of the transverse rod (11) is provided with a limiting rod (12), and, a supporting table (14) is fixedly connected to the top surface of the base (1) and located below the air cylinder (4), a punched hole (15) is formed in the top surface of the supporting table (14), and pressing mechanisms (16) are symmetrically and fixedly connected to the top surface of the supporting table (14) and located on two sides of the punched hole (15);
hold-down mechanism (16) include bracing piece (1601), the top fixedly connected with locating plate (1602) of bracing piece (1601), be provided with screw rod (1603) through the screw thread on locating plate (1602), the bottom of screw rod (1603) is provided with briquetting (1604).
2. The spacer punch apparatus for aerospace machinery of claim 1, wherein: and a collecting tank (8) is arranged on the top surface of the base (1) and below the supporting table (14).
3. The spacer punch apparatus for aerospace machinery of claim 1, wherein: an anti-skid bulge (1605) is fixedly connected to the bottom surface of the pressing block (1604).
4. The spacer punch apparatus for aerospace machinery of claim 1, wherein: the side of the supporting rod (1601) is provided with a limiting sliding groove, and the limiting sliding groove is matched with a limiting sliding rod fixedly connected with the side of the pressing block (1604) for use.
5. The spacer punch apparatus for aerospace machinery of claim 1, wherein: a reinforcing rod is fixedly connected between the positioning plate (1602) and the supporting rod (1601).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022179627.1U CN213256560U (en) | 2020-09-29 | 2020-09-29 | Spacer punching device for aerospace machinery |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022179627.1U CN213256560U (en) | 2020-09-29 | 2020-09-29 | Spacer punching device for aerospace machinery |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213256560U true CN213256560U (en) | 2021-05-25 |
Family
ID=75947010
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022179627.1U Active CN213256560U (en) | 2020-09-29 | 2020-09-29 | Spacer punching device for aerospace machinery |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213256560U (en) |
-
2020
- 2020-09-29 CN CN202022179627.1U patent/CN213256560U/en active Active
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