CN204918826U - Anodization anchor clamps chuck - Google Patents
Anodization anchor clamps chuck Download PDFInfo
- Publication number
- CN204918826U CN204918826U CN201520558900.8U CN201520558900U CN204918826U CN 204918826 U CN204918826 U CN 204918826U CN 201520558900 U CN201520558900 U CN 201520558900U CN 204918826 U CN204918826 U CN 204918826U
- Authority
- CN
- China
- Prior art keywords
- terminal end
- bare terminal
- studs
- exposed core
- nut
- Prior art date
- 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.)
- Expired - Fee Related
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- Clamps And Clips (AREA)
Abstract
The utility model relates to an anodization anchor clamps chuck, including collet bodies (2) and fixed frame spare (3), the link of collet bodies (2) is fixed through two sets of bolt and nut on fixed frame spare (3), the exposed core of collet bodies (2) is opened and shut by a set of stud component control, the stud subassembly includes that one stud (6) of passing the exposed core, butterfly nut (7) install the one end in stud (6) from exposed core one side is outer, in the inboard and the outside of exposed core opposite side, one nut (5) respectively are equipped with on stud (6) two nuts (5) closely cooperate with the exposed core, the exposed core adopts the chamfer design.
Description
Technical field
The utility model belongs to mechanical engineering technical field, relates to a kind of anodizing clamping fixture head.
Background technology
Aircraft product is when surface treatment, and often need product to fix, product fixed form difference will bring different-effect to product surface process, and can not there be scuffing on the surface of aircraft product, goes out the defect such as pleat, watermark.The chuck that existing anodizing fixture uses, milling liquid cannot flow down smoothly from jaw face, and impact is normally produced, and cannot ensure product surface quality.Prior art is because contact area is large, and spring clamp causes product surface to produce defect, can realize product surface quality requirement by design chuck, guarantee to produce qualified product, chuck method for dismounting is simple, is convenient to assembling, there is enough clamping forces, meet product surface quality requirement.
Utility model content
The technical problems to be solved in the utility model:
Avoid milling liquid in milling process cannot flow down phenomenon smoothly from jaw face, occur scratching, going out the defect such as pleat, watermark, to process qualified product and to be convenient to product handling, meet how each product packing problem simultaneously.
The technical solution of the utility model:
The utility model is supplied to a kind of anodizing clamping fixture head, comprise collet body (2) and fixed frame frame member (3), the coupling end of described collet body 2 is fixed on described fixed frame frame member (3) by two groups of bolt and nuts, the bare terminal end of described collet body 2 controls folding by one group of studs assembly, described studs assembly comprises a studs 6 through bare terminal end, wing nut 7 is arranged on one end of studs 6 from bare terminal end side, in the inner side and outer side of bare terminal end opposite side, described studs 6 is respectively equipped with two nuts 5 described in a nut 5 to closely cooperate with bare terminal end, described bare terminal end adopts chamfer design.
Between described two nuts 5 and bare terminal end, packing ring 4 is housed, packing ring 4 is housed between wing nut 7 and bare terminal end.
The beneficial effects of the utility model:
The utility model adopts Split Positioning structure, can effectively contact with product, aircraft product can be made in anodizing process not occur watermark phenomenon by designing a kind of special carrier, guarantee that product surface quality is qualified, chuck is installed safe and reliable, and method for dismounting is simple, is convenient to assembling, there is the function that is rigidly connected, meet the requirement of aircraft product surface quality.Solve the problem that multiple product produces qualified product in normal anodizing situation, this structural orientation is reliable, and it is firm to clamp, simple to operation.
Accompanying drawing explanation
Fig. 1 is the utility model structural representation;
Wherein 1-bolt 2-collet body 3-fixed frame frame member 4-packing ring 5-nut 6-studs 7-wing nut embodiment.
Embodiment
Below the utility model is described in further details.
Carry out with product orientation before, first by studs 6, packing ring 4, nut 5, wing nut 7 is assembled on collet body 2, then by the chuck component that assembles by bolt 1, packing ring 4, nut 5, is connected to chuck component in fixed frame frame member 3 and realizes linkage function, realizes the effect of clamping product by adjustment wing nut 7.
Claims (2)
1. an anodizing clamping fixture head, it is characterized in that, comprise collet body (2) and fixed frame frame member (3), the coupling end of described collet body (2) is fixed on described fixed frame frame member (3) by two groups of bolt and nuts, the bare terminal end of described collet body (2) controls folding by one group of studs assembly, described studs assembly comprises a studs (6) through bare terminal end, wing nut (7) is arranged on one end of studs (6) from bare terminal end side, in the inner side and outer side of bare terminal end opposite side, described studs (6) is respectively equipped with described two nuts (5) of nut (5) to closely cooperate with bare terminal end, described bare terminal end adopts chamfer design.
2. a kind of anodizing clamping fixture head according to claim 1, it is characterized in that, between described two nuts (5) and bare terminal end, packing ring (4) is housed, packing ring (4) is housed between wing nut (7) and bare terminal end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520558900.8U CN204918826U (en) | 2015-07-29 | 2015-07-29 | Anodization anchor clamps chuck |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520558900.8U CN204918826U (en) | 2015-07-29 | 2015-07-29 | Anodization anchor clamps chuck |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204918826U true CN204918826U (en) | 2015-12-30 |
Family
ID=54967972
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520558900.8U Expired - Fee Related CN204918826U (en) | 2015-07-29 | 2015-07-29 | Anodization anchor clamps chuck |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204918826U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105671613A (en) * | 2016-03-21 | 2016-06-15 | 哈尔滨飞机工业集团有限责任公司 | Anodizing clamp collet chuck |
-
2015
- 2015-07-29 CN CN201520558900.8U patent/CN204918826U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105671613A (en) * | 2016-03-21 | 2016-06-15 | 哈尔滨飞机工业集团有限责任公司 | Anodizing clamp collet chuck |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20151230 Termination date: 20170729 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |