CN204235174U - A kind of for multiple aviation part quick-replaceable and the frock clamp of Set and Positioning - Google Patents
A kind of for multiple aviation part quick-replaceable and the frock clamp of Set and Positioning Download PDFInfo
- Publication number
- CN204235174U CN204235174U CN201420685177.5U CN201420685177U CN204235174U CN 204235174 U CN204235174 U CN 204235174U CN 201420685177 U CN201420685177 U CN 201420685177U CN 204235174 U CN204235174 U CN 204235174U
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- CN
- China
- Prior art keywords
- positioning
- plate
- replaceable
- part template
- frock clamp
- 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 - Lifetime
Links
- 238000003825 pressing Methods 0.000 claims abstract description 7
- 230000006835 compression Effects 0.000 claims description 6
- 238000007906 compression Methods 0.000 claims description 6
- 230000035807 sensation Effects 0.000 claims description 3
- 125000003003 spiro group Chemical group 0.000 claims description 3
- 238000004519 manufacturing process Methods 0.000 abstract description 8
- 238000000034 method Methods 0.000 abstract description 5
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 238000005516 engineering process Methods 0.000 description 3
- 238000007689 inspection Methods 0.000 description 3
- 238000011112 process operation Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
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- Jigs For Machine Tools (AREA)
Abstract
本实用新型公开了一种用于多个航空零件快速更换并装夹定位的工装夹具，包括底板、前板、零件模板和后板，所述零件模板上部从左到右等间距设置若干V型槽，V型槽槽向为前后方向，零件模板底部设置两个定位孔，所述底板顶部设置两根定位柱与定位孔匹配，所述前板和后板通过固定螺栓分别固定在零件模板的前部和后部，所述前板上还螺纹连接若干前后向的压紧棒并对应每个V型槽。本实用新型的有益效果：可一次装夹多个航空零件且装夹过程在机床外进行，提高了生产效率和数控机床利用率；装夹简单，大幅度降低了频繁装夹工件的劳动强度，节约了生产成本。
The utility model discloses a tooling fixture for fast replacement and clamping and positioning of multiple aviation parts, which comprises a bottom plate, a front plate, a part template and a rear plate, and several V-shaped parts are arranged at equal intervals from left to right on the upper part of the part template. The V-shaped groove is in the front and rear directions. Two positioning holes are set at the bottom of the part template, and two positioning columns are set on the top of the bottom plate to match the positioning holes. The front plate and the rear plate are respectively fixed on the part template by fixing bolts. At the front and the rear, several forward and backward pressing rods are screwed on the front plate and correspond to each V-shaped groove. The beneficial effects of the utility model: multiple aviation parts can be clamped at one time, and the clamping process is carried out outside the machine tool, which improves the production efficiency and the utilization rate of the CNC machine tool; the clamping is simple, and the labor intensity of frequent clamping workpieces is greatly reduced. Production cost is saved.
Description
Technical field
The utility model relates to a kind of frock clamp, particularly a kind of for multiple aviation part quick-replaceable and the frock clamp of Set and Positioning, belongs to Computerized Numerical Control processing technology field.
Background technology
Our unit is at present at a certain aviation part of processing, and its structure as shown in Figure 1, 2.The production lot of this aviation part is large, and quality requirement is high, and each part must by process operation person self-inspection after production completes, and the qualified rear dish of self-inspection can be delivered to special inspection place and recheck, thus strict guarantee product quality.
In process, because part is little, process time is short, need on digital controlled processing central machine tool frequent renewal part Set and Positioning.Continuous replacing like this, constantly Set and Positioning mode also exist following weak point:
One, the machining accuracy of part not easily ensures;
The effective rate of utilization of two, actual production efficiency and numerical control machine tool is very low;
Three, the labour intensity of process operation person is also large.
Because this part needs production fast in enormous quantities, therefore, how to enhance productivity, ensure that product quality is a very important problem simultaneously.
Utility model content
Goal of the invention of the present utility model is: for the demand proposed in background technology, provides a kind of for multiple aviation part quick-replaceable and the frock clamp of Set and Positioning, can meet the demands.
The technical solution adopted in the utility model is such:
A kind of for multiple aviation part quick-replaceable and the frock clamp of Set and Positioning, comprise base plate, header board, part template and rear plate, described part template top is the some V-type grooves of spaced set from left to right, V-type groove groove is to being fore-and-aft direction, two locating holes are set bottom part template, described base plate top arranges two locating dowels and mates with locating hole, described front and rear panels are separately fixed at the front and rear of part template by set bolt, some sagittal compressions that described header board is also threaded rod corresponding each V-type groove.
As preferably, described V-type groove has six.
As preferably, described set bolt has the six roots of sensation, arranges two respectively in left, center, right portion.
As preferably, described compression rod is divided into screw rod and pressing plate two parts, and to being threaded on header board before and after screw rod, pressing plate is fixedly connected on spiro rod rear end.
In sum, owing to have employed technique scheme, the beneficial effects of the utility model are:
1, can the multiple aviation part of clamped one time, and clamping process is carried out outside lathe, improves actual production efficiency and Digit Control Machine Tool utilization rate;
2, clamping is simple, considerably reduces the labour intensity of frequent clamping workpiece, has saved the production cost of my unit;
3, product quality can obtain good guarantee.
Accompanying drawing explanation
Fig. 1 is the front view of aviation part to be detected.
Fig. 2 is the right view of aviation part to be detected.
Fig. 3 is three-dimensional structure diagram of the present utility model.
Mark in figure: 1 is base plate, and 2 is locating dowel, and 3 is set bolt, and 4 is header board, and 5 is part template, and 6 is rear plate, and 7 is V-type groove, 8 for compressing rod.
Detailed description of the invention
Below in conjunction with accompanying drawing, the utility model is described in detail.
Embodiment:
As shown in Figure 3, a kind of for multiple aviation part quick-replaceable and the frock clamp of Set and Positioning, comprise base plate 1, header board 4, part template 5 and rear plate 6, described part template 5 top is the some V-type grooves 7 of spaced set from left to right, V-type groove 7 groove is to being fore-and-aft direction, two locating holes are set bottom part template 5, described base plate 1 top arranges two locating dowels 2 and mates with locating hole, described header board 4 and rear plate 6 are separately fixed at the front and rear of part template 5 by set bolt 3, some sagittal compressions that described header board 4 is also threaded rod 8 corresponding each V-type groove 7.
Described V-type groove 6 has six.
Described set bolt 3 has the six roots of sensation, arranges two respectively in left, center, right portion.
Described compression rod 8 is divided into screw rod and pressing plate two parts, and to being threaded on header board 4 before and after screw rod, pressing plate is fixedly connected on spiro rod rear end.
Part shown in Fig. 1, Fig. 2 is positioned over part template 5 each V-type groove 7 in, then rotate compress rod 8, part is pushed against on rear plate 6.After part installs, header board 4, part template 5, rear plate 6 and each part entirety are put on base plate 1, the locating hole allowing locating dowel 2 insert bottom part template 5 positions.
The foregoing is only preferred embodiment of the present utility model; not in order to limit the utility model; all do within spirit of the present utility model and principle any amendment, equivalent to replace and improvement etc., all should be included within protection domain of the present utility model.
Claims (4)
1. one kind for multiple aviation part quick-replaceable and the frock clamp of Set and Positioning, it is characterized in that: comprise base plate (1), header board (4), part template (5) and rear plate (6), described part template (5) top is the some V-type grooves (7) of spaced set from left to right, V-type groove (7) groove is to being fore-and-aft direction, part template (5) bottom arranges two locating holes, described base plate (1) top arranges two locating dowels (2) and mates with locating hole, described header board (4) and rear plate (6) are separately fixed at the front and rear of part template (5) by set bolt (3), some sagittal compressions rod (8) that described header board (4) is also threaded corresponding each V-type groove (7).
2. according to claim 1 a kind of for multiple aviation part quick-replaceable and the frock clamp of Set and Positioning, it is characterized in that: described V-type groove (6) has six.
3. according to claim 1 a kind of for multiple aviation part quick-replaceable and the frock clamp of Set and Positioning, it is characterized in that: described set bolt (3) has the six roots of sensation, arranges two respectively in left, center, right portion.
4. according to claim 1 a kind of for multiple aviation part quick-replaceable and the frock clamp of Set and Positioning, it is characterized in that; Described compression rod (8) is divided into screw rod and pressing plate two parts, and to being threaded on header board (4) before and after screw rod, pressing plate is fixedly connected on spiro rod rear end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420685177.5U CN204235174U (en) | 2014-11-17 | 2014-11-17 | A kind of for multiple aviation part quick-replaceable and the frock clamp of Set and Positioning |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420685177.5U CN204235174U (en) | 2014-11-17 | 2014-11-17 | A kind of for multiple aviation part quick-replaceable and the frock clamp of Set and Positioning |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204235174U true CN204235174U (en) | 2015-04-01 |
Family
ID=52764726
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420685177.5U Expired - Lifetime CN204235174U (en) | 2014-11-17 | 2014-11-17 | A kind of for multiple aviation part quick-replaceable and the frock clamp of Set and Positioning |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204235174U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104476227A (en) * | 2014-11-17 | 2015-04-01 | 成都四威高科技产业园有限公司 | Tool clamp for fast replacing and clamping and locating plurality of aeronautical parts |
-
2014
- 2014-11-17 CN CN201420685177.5U patent/CN204235174U/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104476227A (en) * | 2014-11-17 | 2015-04-01 | 成都四威高科技产业园有限公司 | Tool clamp for fast replacing and clamping and locating plurality of aeronautical parts |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term |
Granted publication date: 20150401 |
|
| CX01 | Expiry of patent term |