CN102689145B - Method for controlling numeric control machining deformation of slender and complicated T-shaped component - Google Patents
Method for controlling numeric control machining deformation of slender and complicated T-shaped component Download PDFInfo
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- CN102689145B CN102689145B CN201210182848.1A CN201210182848A CN102689145B CN 102689145 B CN102689145 B CN 102689145B CN 201210182848 A CN201210182848 A CN 201210182848A CN 102689145 B CN102689145 B CN 102689145B
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- 238000003754 machining Methods 0.000 title claims abstract description 19
- 238000000034 method Methods 0.000 title claims abstract description 16
- 238000005520 cutting process Methods 0.000 claims abstract description 29
- 238000003466 welding Methods 0.000 claims abstract description 7
- 238000003801 milling Methods 0.000 claims abstract description 4
- 238000004519 manufacturing process Methods 0.000 abstract description 2
- 238000007669 thermal treatment Methods 0.000 abstract 1
- 238000010586 diagram Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000004458 analytical method Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
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Abstract
The invention provides a method for controlling numeric control machining deformation of a slender and complicated T-shaped component, which comprises the following steps of: 1), dividing the machined slender and complicated T-shaped component into a left subpackage member and a right subpackage member, i.e. a subpackage member I and a subpackage member II; 2) performing coarse machining on the subpackage member I and the subpackage member II and manufacturing a positioning reference plane and a positioning hole; 3) fixing the subpackage member I and the subpackage member II on a numerically-controlled milling machine machining table board through a fixed tool; 4) performing equal-height drop layer ring cutting on components in a shallow-cutting machining way; 5) reserving machining allowance to an assembling part; 6) welding the subpackage member I and the subpackage member II into a whole and carrying out thermal treatment; and 7) completing the machining process of the slender and complicated T-shaped component. By adopting the method, the deformation of the tail part of the assembly before the welding of the component can be eliminated in the numeric control machining process, and the deformation amount is removed.
Description
Technical field
The invention relates to a kind of part by numerical control machining deformation control method, relates in particular to the T-shaped part by numerical control machining deformation of a kind of elongated complexity control method.
Background technology
Originally in digital control processing field, if run into elongated T-shaped part, can in every procedure of process, all produce part deformation, finally proofread and correct difficultly, probably have a strong impact on the final processing dimension of part and cause part to be scrapped.Therefore, the Deformation control in machining is very important for follow-up processing, and it directly affects the crudy of subsequent parts.
Summary of the invention
The object of the invention is to provide the T-shaped part by numerical control machining deformation of a kind of elongated complexity control method, can in NC Machining Process, eliminate the afterbody distortion of weld parts front assembly, and deflection is removed.
The technical scheme of the invention: the T-shaped part by numerical control machining deformation of elongated complexity control method, comprises the steps:
1) the processed T-shaped part of elongated complexity is divided into left and right two subassemblys, i.e. subassembly I and subassembly II;
2) subassembly I and subassembly II are carried out to roughing and made positioning datum plane and locating hole;
3) subassembly I and subassembly II are fixed on CNC milling machine processing table top by fixing tool;
4) adopt the shallow processing mode of cutting to carry out the contour layer ring cutting that fall to part;
5) to the reserved allowance in assembling position;
6) subassembly I and subassembly II are welded into as a whole and are heat-treated;
7) complete the T-shaped part machinery process of elongated complexity.
The concrete grammar of described step 4) is: adopt the contour cutting way that falls layer in both sides, machine spindle speed is 220～300RPM, and cutting depth is 0.5～2mm, and cutting width is 60～70mm, feed speed is 700～1000mm/min, and adopts the modular cutting tool assembly of end mill body and blade welding.
The beneficial effect of the invention: adopt the shallow processing mode of cutting to carry out the contour layer ring cutting that fall in both sides to part, by improving machine spindle speed, reduce cutting depth, increase cutting width, increase feed speed, and the modular cutting tool assembly that adopts end mill body and blade to weld, make material stress in working angles along with the discharge of cutting has obtained sufficient release, reduce stress and concentrated the part deformation causing, eliminate the afterbody distortion of weld parts front assembly, working (machining) efficiency also improves thereupon, can improve more than 30%, has greatly shortened the manufacturing cycle of part.
Accompanying drawing explanation
Fig. 1 is the deformation state schematic diagram of part to be processed before welding.
Fig. 2 is that the A of Fig. 1 is to view.
Fig. 3 is that the B of Fig. 1 is to view.
Fig. 4 is the rear part schematic diagram of welding.
The specific embodiment
The T-shaped part by numerical control machining deformation of elongated complexity control method, as shown in Figures 1 to 4, comprises the steps:
1) the processed T-shaped part of elongated complexity is divided into left and right two subassemblys, i.e. subassembly I and subassembly II;
2) subassembly I and subassembly II are carried out to roughing and made positioning datum plane and locating hole;
3) subassembly I and subassembly II are fixed on CNC milling machine processing table top by fixing tool;
4) adopt the shallow processing mode of cutting to carry out the contour layer ring cutting that fall to part;
5) to the reserved allowance in assembling position;
6) subassembly I and subassembly II are welded into as a whole and are heat-treated;
7) complete the T-shaped part machinery process of elongated complexity.
The concrete grammar of described step 4) is: adopt the contour cutting way that falls layer in both sides, machine spindle speed is 220～300RPM, and cutting depth is 0.5～2mm, and cutting width is 60～70mm, feed speed is 700～1000mm/min, and adopts the modular cutting tool assembly of end mill body and blade welding.
It is shallow that to cut processing be AF1410(16Co14Ni10Cr2Mo to this kind of material trademark) processing of unimach is a kind of new processing mode.
Now selecting a φ 63R4 cutter is example, and the shallow concrete cutting parameter of cutting processing and tradition processing contrasts as follows:
Can find out and adopt shallow superiority of cutting processing mode from upper table analysis.
Claims (2)
1. the T-shaped part by numerical control machining deformation of elongated complexity control method, is characterized in that, comprises the steps:
1) the processed T-shaped part of elongated complexity is divided into left and right two subassemblys, i.e. subassembly I and subassembly II;
2) subassembly I and subassembly II are carried out to roughing and made positioning datum plane and locating hole;
3) subassembly I and subassembly II are fixed on CNC milling machine processing table top by fixing tool;
4) adopt the shallow processing mode of cutting to carry out the contour layer ring cutting that fall to part;
5) to the reserved allowance in assembling position;
6) subassembly I and subassembly II are welded into as a whole and are heat-treated;
7) complete the T-shaped part machinery process of elongated complexity.
2. the T-shaped part by numerical control machining deformation of elongated complexity as claimed in claim 1 control method, it is characterized in that, the concrete grammar of described step 4) is: adopt contour ring cutting mode of falling layer, machine spindle speed is 220～300RPM, cutting depth is 0.5～2mm, cutting width is 60～70mm, and feed speed is 700～1000mm/min, and adopts the modular cutting tool assembly of end mill body and blade welding.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210182848.1A CN102689145B (en) | 2012-06-06 | 2012-06-06 | Method for controlling numeric control machining deformation of slender and complicated T-shaped component |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210182848.1A CN102689145B (en) | 2012-06-06 | 2012-06-06 | Method for controlling numeric control machining deformation of slender and complicated T-shaped component |
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| Publication Number | Publication Date |
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| CN102689145A CN102689145A (en) | 2012-09-26 |
| CN102689145B true CN102689145B (en) | 2014-06-04 |
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| CN201210182848.1A Expired - Fee Related CN102689145B (en) | 2012-06-06 | 2012-06-06 | Method for controlling numeric control machining deformation of slender and complicated T-shaped component |
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Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103273292B (en) * | 2013-06-14 | 2016-04-20 | 沈阳飞机工业（集团）有限公司 | The control of the T-shaped part deformation of a kind of elongated complexity and compensation method |
| CN103464815B (en) * | 2013-08-29 | 2015-10-28 | 宁波永博机械制造有限公司 | A kind of slender axles highly-efficient processing device |
| CN105945545B (en) * | 2016-06-15 | 2018-07-10 | 沈阳飞机工业（集团）有限公司 | A kind of processing method of ultrathin long rod reamer |
| CN107570966B (en) * | 2017-08-17 | 2019-05-10 | 西安电子工程研究所 | A kind of method of regulating arm processing in frequency multiplier |
| CN111203579B (en) * | 2020-03-16 | 2021-02-05 | 沈阳飞机工业（集团）有限公司 | Machining method before quenching of AF1410 steel part |
| CN113927256A (en) * | 2021-11-18 | 2022-01-14 | 航天科工哈尔滨风华有限公司 | Machining method for large titanium alloy thin-wall deep-cavity cabin formed through laser deposition |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH06339819A (en) * | 1992-10-17 | 1994-12-13 | Hoesch Platinen Gmbh | Method for manufacturing welded steel plate-made intermediate article |
| CN1406709A (en) * | 2001-09-04 | 2003-04-02 | 宫野利治 | System and method for processing long and thin component |
| CN1498714A (en) * | 2002-11-07 | 2004-05-26 | ˹�ڿ���Ī�ض�˹ | One-way scanning laser welding method for T-shape assembly of metalic parts |
| CN1974054A (en) * | 2006-12-08 | 2007-06-06 | 青特集团有限公司 | Slender stepped shaft machining process |
| CN101402166A (en) * | 2008-11-14 | 2009-04-08 | 扬州市天禾粉末冶金工业有限公司 | Process for manufacturing T type screwed cap |
-
2012
- 2012-06-06 CN CN201210182848.1A patent/CN102689145B/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH06339819A (en) * | 1992-10-17 | 1994-12-13 | Hoesch Platinen Gmbh | Method for manufacturing welded steel plate-made intermediate article |
| CN1406709A (en) * | 2001-09-04 | 2003-04-02 | 宫野利治 | System and method for processing long and thin component |
| CN1498714A (en) * | 2002-11-07 | 2004-05-26 | ˹�ڿ���Ī�ض�˹ | One-way scanning laser welding method for T-shape assembly of metalic parts |
| CN1974054A (en) * | 2006-12-08 | 2007-06-06 | 青特集团有限公司 | Slender stepped shaft machining process |
| CN101402166A (en) * | 2008-11-14 | 2009-04-08 | 扬州市天禾粉末冶金工业有限公司 | Process for manufacturing T type screwed cap |
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