CN104028950A - Method for machining dihedral-angle plane with position requirements - Google Patents
Method for machining dihedral-angle plane with position requirements Download PDFInfo
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- CN104028950A CN104028950A CN201410256958.7A CN201410256958A CN104028950A CN 104028950 A CN104028950 A CN 104028950A CN 201410256958 A CN201410256958 A CN 201410256958A CN 104028950 A CN104028950 A CN 104028950A
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- China
- Prior art keywords
- plane
- datum level
- dihedral
- fabrication hole
- machining
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P13/00—Making metal objects by operations essentially involving machining but not covered by a single other subclass
- B23P13/02—Making metal objects by operations essentially involving machining but not covered by a single other subclass in which only the machining operations are important
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Drilling And Boring (AREA)
Abstract
The invention relates to a method for machining a dihedral-angle plane with position requirements. The plane forms an included angle theta 1 with the bottom surface in a front view and forms another included angle theta 2 with the bottom surface in a side view. The method includes the machining steps of 1), firstly, machining three surfaces vertical in pairwise on a machining piece; 2), setting one point on a third reference plane and drilling a first technology hole via the point and vertical to the third reference plane; 3), setting one point on the axis of the first technology hole and drilling a second technology hole in a plane opposite to the second reference plate, wherein the second reference plane forms an included angle theta 1 with the first reference plane; 4), rotating by the angle theta 2 along the axis of the second technology hole; 5), acquiring distance E between the center in the end face of the second technical hole and the side A of the dihedral-angle plane through digital-to-analogue conversion according to the set value and horizontally machining the side A to obtain the dihedral-angle plate with the position requirements. The two holes vertical to each other and located on the same plane are taken as the technical holes, so that machining precision can be guaranteed.
Description
Technical field
The present invention relates to a kind of dihedral plane surface processing method that has status requirement, belong to process.
Background technology
In machining; tool locating part usually can run into processing or the check of the dihedral that has status requirement, has the dihedral angle plane of status requirement, at present a lot of for processing the method for dihedral class plane; but all having complex process, there is the problems such as error is large in processing.
Summary of the invention
The technical problem to be solved in the present invention is to provide a kind of dihedral plane surface processing method that has status requirement, the method adopt two mutually vertical and two holes in same plane as fabrication hole, thereby guarantee machining accuracy.
For overcoming the above problems, concrete technical scheme of the present invention is as follows: a kind of dihedral plane surface processing method that has status requirement, wherein this plane is θ with bottom surface angle in front view
1, in side view, be θ with the angle of bottom surface
2, comprise the following steps and process:
1) on workpiece, first process three faces perpendicular to each other: the first datum level, the second datum level and the 3rd datum level, set up in theory geometric coordinate system;
2) on the 3rd datum level, set a bit, and perpendicular to the 3rd datum level, drill the first fabrication hole through this o'clock, its axis is distinguished parallel with the first datum level with the second datum level simultaneously;
3) on the axis of the first fabrication hole, set a bit, in the relative plane of the second datum level, drill through this point and perpendicular to the second fabrication hole of the first fabrication hole axis, the axis of the second fabrication hole is parallel with the 3rd datum level, and with the angle of the first datum level be θ
1;
4) insertion process pin in the second fabrication hole, utilize technique pin by the integral body of workpiece the axis rotation θ along the second fabrication hole
2angle;
5) according to setting value, can obtain the second fabrication hole at the distance E of the distance of center circle dihedral of end face plane A face by digital-to-analogue conversion, level is processed A face, obtains the dihedral plane of status requirement.
This has the dihedral plane surface processing method of status requirement to adopt on feature position to make axis at the orthogonal fabrication hole of same plane two, wherein the first fabrication hole for control hole axis its to the distance between datum plane, the dihedral angle plane parallel of auxiliary process axially bored line and part, for controlling the position of dihedral angle plane.The method is not only easy, and simple to operate, and precision is high.
Accompanying drawing explanation
Fig. 1 is the structural representation of workpiece.
Fig. 2 is the front view of workpiece.
Fig. 3 is workpiece rotation θ
2a after angle is to figure.
Fig. 4 is the projection view perpendicular to the first datum level.
The specific embodiment
As shown in Figures 1 to 4, a kind of dihedral plane surface processing method that has status requirement, wherein this plane is θ with bottom surface angle in front view
1, in side view, be θ with the angle of bottom surface
2, comprise the following steps and process:
1) on workpiece, first process three faces perpendicular to each other: the first datum level 1, the second datum level 2 and the 3rd datum level 3, set up in theory geometric coordinate system, as shown in Figure 2, the first datum level 1 is positioned in XY plane, the second datum level 2 is positioned in YZ plane, and the 3rd datum level 3 is positioned in XZ plane;
2) on the 3rd datum level 3, set a bit, its coordinate figure determines, and perpendicular to the 3rd datum level 3, drills the first fabrication hole 4 through this o'clock, and the axis 41 of the first fabrication hole 4 is parallel with the second datum level 2 difference with the first datum level 1 simultaneously;
3) on the axis 41 of the first fabrication hole 4, setting a bit this coordinate figure also should be through determining, in the relative plane of the second datum level 2, drill through this point and perpendicular to the second fabrication hole 5 of the first fabrication hole 4 axis, the axis 51 of the second fabrication hole 5 is parallel with the 3rd datum level 3, and with the angle of the first datum level 1 be θ
1;
4) at the interior insertion process pin of the second fabrication hole 5, utilize technique pin by the integral body of workpiece the axis 51 rotation θ along the second fabrication hole 5
2angle, as shown in Figure 3;
5) according to setting value, can obtain the second fabrication hole 5 at the distance E of the distance of center circle dihedral of end face plane A face by digital-to-analogue conversion, level is processed A face, obtains the dihedral plane of status requirement.
The method is not only applicable to the processing of dihedral, is applicable to the measurement of relation between dihedral and other geometric elements to be processed simultaneously.
Claims (1)
1. a dihedral plane surface processing method that has status requirement, wherein this plane is θ with bottom surface angle in front view
1, in side view, be θ with the angle of bottom surface
2, it is characterized in that comprising the following steps and process:
1) on workpiece, first process three faces perpendicular to each other: the first datum level (1), the second datum level (2) and the 3rd datum level (3), set up in theory geometric coordinate system;
2) set a bit the 3rd datum level (3) is upper, and perpendicular to the 3rd datum level (3), drill the first fabrication hole (4) through this o'clock, its axis is parallel with the second datum level (2) difference with the first datum level (1) simultaneously;
3) on the axis of the first fabrication hole (4), set a bit, in the relative plane of the second datum level (2), drill through this point and perpendicular to second fabrication hole (5) of the first fabrication hole (4) axis, the axis of the second fabrication hole (5) is parallel with the 3rd datum level (3), and with the angle of the first datum level (1) be θ
1;
4) insertion process pin in the second fabrication hole (5), utilize technique pin by the integral body of workpiece the axis rotation θ along the second fabrication hole (5)
2angle;
5) according to setting value, can obtain the second fabrication hole (5) at the distance E of the distance of center circle dihedral of end face plane A face by digital-to-analogue conversion, level is processed A face, obtains the dihedral plane of status requirement.
Priority Applications (1)
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CN201410256958.7A CN104028950B (en) | 2014-06-11 | 2014-06-11 | There is the dihedral plane surface processing method of status requirement |
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CN201410256958.7A CN104028950B (en) | 2014-06-11 | 2014-06-11 | There is the dihedral plane surface processing method of status requirement |
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CN104028950A true CN104028950A (en) | 2014-09-10 |
CN104028950B CN104028950B (en) | 2016-11-23 |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106180831A (en) * | 2016-07-13 | 2016-12-07 | 中铁宝桥集团有限公司 | A kind of solid manganese steel frog end fitting surface processing method |
CN117382730A (en) * | 2023-10-28 | 2024-01-12 | 马鞍山市一川金属科技有限公司 | Curved arm plate structure assembly |
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JP2003251532A (en) * | 2002-02-28 | 2003-09-09 | Akita Atsumi Kogyo Kk | Cutting and grinding complex and precision machining method for component member of variable valve device, etc. |
JP2004320968A (en) * | 2003-04-21 | 2004-11-11 | Tamagawa Seiki Co Ltd | Hollow shaft machining method for electric rotating machine having hollow shaft |
CN101412177A (en) * | 2008-12-11 | 2009-04-22 | 江西昌河航空工业有限公司 | Method for processing roulette and tooling fixture |
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CN103008977A (en) * | 2012-12-10 | 2013-04-03 | 大连瑞谷科技有限公司 | Special processing technology of angular contact precision bearing retainer |
CN103433689A (en) * | 2013-09-02 | 2013-12-11 | 遵义市节庆机电有限责任公司 | Machining process of rod-like iron core |
CN103506865A (en) * | 2012-06-29 | 2014-01-15 | 安徽华菱汽车有限公司 | Machining method of cylinder cover air intake slope and cylinder cover clamping device |
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2014
- 2014-06-11 CN CN201410256958.7A patent/CN104028950B/en active Active
Patent Citations (7)
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JP2003251532A (en) * | 2002-02-28 | 2003-09-09 | Akita Atsumi Kogyo Kk | Cutting and grinding complex and precision machining method for component member of variable valve device, etc. |
JP2004320968A (en) * | 2003-04-21 | 2004-11-11 | Tamagawa Seiki Co Ltd | Hollow shaft machining method for electric rotating machine having hollow shaft |
CN101412177A (en) * | 2008-12-11 | 2009-04-22 | 江西昌河航空工业有限公司 | Method for processing roulette and tooling fixture |
CN103506865A (en) * | 2012-06-29 | 2014-01-15 | 安徽华菱汽车有限公司 | Machining method of cylinder cover air intake slope and cylinder cover clamping device |
CN102806441A (en) * | 2012-07-31 | 2012-12-05 | 宁波韵升高科磁业有限公司 | Method for machining circular magnetic steel |
CN103008977A (en) * | 2012-12-10 | 2013-04-03 | 大连瑞谷科技有限公司 | Special processing technology of angular contact precision bearing retainer |
CN103433689A (en) * | 2013-09-02 | 2013-12-11 | 遵义市节庆机电有限责任公司 | Machining process of rod-like iron core |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
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CN106180831A (en) * | 2016-07-13 | 2016-12-07 | 中铁宝桥集团有限公司 | A kind of solid manganese steel frog end fitting surface processing method |
CN117382730A (en) * | 2023-10-28 | 2024-01-12 | 马鞍山市一川金属科技有限公司 | Curved arm plate structure assembly |
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CN104028950B (en) | 2016-11-23 |
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