CN112008102A - Boring method for elliptical hole of bushing - Google Patents
Boring method for elliptical hole of bushing Download PDFInfo
- Publication number
- CN112008102A CN112008102A CN202010687949.9A CN202010687949A CN112008102A CN 112008102 A CN112008102 A CN 112008102A CN 202010687949 A CN202010687949 A CN 202010687949A CN 112008102 A CN112008102 A CN 112008102A
- Authority
- CN
- China
- Prior art keywords
- boring
- elliptical hole
- bushing
- machining
- center
- 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.)
- Granted
Links
- 238000000034 method Methods 0.000 title claims abstract description 20
- 238000003754 machining Methods 0.000 claims abstract description 36
- 230000000694 effects Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000003672 processing method Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B35/00—Methods for boring or drilling, or for working essentially requiring the use of boring or drilling machines; Use of auxiliary equipment in connection with such methods
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B41/00—Boring or drilling machines or devices specially adapted for particular work; Accessories specially adapted therefor
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Drilling And Boring (AREA)
Abstract
The invention discloses a boring method of an elliptical hole of a bushing, which is characterized in that a machining coordinate system is established by taking the center of the elliptical hole of the bushing as an original point, and a boring cutter conducts multiple equidistant offset machining along the forward direction or the reverse direction of a machining direction from the original point. According to the invention, the tool-connecting steps on the inner wall of the elliptical hole can be effectively reduced through continuous equidistant offset boring, the processing quality is improved, and the tool-back risk of a long boring tool is avoided when a deep hole is processed. When the boring machine is used for boring the elliptical hole, the uniform deviation of each cutter is determined by a numerical control program, the boring machine is accurate and controllable, and the operation of workers and machining errors caused by the operation can be effectively reduced.
Description
Technical Field
The invention belongs to the technical field of machining, and particularly relates to a boring method of an elliptical hole of a bushing.
Background
In the machining process of parts, in order to meet the requirements of assembly and use, the bushing is generally required to prepare an elliptical hole with high precision. Boring when the two sides of the major axis of the elliptical hole are respectively offset to the maximum value by using a boring cutter, and leaving a larger cutter connecting step at the hole wall cutter connecting position to influence the surface quality of the part; because certain lining materials (such as 30 CrMnSiA) have higher special performance and rigidity and are not easy to cut, the traditional processing method is that a boring cutter is vertically deviated to directly bore an elliptical hole to the final size once, the cutting amount is large, the cutting force is large, the cutter is likely to cause tooth breakage, the surface of a part is scratched, and the stability and the safety of the processing process are reduced; when a deep hole is machined, the working length of a boring cutter is large, the rigidity is insufficient, cutter back-off can occur, and the final machining size precision of a part is influenced; based on this for improving bush machining precision and stability, provide the bore hole method of bush elliptical hole.
Disclosure of Invention
The invention discloses a boring method of an elliptical hole of a bushing, aiming at solving the problems, the boring method enables the machining process to be more stable, and can effectively avoid cutter tooth breakage caused by large cutting allowance and excessive cutting force. Aiming at deep hole machining, by adjusting the offset of each cutter, the cutter back-off condition caused by the fact that the working length of the boring cutter is large and the rigidity of the cutter is insufficient can be effectively avoided, and the machining precision of parts is guaranteed.
The invention is mainly realized by the following technical scheme: a boring method for an elliptical hole of a bushing is characterized in that a machining coordinate system is established by taking the center of the elliptical hole of the bushing as an original point, and a boring cutter conducts multiple equidistant offset machining in the forward direction or the reverse direction of a machining direction from the original point until a machining end point stops.
In order to better implement the invention, further, the boring cutter performs equidistant offset boring according to 0.2 mm.
In order to better realize the invention, a machining coordinate system is further established by taking the center of the elliptical hole of the short bushing as an origin, and the boring cutter respectively performs circle center upward equidistant shift for a plurality of times and circle center downward equidistant shift for a plurality of times along the Y direction of the machining coordinate system until end points at two ends of the major axis of the elliptical hole are machined.
In order to better implement the invention, further, the total offsets of the circle center which is equidistantly shifted upwards and the circle center which is equidistantly shifted downwards are respectively 1mm, and the circle center is equidistantly shifted upwards for 5 times and the circle center is equidistantly shifted downwards for 5 times.
In order to better implement the invention, further, when the long bushing is machined, the working length L of the boring cutter is greater than the length H of the bushing.
The invention has the beneficial effects that:
(1) according to the invention, the tool-connecting steps on the inner wall of the elliptical hole can be effectively reduced through continuous equidistant offset boring, the processing quality is improved, and the tool-back risk of a long boring tool is avoided when a deep hole is processed. When the boring machine is used for boring the elliptical hole, the uniform deviation of each cutter is determined by a numerical control program, the boring machine is accurate and controllable, and the operation of workers and machining errors caused by the operation can be effectively reduced.
(2) The offset of each cutter is controlled aiming at difficult-to-machine materials (such as 30 CrMnSiA), so that the machining process is more stable, and the cutter tooth breakage caused by large cutting allowance and overlarge cutting force can be effectively avoided; aiming at deep hole machining, the offset of each cutter is adjusted, the cutter back-off condition caused by the fact that the working length of the boring cutter is large and the rigidity of the cutter is insufficient can be effectively avoided, and the machining precision of parts is guaranteed.
Drawings
FIG. 1 is an assembly view of a short bushing for a part;
FIG. 2 is a cross-sectional view taken along line A-A of FIG. 1;
FIG. 3 is a schematic structural view of the upper half of the bored elliptical hole;
FIG. 4 is a schematic structural diagram of the lower half of the bored elliptical hole;
FIG. 5 is a residual comparison of a conventional bore and a bore of the present invention;
FIG. 6 is an assembled view of the elongated bushing of the part;
FIG. 7 is a cross-sectional view taken along line A-A of FIG. 6;
FIG. 8 is a schematic view of the construction of a long bushing;
fig. 9 is a schematic structural diagram of a boring cutter back-off tool.
Wherein: 1-part, 2-short bush, 3-processing coordinate system, 8-boring cutter and 9-long bush.
Detailed Description
Example 1:
a boring method of an elliptical hole of a bushing is used for boring the elliptical hole of a short bushing 2, as shown in figures 1-2: and establishing a machining coordinate system 3 by taking the center of the elliptical hole of the short bushing 2 as an origin, wherein the center of the elliptical hole of the bushing is equidistantly shifted upwards for 5 times (total offset is 1 mm) and is equidistantly shifted downwards for 5 times (total offset is 1 mm) in the Y + direction and the Y-direction of the machining coordinate system 3 respectively. The centre of a circle of the initial hole is equidistantly shifted upwards for 5 times (total offset is 1 mm), the centre of a circle is equidistantly shifted downwards for 5 times (total offset is 1 mm), the offset of each boring hole is only 0.2mm, and the cutting allowance can be effectively reduced to protect the cutter and improve the machining precision.
As shown in fig. 3, in the process of boring the bushing elliptical hole with the accuracy requirement 4, the total upward offset 5 of the circle center is divided into five equal parts, the boring cutter 8 starts from the original point of the machining coordinate system 3, and bores five times by sequentially offsetting 0.2mm in the Y + direction until the end point of the elliptical hole major axis is machined, so that the boring effect of the total upward offset of 1mm is achieved.
As shown in fig. 4, the total downward offset of 1mm from the center of the circle is divided into five equal parts, and the boring tool 8 performs five boring operations by sequentially shifting 0.2mm in the Y-direction from the origin of the machining coordinate system 3 through the control of the numerical control program until the other end point of the major axis of the elliptical hole is machined, thereby achieving the cutting effect of the total downward offset of 1 mm.
The track of the boring cutter 8 is started from the original point of the processing coordinate system 3, the boring is continuously and equivalently carried out for 5 times in the Y + direction to achieve the original cutting effect of offsetting the total offset for one time by 1mm, and then the boring is continuously and equivalently carried out for 5 times in the opposite direction (Y-direction) from the original point of the processing coordinate system 3 to achieve the original cutting effect of offsetting the total offset for one time by 1mm, so that the cutter connecting steps on the inner wall of the elliptical hole can be effectively reduced, the processing quality is improved, and the cutter back-off risk of the long boring cutter 8 is avoided when the deep hole is processed.
As shown in fig. 5, fig. 5 (a) is an elliptical hole obtained by a conventional boring method, and fig. 5 (b) is an elliptical hole obtained by boring according to the present invention. Compared with the traditional bushing elliptical hole boring method, the method has the advantages that the total upward deviation of the circle center is 1mm, the total downward deviation of the circle center is 1mm, the total upward deviation of the circle center is evenly divided, the tool receiving residue on the inner wall of the elliptical hole is effectively reduced, and meanwhile, the processing stability of the material difficult to process is improved. When the boring machine is used for boring the elliptical hole, the uniform deviation of each cutter is determined by a numerical control program, the boring machine is accurate and controllable, and the operation of workers and machining errors caused by the operation can be effectively reduced.
As shown in fig. 6-9, when the long bush 9 is machined, the working length L of the boring cutter 8 is greater than the length H of the bush, and the center of the circle is equidistantly shifted upwards for 5 times (total offset 1 mm) and downwards for 5 times (total offset 1 mm), so that the cutter back-off condition caused by insufficient cutter rigidity (cutter back-off H1 is reduced or zero) is effectively avoided, and the dimensional accuracy of the part 1 is ensured.
The offset of each cutter is controlled aiming at difficult-to-machine materials (such as 30 CrMnSiA), so that the machining process is more stable, and the cutter tooth breakage caused by large cutting allowance and overlarge cutting force can be effectively avoided; aiming at deep hole machining, the offset of each cutter is adjusted, the cutter back-off condition caused by the fact that the working length of the boring cutter 8 is large and the rigidity of the cutter is insufficient can be effectively avoided, and the machining precision of the part 1 is guaranteed.
The above description is only a preferred embodiment of the present invention, and is not intended to limit the present invention in any way, and all simple modifications and equivalent variations of the above embodiments according to the technical spirit of the present invention are included in the scope of the present invention.
Claims (5)
1. A boring method for an elliptical hole of a bushing is characterized in that a machining coordinate system is established by taking the center of the elliptical hole of the bushing as an original point, and a boring cutter conducts multiple equidistant offset machining in the forward direction or the reverse direction of a machining direction from the original point until a machining end point stops.
2. The method for boring the elliptical hole of the bushing as claimed in claim 1, wherein the boring cutter bores equidistantly and offset by 0.2 mm.
3. A boring method of an elliptical hole of a bushing according to claim 1 or 2, characterized in that a machining coordinate system is established with the center of the elliptical hole of the short bushing as an origin, and the boring cutter performs upward equidistant shifting of the center of the circle and downward equidistant shifting of the center of the circle several times along the Y direction of the machining coordinate system until the end points of the two ends of the major axis of the elliptical hole are machined.
4. A boring method of an elliptical hole in a bush as claimed in claim 3, characterized in that the total offset of the center of the circle shifted upward equidistantly and the center of the circle shifted downward equidistantly is 1mm, and the center of the circle shifted upward equidistantly and the center of the circle shifted downward equidistantly and 5 times respectively.
5. The method for boring the elliptical hole of the bushing as claimed in claim 1, wherein the working length L of the boring cutter is greater than the length H of the bushing when the long bushing is machined.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010687949.9A CN112008102B (en) | 2020-07-16 | 2020-07-16 | Boring method for elliptical hole of bushing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010687949.9A CN112008102B (en) | 2020-07-16 | 2020-07-16 | Boring method for elliptical hole of bushing |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN112008102A true CN112008102A (en) | 2020-12-01 |
| CN112008102B CN112008102B (en) | 2022-06-14 |
Family
ID=73498824
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010687949.9A Active CN112008102B (en) | 2020-07-16 | 2020-07-16 | Boring method for elliptical hole of bushing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112008102B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN118897505A (en) * | 2024-10-09 | 2024-11-05 | 潍柴动力股份有限公司 | Post-processing method of boring programming tool position source file and related device and machine tool system |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5730036A (en) * | 1994-10-07 | 1998-03-24 | Kabushiki Kikai Kabushiki Kaisha | Method of cutting ellipse contour with numerically-controlled machine tools |
| CN201862829U (en) * | 2010-09-16 | 2011-06-15 | 无锡华光工业锅炉有限公司 | Elliptical hole processing device |
| CN102968092A (en) * | 2012-12-10 | 2013-03-13 | 成都飞机工业(集团)有限责任公司 | Compilation method of numerical control (NC) program for boring high-precision symmetrical taper hole |
| CN206241299U (en) * | 2016-11-23 | 2017-06-13 | 山东滨州渤海活塞股份有限公司 | Connecting rod boring machine for boring special-shaped holes |
| CN206764404U (en) * | 2017-05-04 | 2017-12-19 | 重庆帅邦机械有限公司 | A kind of lathe boring crank eccentric orfice hydraulic pressure tunable arrangement |
-
2020
- 2020-07-16 CN CN202010687949.9A patent/CN112008102B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5730036A (en) * | 1994-10-07 | 1998-03-24 | Kabushiki Kikai Kabushiki Kaisha | Method of cutting ellipse contour with numerically-controlled machine tools |
| CN201862829U (en) * | 2010-09-16 | 2011-06-15 | 无锡华光工业锅炉有限公司 | Elliptical hole processing device |
| CN102968092A (en) * | 2012-12-10 | 2013-03-13 | 成都飞机工业(集团)有限责任公司 | Compilation method of numerical control (NC) program for boring high-precision symmetrical taper hole |
| CN206241299U (en) * | 2016-11-23 | 2017-06-13 | 山东滨州渤海活塞股份有限公司 | Connecting rod boring machine for boring special-shaped holes |
| CN206764404U (en) * | 2017-05-04 | 2017-12-19 | 重庆帅邦机械有限公司 | A kind of lathe boring crank eccentric orfice hydraulic pressure tunable arrangement |
Non-Patent Citations (2)
| Title |
|---|
| 何建民: "《铣工操作技术》", 31 August 1977, 机械工业出版社 * |
| 袁锡璠: "《现代机械制造工艺装备标准应用手册》", 31 December 1997, 机械工业出版社 * |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN118897505A (en) * | 2024-10-09 | 2024-11-05 | 潍柴动力股份有限公司 | Post-processing method of boring programming tool position source file and related device and machine tool system |
Also Published As
| Publication number | Publication date |
|---|---|
| CN112008102B (en) | 2022-06-14 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN203171033U (en) | Multi-stage composite chamfering forming drill | |
| CN103028752B (en) | Processing method for phi 52H7*850 deep hinge pin keyhole at matched position of parts of different materials | |
| CN112008102B (en) | Boring method for elliptical hole of bushing | |
| CN105522340A (en) | Main valve hole machining method for water press distributor valve body | |
| CN102310220A (en) | Process for roughly machining small groove by milling machine | |
| CN107900418A (en) | A kind of frock clamp for axial workpiece drilling processing | |
| CN108000081A (en) | A kind of high speed CNC deep hole processing methods | |
| CN105642918A (en) | Machining method for spiral rope groove of winding drum of large ship elevator | |
| CN102198527A (en) | Method for correcting eccentricity of drill type deep hole | |
| CN112372024A (en) | Method for machining deep hole with diameter more than 30 times by using inner-cooling drill bit | |
| CN222385972U (en) | Deep hole high-precision depth control device | |
| CN103586509A (en) | Forming spot-facer | |
| CN104338978A (en) | High-strength highly-durable drill bit | |
| CN108788635B (en) | Method for machining taper hole by using taper hole cutter | |
| CN211840295U (en) | Stepped drill tool | |
| CN105479099A (en) | Improved technology for machining deep groove parts by numerically-controlled lathe | |
| CN201320625Y (en) | Spiral drill reamer | |
| CN105382498A (en) | Processing method for thin-wall inner-cavity slender shaft component | |
| CN215199679U (en) | Machining tool for lathe | |
| CN107900379A (en) | A kind of processing method of helicla flute | |
| CN210172564U (en) | Piston machining cutter and piston machining lathe with same | |
| CN113458426A (en) | Method for machining and forming miniature bearing at one time | |
| CN203401119U (en) | High-strength highly-durable drill | |
| CN208083577U (en) | A kind of 5 sword precise forming reamers of PCD | |
| CN2933669Y (en) | Drill head for manufacturing crosswise aperture |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |