CN102166709A - Steel roof aluminum skirt piston machining process - Google Patents
Steel roof aluminum skirt piston machining process Download PDFInfo
- Publication number
- CN102166709A CN102166709A CN2011101397819A CN201110139781A CN102166709A CN 102166709 A CN102166709 A CN 102166709A CN 2011101397819 A CN2011101397819 A CN 2011101397819A CN 201110139781 A CN201110139781 A CN 201110139781A CN 102166709 A CN102166709 A CN 102166709A
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- boring
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Abstract
The invention discloses a steel roof aluminum skirt piston machining process, which comprises the following steps of: a, performing rough turning on a head and an excircle, and performing rough turning on a seam allowance and the excircle; b, roughly boring a pin hole, and milling the radius; c, performing finish turning on the seam allowance, milling a central hole, and performing semi-finish turning on the excircle and a top surface; d, performing semi-finish boring on the pin hole; e, boring the inner distance; f, checking the shape of an inner cavity; g, drilling; h, milling a spherical surface of a counter bore; i, drilling an oil return hole; j, turning a lock groove, and turning chamfering of the pin hole; k, milling an oil groove of the pin hole; l, performing finish boring on the pin hole; m, imitating an ellipse; n, turning holes and chamfering; and o, forming fitter chamfering, removing burr and flashing, and cleaning. By the steel roof aluminum skirt piston machining process, the machining accuracy is high, the process flow is precise and the quality of the machined product is high.
Description
Technical field
The present invention relates to a kind of steel crown and aluminum skirt piston processing technology.
Background technology
Traditional steel crown and aluminum skirt piston processing technology because technological process is meticulous inadequately, and on the artificial aging link technological requirement inaccuracy, cause the piston precision that processes by this kind processing technology not enough, product quality is relatively poor.
Summary of the invention
The purpose of this invention is to provide a kind of steel crown and aluminum skirt piston processing technology.
The technical scheme that the present invention is adopted for achieving the above object is: a kind of steel crown and aluminum skirt piston processing technology may further comprise the steps:
Step a, rough turn head and cylindrical, rough turn seam and cylindrical;
Step b, the heavy boring pin-and-hole mills radius;
Step c, the finish turning seam mills centre bore, half finish turning cylindrical and end face;
Steps d, half precision bored hole;
Step e, distance in the boring;
Step f checks cavity shape;
Step g, boring;
Step h mills the counterbore sphere;
Step j bores spill port;
Step k, lock annular groove, car pin-and-hole chamfering;
Step L mills the pin-and-hole oil duct;
Step m, precision bored hole;
Step n, imitative car ellipse;
Step o, car hole, chamfering;
Step p, pincers worker chamfered edge and deburring burr clean.
Boring is interior apart from being distances in boring 60,62 and 100 among the described step e.
Boring is for boring 6-8,4-13,6.5 and 2-9 holes in the described step g.
Steel crown and aluminum skirt piston processing technology of the present invention, the machining accuracy height, technological process is rigorous, and the product processed quality is higher.
Description of drawings
The invention will be further described below in conjunction with the drawings and specific embodiments.
Fig. 1 is the process chart of steel crown and aluminum skirt piston processing technology of the present invention.
The specific embodiment
As shown in Figure 1, steel crown and aluminum skirt piston processing technology of the present invention may further comprise the steps: step a, rough turn head and cylindrical, rough turn seam and cylindrical; Step b, the heavy boring pin-and-hole mills 4-25 radiuses; Step c, the finish turning seam mills centre bore, half finish turning cylindrical and end face; Steps d, half precision bored hole; Step e, distance in the boring 60,62 and 100; Step f checks cavity shape; Step g is bored 6-8,4-13,6.5 and 2-9 holes; Step h mills 4-27 counterbore spheres; Step j bores 2-6 spill ports; Step k, lock annular groove, car pin-and-hole chamfering; Step L mills the pin-and-hole oil duct; Step m, precision bored hole; Step n, imitative car ellipse; Step o, car 20 holes, 4-13,2-9,6.5 chamferings; Step p, pincers worker chamfered edge and deburring burr clean.
Claims (3)
1. a steel crown and aluminum skirt piston processing technology is characterized in that, may further comprise the steps:
Step a, rough turn head and cylindrical, rough turn seam and cylindrical;
Step b, the heavy boring pin-and-hole mills radius;
Step c, the finish turning seam mills centre bore, half finish turning cylindrical and end face;
Steps d, half precision bored hole;
Step e, distance in the boring;
Step f checks cavity shape;
Step g, boring;
Step h mills the counterbore sphere;
Step j bores spill port;
Step k, lock annular groove, car pin-and-hole chamfering;
Step L mills the pin-and-hole oil duct;
Step m, precision bored hole;
Step n, imitative car ellipse;
Step o, car hole, chamfering;
Step p, pincers worker chamfered edge and deburring burr clean.
2. steel crown and aluminum skirt piston processing technology according to claim 1 is characterized in that: boring is interior apart from being distances in boring 60,62 and 100 among the described step e.
3. steel crown and aluminum skirt piston processing technology according to claim 1 is characterized in that: boring is for boring 6-8,4-13,6.5 and 2-9 holes in the described step g.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2011101397819A CN102166709A (en) | 2011-05-27 | 2011-05-27 | Steel roof aluminum skirt piston machining process |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2011101397819A CN102166709A (en) | 2011-05-27 | 2011-05-27 | Steel roof aluminum skirt piston machining process |
Publications (1)
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CN102166709A true CN102166709A (en) | 2011-08-31 |
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CN2011101397819A Pending CN102166709A (en) | 2011-05-27 | 2011-05-27 | Steel roof aluminum skirt piston machining process |
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Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103753155A (en) * | 2013-12-25 | 2014-04-30 | 重庆水轮机厂有限责任公司 | Processing method for annular piston of water turbine and processing tool |
CN105750838A (en) * | 2016-04-13 | 2016-07-13 | 浙江锠泰机械工业有限公司 | Surface treatment method of piston hole in compressor |
CN108340172A (en) * | 2018-02-11 | 2018-07-31 | 安徽江淮汽车集团股份有限公司 | A kind of processing technology of diesel engine piston |
CN108723726A (en) * | 2018-04-24 | 2018-11-02 | 华意压缩机股份有限公司 | Piston and processing technology thereof |
CN109396774A (en) * | 2018-12-12 | 2019-03-01 | 湖南江滨机器(集团)有限责任公司 | A kind of method for making piston and piston production line |
CN115401427A (en) * | 2022-10-12 | 2022-11-29 | 中航动力株洲航空零部件制造有限公司 | Machining process for inner cavity of spacing ring |
-
2011
- 2011-05-27 CN CN2011101397819A patent/CN102166709A/en active Pending
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103753155A (en) * | 2013-12-25 | 2014-04-30 | 重庆水轮机厂有限责任公司 | Processing method for annular piston of water turbine and processing tool |
CN103753155B (en) * | 2013-12-25 | 2016-05-18 | 重庆水轮机厂有限责任公司 | A kind of hydraulic turbine annular piston processing technology and machining tool thereof |
CN105750838A (en) * | 2016-04-13 | 2016-07-13 | 浙江锠泰机械工业有限公司 | Surface treatment method of piston hole in compressor |
CN108340172A (en) * | 2018-02-11 | 2018-07-31 | 安徽江淮汽车集团股份有限公司 | A kind of processing technology of diesel engine piston |
CN108723726A (en) * | 2018-04-24 | 2018-11-02 | 华意压缩机股份有限公司 | Piston and processing technology thereof |
CN109396774A (en) * | 2018-12-12 | 2019-03-01 | 湖南江滨机器(集团)有限责任公司 | A kind of method for making piston and piston production line |
CN115401427A (en) * | 2022-10-12 | 2022-11-29 | 中航动力株洲航空零部件制造有限公司 | Machining process for inner cavity of spacing ring |
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Application publication date: 20110831 |