CN104625614A - Method for machining stainless steel deep-hole thin-wall part - Google Patents
Method for machining stainless steel deep-hole thin-wall part Download PDFInfo
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- CN104625614A CN104625614A CN201410744263.3A CN201410744263A CN104625614A CN 104625614 A CN104625614 A CN 104625614A CN 201410744263 A CN201410744263 A CN 201410744263A CN 104625614 A CN104625614 A CN 104625614A
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- 238000000034 method Methods 0.000 title claims abstract description 12
- 239000010935 stainless steel Substances 0.000 title claims abstract description 12
- 229910001220 stainless steel Inorganic materials 0.000 title claims abstract description 12
- 238000003754 machining Methods 0.000 title abstract description 13
- 239000000463 material Substances 0.000 claims abstract description 13
- 238000010438 heat treatment Methods 0.000 claims abstract description 6
- 238000010791 quenching Methods 0.000 claims abstract description 5
- 230000000171 quenching effect Effects 0.000 claims abstract description 5
- 238000000137 annealing Methods 0.000 claims abstract description 4
- 238000005553 drilling Methods 0.000 claims abstract description 4
- 238000003672 processing method Methods 0.000 claims description 9
- 239000010730 cutting oil Substances 0.000 claims description 6
- 239000002173 cutting fluid Substances 0.000 claims description 3
- 239000003921 oil Substances 0.000 claims description 3
- 238000005520 cutting process Methods 0.000 abstract description 6
- 238000001816 cooling Methods 0.000 abstract description 3
- 239000010687 lubricating oil Substances 0.000 abstract 1
- 238000004519 manufacturing process Methods 0.000 abstract 1
- 230000003746 surface roughness Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 238000005728 strengthening Methods 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 229910001069 Ti alloy Inorganic materials 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 239000012141 concentrate Substances 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 229910000734 martensite Inorganic materials 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 238000004881 precipitation hardening Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
- 238000005496 tempering Methods 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
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
- B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Drilling And Boring (AREA)
Abstract
The invention relates to the field of machining, in particular to a method for machining a stainless steel deep-hole thin-wall part. The method comprises the following steps that a proper blank material is selected, annealing treatment is carried out, and the cutting machining performance of the material is improved; rough turning is carried out, wherein working allowance of a blank is removed, and a workpiece inner hole is machined in dedicated equipment through a corresponding deep hole inner ejector drill; heat treatment and quenching are carried out; the appearance of a workpiece is clamped, and the end faces of the workpiece are turned; lead hole turning and chamfering are carried out; pull-boring and pull-hinging are carried out, the number of times of pull-boring and pull-hinging can be determined according to the working allowance, the number is generally two to four, pull-boring is carried out two times on a dedicated deep hole drilling and boring machine according to the characteristic of the part, after pull-boring is carried out once, the inner hole is machined with certain working allowance reserved, the inner hole is machined to the required size finally, and cooling lubricating oil is adopted in the machining process. According to the method, the precision requirement of the workpiece can be guaranteed, quality is stable and reliable, machining difficulty can be reduced, production efficiency can be improved, and the labor intensity of workers can be reduced.
Description
Technical field
The present invention relates to field of machining, be specifically related to stainless steel deep hole thin-walled parts processing method.
Background technology
Deep hole machining is as a kind of strongly professional, machining process that difficulty of processing is large, be widely used in the military industries such as Aeronautics and Astronautics, its processing precision direct influence the performance of product, particularly along with novel high-strength, high hardness material get more and more as difficult-to-machine material application such as titanium alloy, stainless steel, heat resisting steel, deep hole machining is had higher requirement.Therefore, for difficult-to-machine material, how to improve deep hole machining precision and become hot issue in machining.
Part material hardness is high, processing difficulties, following difficult point is mainly contained: (1) workpiece is precipitation-hardening stainless steel in actual process, martensitic structure is changed into after Quenching Treatment and cold treatment, precipitation strength phase after tempering, possess the resultant effect of phase transformation strengthening and ageing strengthening, there is after finished heat treatment high strength, plasticity, toughness and resistance to corrosion.(2) workpiece belongs to nickel-base alloy, thermal conductivity extreme difference, and during cutting, heat concentrates on cutting edge relief angle, causes cutting edge to produce plastic deformation, bonding and diffusive wear.(3) easily produce work hardening phenomenon in workpiece process, exacerbate the wearing and tearing of cutter, surface roughness value increases, and cutter life is reduced greatly, and cutter loss is serious.(4) during deep hole machining, chip removal is longer at rake face skidding distance, and chip easily and hole wall occurs to rub and extruding, and cutting temperature raises, and pulls bore area, is unfavorable for the precision in hole and the guarantee of surface roughness.(5) endoporus draw ratio is 1:10, and belong to deep hole thin-walled parts, required precision is higher, adopts conventional processing method to be difficult to ensure.(6) after heat treatment, the strength of materials and hardness high.
Summary of the invention
In order to final result the problems referred to above, the invention provides one and can ensure workpiece accuracy requirement, steady quality is reliable, reduces difficulty of processing, enhances productivity, and reduces the stainless steel deep hole thin-walled parts processing method of labor strength.
Stainless steel deep hole thin-walled parts processing method of the present invention, comprises the following steps:
The first step, selects suitable blank material, annealing in process, improves the machinability of material;
Second step, rough turn, remove the allowance of blank, inner hole of workpiece, on special equipment, adopts ejector drill processing in corresponding deep hole;
3rd step, heat treatment, quenching;
4th step, clamping workpiece profile, car workpiece end face;
5th step, car bullport and chamfering;
6th step, draw boring, draw hinge, draw boring, draw reamer number can determine according to allowance, be generally 2-4 cuttves, according to the feature of this part, on special deep hole drilling and boring machine, point two cuttves draw boring, after one cutter draws hinge, be machined to by endoporus and stay certain allowance, endoporus is machined to and requires size the most at last, in process, adopt cutting oil;
7th step, clamping workpiece profile, turner part both ends of the surface, ensure the overall length of workpiece, then adopt disposable mandrel, with Internal hole positioning, rough turn cylindrical is to requiring size, and as superfinishing honing benchmark, finally with excircle orientation, after centering, boring endoporus only requires size;
8th step, superfinishing Hole honing, adopts special Deep-hole Grouting oil in superfinishing Hole honing;
9th step, adopts disposable axle, with Internal hole positioning, and clamped one time, finish turning profile and two ends screw thread;
Tenth step, with excircle of workpiece location, after centering, the stepped hole at car endoporus two ends only requires size;
Preferably, boring cutter is drawn to adopt the uniform 180 ° of symmetrical centre cutters of four teeth.
Preferably, cutting oil adopts moral to moisten precious T400 inspecting hole extreme pressure cutting fluid.
The present invention can ensure workpiece accuracy requirement, and steady quality is reliable, reduces difficulty of processing, enhances productivity, and reduces labor strength.
Detailed description of the invention
Stainless steel deep hole thin-walled parts processing method of the present invention, comprises the following steps:
The first step, selects suitable blank material, annealing in process, improves the machinability of material;
Second step, rough turn, remove the allowance of blank, inner hole of workpiece, on special equipment, adopts ejector drill processing in corresponding deep hole;
3rd step, heat treatment, quenching;
4th step, clamping workpiece profile, car workpiece end face;
5th step, car bullport and chamfering;
6th step, draw boring, draw hinge, draw boring, draw reamer number can determine according to allowance, be generally 2-4 cuttves, according to the feature of this part, on special deep hole drilling and boring machine, point two cuttves draw boring, after one cutter draws hinge, be machined to by endoporus and stay certain allowance, endoporus is machined to and requires size the most at last, in process, adopt cutting oil;
7th step, clamping workpiece profile, turner part both ends of the surface, ensure the overall length of workpiece, then adopt disposable mandrel, with Internal hole positioning, rough turn cylindrical is to requiring size, and as superfinishing honing benchmark, finally with excircle orientation, after centering, boring endoporus only requires size;
8th step, superfinishing Hole honing, adopts special Deep-hole Grouting oil in superfinishing Hole honing;
9th step, adopts disposable axle, with Internal hole positioning, and clamped one time, finish turning profile and two ends screw thread;
Tenth step, with excircle of workpiece location, after centering, the stepped hole at car endoporus two ends only requires size; Boring cutter is drawn to adopt the uniform 180 ° of symmetrical centre cutters of four teeth.Cutting oil adopts moral to moisten precious T400 inspecting hole extreme pressure cutting fluid, it its have good cooling, the effect of cleaning misfortune essence, and there is higher heat-resisting, withstand voltage properties.When drawing boring, drawing hinge, make part and cutter obtain the band of cooling profit fully, effectively reduce the temperature of part, cutter, reduce the wearing and tearing of cutter, prevent long-pending generation of cutting, Part Surface Roughness is minimized.
Claims (3)
1. a stainless steel deep hole thin-walled parts processing method, is characterized in that, comprise the following steps:
The first step, selects suitable blank material, annealing in process, improves the machinability of material;
Second step, rough turn, remove the allowance of blank, inner hole of workpiece, on special equipment, adopts ejector drill processing in corresponding deep hole;
3rd step, heat treatment, quenching;
4th step, clamping workpiece profile, car workpiece end face;
5th step, car bullport and chamfering;
6th step, draw boring, draw hinge, draw boring, draw reamer number can determine according to allowance, be generally 2-4 cuttves, according to the feature of this part, on special deep hole drilling and boring machine, point two cuttves draw boring, after one cutter draws hinge, be machined to by endoporus and stay certain allowance, endoporus is machined to and requires size the most at last, in process, adopt cutting oil;
7th step, clamping workpiece profile, turner part both ends of the surface, ensure the overall length of workpiece, then adopt disposable mandrel, with Internal hole positioning, rough turn cylindrical is to requiring size, and as superfinishing honing benchmark, finally with excircle orientation, after centering, boring endoporus only requires size;
8th step, superfinishing Hole honing, adopts special Deep-hole Grouting oil in superfinishing Hole honing;
9th step, adopts disposable axle, with Internal hole positioning, and clamped one time, finish turning profile and two ends screw thread;
Tenth step, with excircle of workpiece location, after centering, the stepped hole at car endoporus two ends only requires size.
2. stainless steel deep hole thin-walled parts processing method as claimed in claim 1, is characterized in that, described in draw boring cutter to adopt the uniform 180 ° of symmetrical centre cutters of four teeth.
3. stainless steel deep hole thin-walled parts processing method as claimed in claim 2, is characterized in that, described cutting oil adopts moral to moisten precious T400 inspecting hole extreme pressure cutting fluid.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410744263.3A CN104625614A (en) | 2014-12-09 | 2014-12-09 | Method for machining stainless steel deep-hole thin-wall part |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410744263.3A CN104625614A (en) | 2014-12-09 | 2014-12-09 | Method for machining stainless steel deep-hole thin-wall part |
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| Publication Number | Publication Date |
|---|---|
| CN104625614A true CN104625614A (en) | 2015-05-20 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410744263.3A Pending CN104625614A (en) | 2014-12-09 | 2014-12-09 | Method for machining stainless steel deep-hole thin-wall part |
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Cited By (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105414890A (en) * | 2015-11-24 | 2016-03-23 | 沈阳黎明航空发动机(集团)有限责任公司 | Finish machining method for thin-walled conduit |
| CN105499935A (en) * | 2016-01-21 | 2016-04-20 | 中国矿业大学 | Machining technology for batch production of thin and long deep-hole complex parts |
| CN105750843A (en) * | 2016-04-29 | 2016-07-13 | 中国原子能科学研究院 | Inner hole machining method for molybdenum alloy thin-walled long pipe |
| CN105921955A (en) * | 2016-06-22 | 2016-09-07 | 山西平阳重工机械有限责任公司 | Machining method of high-precision step deep hole part |
| CN105945539A (en) * | 2016-07-12 | 2016-09-21 | 合肥新沪屏蔽泵有限公司 | Shield pump rotary shaft hole machining process |
| CN106015339A (en) * | 2016-06-30 | 2016-10-12 | 湖北三江航天红阳机电有限公司 | Machining method for conical-hole, thin-walled and high-precision shaft sleeve type part |
| CN106392118A (en) * | 2016-11-16 | 2017-02-15 | 中航飞机起落架有限责任公司 | Machining method for deep hole reverse cavity of undercarriage |
| CN108115176A (en) * | 2017-12-18 | 2018-06-05 | 航天科工哈尔滨风华有限公司 | A kind of high-precision step shaft titanium alloy material Fine and Deep Hole high-efficiency machining method |
| CN108127335A (en) * | 2017-10-31 | 2018-06-08 | 武汉船用机械有限责任公司 | A kind of processing method of taper pin-hole |
| CN108247302A (en) * | 2018-04-04 | 2018-07-06 | 四川华都核设备制造有限公司 | A kind of control rod drive mechanism blind hole stick stroke casing processing method and device |
| CN109079447A (en) * | 2018-10-18 | 2018-12-25 | 中船动力有限公司 | Diesel engine stand deep hole processing method |
| CN110091127A (en) * | 2019-04-25 | 2019-08-06 | 上海航天精密机械研究所 | A kind of thin-wall long and thin pipe fitting entirety precision machining method |
| CN110625139A (en) * | 2019-10-08 | 2019-12-31 | 江西洪都航空工业集团有限责任公司 | Machining process for bushing with conical hole |
| CN111015112A (en) * | 2019-12-23 | 2020-04-17 | 贵州凯星液力传动机械有限公司 | Machining method for thin-wall circular ring part |
| CN111805177A (en) * | 2020-07-06 | 2020-10-23 | 宁波市利宏航天科技有限公司 | Processing method of integrated circular thin-walled tube |
| CN112475792A (en) * | 2020-11-02 | 2021-03-12 | 武汉重工铸锻有限责任公司 | High-precision thin-wall copper part machining method |
| CN113649764A (en) * | 2020-12-22 | 2021-11-16 | 雅安新航精密铸造有限公司 | Machining process for discontinuous elongated holes in inclined plane of aviation casting part |
| CN114310160A (en) * | 2021-12-06 | 2022-04-12 | 齐齐哈尔建华机械有限公司 | Method for machining hardened deep-hole inner cone part |
| CN114789262A (en) * | 2022-06-02 | 2022-07-26 | 德州普利森机床有限公司 | A kind of deep hole machining technology of egg-shaped inner cavity |
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2014
- 2014-12-09 CN CN201410744263.3A patent/CN104625614A/en active Pending
Cited By (25)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105414890A (en) * | 2015-11-24 | 2016-03-23 | 沈阳黎明航空发动机(集团)有限责任公司 | Finish machining method for thin-walled conduit |
| CN105499935A (en) * | 2016-01-21 | 2016-04-20 | 中国矿业大学 | Machining technology for batch production of thin and long deep-hole complex parts |
| CN105750843A (en) * | 2016-04-29 | 2016-07-13 | 中国原子能科学研究院 | Inner hole machining method for molybdenum alloy thin-walled long pipe |
| CN105750843B (en) * | 2016-04-29 | 2017-12-26 | 中国原子能科学研究院 | A kind of method for machining bore of molybdenum alloy thin-wall long pipe |
| CN105921955B (en) * | 2016-06-22 | 2018-05-08 | 山西平阳重工机械有限责任公司 | A kind of processing method of high-precision step deep-hole type parts |
| CN105921955A (en) * | 2016-06-22 | 2016-09-07 | 山西平阳重工机械有限责任公司 | Machining method of high-precision step deep hole part |
| CN106015339A (en) * | 2016-06-30 | 2016-10-12 | 湖北三江航天红阳机电有限公司 | Machining method for conical-hole, thin-walled and high-precision shaft sleeve type part |
| CN105945539A (en) * | 2016-07-12 | 2016-09-21 | 合肥新沪屏蔽泵有限公司 | Shield pump rotary shaft hole machining process |
| CN106392118A (en) * | 2016-11-16 | 2017-02-15 | 中航飞机起落架有限责任公司 | Machining method for deep hole reverse cavity of undercarriage |
| CN108127335A (en) * | 2017-10-31 | 2018-06-08 | 武汉船用机械有限责任公司 | A kind of processing method of taper pin-hole |
| CN108127335B (en) * | 2017-10-31 | 2020-06-26 | 武汉船用机械有限责任公司 | Method for machining taper pin hole |
| CN108115176A (en) * | 2017-12-18 | 2018-06-05 | 航天科工哈尔滨风华有限公司 | A kind of high-precision step shaft titanium alloy material Fine and Deep Hole high-efficiency machining method |
| CN108247302A (en) * | 2018-04-04 | 2018-07-06 | 四川华都核设备制造有限公司 | A kind of control rod drive mechanism blind hole stick stroke casing processing method and device |
| CN108247302B (en) * | 2018-04-04 | 2024-02-27 | 四川华都核设备制造有限公司 | Method and device for processing blind hole rod travel sleeve of control rod driving mechanism |
| CN109079447A (en) * | 2018-10-18 | 2018-12-25 | 中船动力有限公司 | Diesel engine stand deep hole processing method |
| CN110091127A (en) * | 2019-04-25 | 2019-08-06 | 上海航天精密机械研究所 | A kind of thin-wall long and thin pipe fitting entirety precision machining method |
| CN110625139A (en) * | 2019-10-08 | 2019-12-31 | 江西洪都航空工业集团有限责任公司 | Machining process for bushing with conical hole |
| CN111015112A (en) * | 2019-12-23 | 2020-04-17 | 贵州凯星液力传动机械有限公司 | Machining method for thin-wall circular ring part |
| CN111805177A (en) * | 2020-07-06 | 2020-10-23 | 宁波市利宏航天科技有限公司 | Processing method of integrated circular thin-walled tube |
| CN112475792A (en) * | 2020-11-02 | 2021-03-12 | 武汉重工铸锻有限责任公司 | High-precision thin-wall copper part machining method |
| CN112475792B (en) * | 2020-11-02 | 2022-05-24 | 武汉重工铸锻有限责任公司 | High-precision thin-wall copper part machining method |
| CN113649764A (en) * | 2020-12-22 | 2021-11-16 | 雅安新航精密铸造有限公司 | Machining process for discontinuous elongated holes in inclined plane of aviation casting part |
| CN114310160A (en) * | 2021-12-06 | 2022-04-12 | 齐齐哈尔建华机械有限公司 | Method for machining hardened deep-hole inner cone part |
| CN114310160B (en) * | 2021-12-06 | 2024-03-15 | 齐齐哈尔建华机械有限公司 | Processing method of quenched deep hole inner cone part |
| CN114789262A (en) * | 2022-06-02 | 2022-07-26 | 德州普利森机床有限公司 | A kind of deep hole machining technology of egg-shaped inner cavity |
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Application publication date: 20150520 |
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