CN102357693B - Method for machining high-precision deep hole - Google Patents

Method for machining high-precision deep hole Download PDF

Info

Publication number
CN102357693B
CN102357693B CN 201110268501 CN201110268501A CN102357693B CN 102357693 B CN102357693 B CN 102357693B CN 201110268501 CN201110268501 CN 201110268501 CN 201110268501 A CN201110268501 A CN 201110268501A CN 102357693 B CN102357693 B CN 102357693B
Authority
CN
China
Prior art keywords
deep hole
hole
machining
workpiece
endoporus
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.)
Expired - Fee Related
Application number
CN 201110268501
Other languages
Chinese (zh)
Other versions
CN102357693A (en
Inventor
戚爱春
韩卫刚
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
No 618 Research Institute of China Aviation Industry
Original Assignee
No 618 Research Institute of China Aviation Industry
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by No 618 Research Institute of China Aviation Industry filed Critical No 618 Research Institute of China Aviation Industry
Priority to CN 201110268501 priority Critical patent/CN102357693B/en
Publication of CN102357693A publication Critical patent/CN102357693A/en
Application granted granted Critical
Publication of CN102357693B publication Critical patent/CN102357693B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
  • Finish Polishing, Edge Sharpening, And Grinding By Specific Grinding Devices (AREA)

Abstract

The invention discloses a method for machining a high-precision deep hole, and particularly relates to a deep hole with the length to diameter ratio being more than 10. Based on the traditional deep hole machining method, the method utilizes the characteristics and advantages of the low-speed wire-cutting for machining a workpiece and adds the low-speed wire-cutting in the finishing machining process of the deep hole, so that the aim of straightening the straightness of an inner hole is achieved, an excellent basis hole for the following honing is provided, and the straightness of the deep hole can be equal to or less than 0.002 mm, and the roughness Ra of the deep hole is 0.4 microns through finish honing and grinding. Compared with the traditional machining method, the method for machining the deep hole disclosed by the invention has the advantages of high efficiency, stable quality and passing rate over 98%.

Description

A kind of method for machining high-precision deep hole
Technical field
The present invention relates to a kind of deep hole processing method, especially draw ratio is greater than 10 deep hole processing method.
Background technology
Deep-Hole Drilling Technology, the supporting subsequent fine process technology of gun drilling especially are the bottlenecks of China's manufacturing industry development always.The draw ratio of multiple valve bush part endoporus has reached more than 10 times in the aeronautical product, linearity requirement≤0.002mm, Ra0.4.Usually in the machining process route after the valve bush part heat treatment, the processing of endoporus is undertaken by four procedures, and a honing is ground for three times.Honing is to revise the defective that produces in the operation of front with the effect of grinding step, manual to a power F radially during honing, shown in Figure of description 1, make its many places crowning become large, then eliminate crowning again, thereby make its linearity bring up to 0.002mm through repeatedly several checks of taking turns and honing, this processing method efficient is low, quality is unstable, and qualification rate is low.
Summary of the invention
The deficiency low for above-mentioned worker's method efficient, that quality is unstable, qualification rate is low the invention provides a kind of slow wire feeding wire-electrode cutting and processing method that utilizes.Purpose of the present invention: for the prior art difficult point, provide a kind of fine-processing technique method of High-precision Deep Hole, the linearity of deep hole is reached≤0.002mm, Ra0.4, and efficient is high, steady quality.
The technical scheme that the present invention takes is: a kind of method for machining high-precision deep hole may further comprise the steps:
Step 1: drill gun roughing endoporus;
Step 2: thick top gem of a girdle-pendant endoporus; Revise various errors and blemish except axis deviation, and good machining benchmark is provided for the silk thread cutting of being careful, stay allowance 0.15 ~ 0.3mm.
Step 3: the silk thread of being careful cutting semifinishing endoporus;
1) utilizes on the slow feeding linear cutting bed hole that cooperates with workpiece (4) cylindrical in mold (1) processing;
2) workpiece (4) is put into the hole of mold (1), and fixing with holding out against screw (2);
3) utilize the silk thread cutting processing of being careful to come the alignment bent hole, for follow-up honing provides good basic hole, stay allowance 0.03~0.05mm; Concrete steps are as follows:
Utilize the centering function of slow wire feeding lathe, determine the center of workpiece (4) bottom outlet, setup parameter carries out semifinishing, stays allowance 0.03~0.05mm, and parameter is as follows:
Wire electrode:
Figure GDA00002648773200021
Brass wire
Wire travelling speed: 10m/min
Thread tension: 2N
Water spray pressure: 0
Pulse width: 6 μ s
Pulse spacing: 0.1 μ s
The average reference voltage of servo-drive system: 34.5V
Step 4: smart top gem of a girdle-pendant endoporus; Honing guarantees the roughness grade number of requirement.
Step 5: grind; Grind and obtain good surface quality, guarantee that part has accurate physical dimension.
Further, in order better to implement the present invention, the above-mentioned screw (2) that holds out against is for copper.
Further, in order better to implement the present invention, the above-mentioned contact surface that holds out against screw (2) and workpiece (4) is circular shape.
Advantage of the present invention and beneficial effect: the silk thread cutting processing of being careful technology is as a kind of special processing technology, has very strong practical value, play an important role at numerous field of industrial productions, its process means in many cases conventional manufacturing technology can't replace.The intrinsic processing characteristics of silk thread cutting owing to be careful: be not subjected to the workpiece material physical property, as the impact of hardening, and itself seldom produces cutting stress, the control of instrument and workpiece relative motion is fairly simple, the clamping of workpiece is relatively simple, has saved cost, has improved efficient.The present invention adopts the silk thread cutting processing of being careful to come " alignment " bent hole in the fine finishining of High-precision Deep Hole, for follow-up honing provides good basic hole, makes the working (machining) efficiency of High-precision Deep Hole improve steady quality.
Description of drawings
Fig. 1 is High-precision Deep Hole traditional diamond-making technique schematic diagram;
Fig. 2 is the machining accuracy deep hole flow chart;
Fig. 3 is the clamping schematic diagram of workpiece when being careful the silk thread cutting processing, 1: mold, 2: hold out against screw, 3: wire electrode, 4: workpiece;
Fig. 4 holds out against the screw schematic diagram;
Fig. 5 is the variation contrast schematic diagram of axis before and after the silk thread cutting processing of being careful.
The specific embodiment
Below in conjunction with the explanation accompanying drawing the present invention is elaborated.
Take an external diameter as
Figure GDA00002648773200031
The workpiece of height L:200mm is example, requires the processing internal diameter to arrive
Figure GDA00002648773200032
Linearity≤0.002mm, roughness 0.4 μ m sets forth the specific embodiment of this patent.
Step 1: drill gun roughing endoporus;
Internal diameter by roughing such as drill gun, heat treatments after size to
Figure GDA00002648773200041
Step 2: thick top gem of a girdle-pendant endoporus; Revise various errors and blemish except axis deviation, and good machining benchmark is provided for the silk thread cutting of being careful, stay allowance 0.15~0.3mm, internal diameter is worked into
Figure GDA00002648773200042
Step 3: the silk thread of being careful cutting semifinishing endoporus;
1) utilizes on the slow feeding linear cutting bed in mold 1 processing and workpiece 4 cylindricals
Figure GDA00002648773200043
The hole that cooperates, fit clearance is 0.04mm;
2) workpiece 4 is put into mold 1, and hand-tight make-up two M5 with annular knurl to hold out against screw 2 fixing, as shown in Figure 3;
Hold out against cut for the surface that holds out against 2 pairs of workpiece 4 of screw is not produced, present embodiment is taked holds out against screw 2 for copper, and further, the contact surface that holds out against screw 2 and workpiece 4 is designed to circular-arc, as shown in Figure 4;
3) utilize the centering function of slow wire feeding lathe, determine the center of workpiece 4 bottom outlets, this center is the working origin of workpiece 4, and setting parameter is as follows:
Lathe: Switzerland Archie Xia Mier ROBFIL 440CC
Wire electrode:
Figure GDA00002648773200044
Brass wire
Wire travelling speed: 10m/min
Thread tension: 2N
Water spray pressure: 0
Pulse width: 6 μ s
Pulse spacing: 0.1 μ s
The average reference voltage of servo-drive system: 34.5V
The employing silk thread cutting processing of being careful is come the alignment bent hole, for follow-up honing provides good basic hole, stays allowance 0.03~0.05mm, and internal diameter size is worked into
Figure GDA00002648773200051
Step 4: smart top gem of a girdle-pendant endoporus; The honing internal diameter size
Figure GDA00002648773200052
And the roughness grade number of assurance requirement;
Step 5: grind; Grind and obtain good surface quality, guarantee that part has accurate physical dimension.
Fig. 5 is the variation contrast schematic diagram of axis before and after the silk thread cutting processing of being careful.
Beneficial effect: the present invention adopts the silk thread cutting processing of being careful to come the alignment bent hole in the processing of High-precision Deep Hole, for follow-up honing provides good basic hole, makes the working (machining) efficiency of High-precision Deep Hole improve steady quality.

Claims (3)

1. method for machining high-precision deep hole may further comprise the steps:
Step 1: drill gun roughing endoporus;
Step 2: thick top gem of a girdle-pendant endoporus; Revise various errors and blemish except axis deviation, and good machining benchmark is provided for the silk thread cutting of being careful, stay allowance 0.15 ~ 0.3mm;
Step 3: the silk thread of being careful cutting semifinishing endoporus;
1) utilizes on the slow feeding linear cutting bed hole that cooperates with workpiece (4) cylindrical in mold (1) processing;
2) workpiece (4) is put into the hole of mold (1), and fixing with holding out against screw (2);
3) utilize the silk thread cutting processing of being careful to come the alignment bent hole, for follow-up honing provides good basic hole, stay allowance 0.03~0.05mm; Concrete steps are as follows:
Utilize the centering function of slow wire feeding lathe, determine the center of workpiece (4) bottom outlet, setup parameter carries out semifinishing, stays allowance 0.03~0.05mm, and parameter is as follows:
Wire electrode:
Figure FDA00002648773100011
Brass wire
Wire travelling speed: 10m/min
Thread tension: 2N
Water spray pressure: 0
Pulse width: 6 μ s
Pulse spacing: 0.1 μ s
The average reference voltage of servo-drive system: 34.5V
Step 4: smart top gem of a girdle-pendant endoporus; Honing guarantees the roughness grade number of requirement;
Step 5: grind; Grind and obtain good surface quality, guarantee that part has accurate physical dimension.
2. method for machining high-precision deep hole according to claim 1 is characterized in that: hold out against screw (2) for copper.
3. method for machining high-precision deep hole according to claim 2 is characterized in that: the contact surface that holds out against screw (2) and workpiece (4) is circular shape.
CN 201110268501 2011-09-08 2011-09-08 Method for machining high-precision deep hole Expired - Fee Related CN102357693B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201110268501 CN102357693B (en) 2011-09-08 2011-09-08 Method for machining high-precision deep hole

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201110268501 CN102357693B (en) 2011-09-08 2011-09-08 Method for machining high-precision deep hole

Publications (2)

Publication Number Publication Date
CN102357693A CN102357693A (en) 2012-02-22
CN102357693B true CN102357693B (en) 2013-04-10

Family

ID=45583105

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201110268501 Expired - Fee Related CN102357693B (en) 2011-09-08 2011-09-08 Method for machining high-precision deep hole

Country Status (1)

Country Link
CN (1) CN102357693B (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102794622B (en) * 2012-09-11 2014-12-24 广州泰胜数控机械有限公司 Machining method of precise inner gear
CN104526532A (en) * 2013-12-27 2015-04-22 邵阳维克液压股份有限公司 Method for machining concentric holes of variable shell of axial plunger pump and clamp
CN103817588B (en) * 2014-03-14 2016-08-17 邓湘凌 Pore finishing method
CN105643032B (en) * 2014-11-14 2018-04-10 中国航空工业第六一八研究所 A kind of processing method of the high-precision small square hole of revolving parts radial direction
CN105643206A (en) * 2015-12-11 2016-06-08 长春航空液压控制有限公司 Processing method for inner hole of ultra-precise valve sleeve
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
CN108246829A (en) * 2017-12-26 2018-07-06 张家港华裕有色金属材料有限公司 A kind of manufacturing method of TA18 titanium alloys seamless tube blank
CN110893579B (en) * 2019-10-22 2021-05-28 南京航空航天大学 Honing surface roughness prediction method considering oilstone yielding
CN112571096B (en) * 2020-12-22 2022-01-14 苏州萨伯工业设计有限公司 Method for adjusting installation precision of lathe tool rest
CN112658696B (en) * 2021-01-06 2023-07-07 宁波舜邦模具科技有限公司 Micron-sized guide pillar hole machining device and machining method
CN113829012B (en) * 2021-09-29 2022-12-06 成都光明光电有限责任公司 Glass discharge tube and method for producing the same
CN114054874B (en) * 2021-11-19 2022-08-16 厦门虹鹭钨钼工业有限公司 High-precision 3D printing two-dimensional collimator positioning and processing method
CN117139759B (en) * 2023-10-31 2024-01-23 赫比(成都)精密塑胶制品有限公司 Machining method of multi-section special-shaped conical hole and workpiece

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62120921A (en) * 1985-11-20 1987-06-02 Mitsubishi Metal Corp Continuously boring machine for superfine deep hole
CN100404195C (en) * 2004-02-20 2008-07-23 上海大量电子设备有限公司 Combined machine-tool possessing fast wire-moving cutting and deep small hole processing functions
CN201659466U (en) * 2009-11-27 2010-12-01 中国直升机设计研究所 Deep-hole grinding device
CN201913271U (en) * 2010-12-16 2011-08-03 东莞市垠星科技发展有限公司 High-precision deep hole processor
CN201940784U (en) * 2010-12-21 2011-08-24 苏州工业职业技术学院 Machining device of large length-diameter ratio nonferrous metal step deep hole

Also Published As

Publication number Publication date
CN102357693A (en) 2012-02-22

Similar Documents

Publication Publication Date Title
CN102357693B (en) Method for machining high-precision deep hole
CN105643032B (en) A kind of processing method of the high-precision small square hole of revolving parts radial direction
CN103949851A (en) Processing method of aluminum alloy thin-wall cylindrical part
CN103406736B (en) Lens tube of digital camera plastic mould precise molectron processing technique
CN204053021U (en) A kind of round-disk shape workpiece Quick drilling tool
CN105171158A (en) Technology for machining conical gas film holes of turbine guide blade
CN101869960A (en) Bush processing technology
CN102744475B (en) Method and device for electrolytic cutting for grouped line electrodes
CN202097619U (en) Grinding tool for taper hole
CN104308310A (en) Efficient and quick electrode-replacing clamping fixture
CN202155619U (en) Electrode for machining internal threads on hard alloy materials
CN204234927U (en) A kind of efficient electrode fast changes clamping fixture
CN204277596U (en) A kind of spindle of numerical control lathe location structure
CN108098474B (en) A kind of processing method of fixture and eccentric drill bushing for the processing of eccentric drill bushing
CN106563858B (en) Revolving parts wire-electrode cutting and processing method based on profile approximatioss
CN104690491A (en) Precision machining method of easy-deformed structure aluminum dovetail groove
CN105522340A (en) Main valve hole machining method for water press distributor valve body
CN101844313A (en) Novel adjustable eccentric clamping head
CN204976137U (en) Positioner is used in lathe processing
CN203449055U (en) Expansion type axial positioner
CN103464988B (en) A kind of uiform section blade profile minute yardstick turbine electric discharge machining apparatus and process thereof
CN105081709A (en) Machining method for large bent top tool rest part
CN205032744U (en) Knife rest structure for processing watch clamping plate by numerical control lathe
CN110293378A (en) A kind of ultraprecise bushing processing method
CN104526427A (en) Lathe main shaft positioning structure

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20130410

Termination date: 20180908