CN114178791A - Machining process of thrust bearing shell or protector shell - Google Patents

Machining process of thrust bearing shell or protector shell Download PDF

Info

Publication number
CN114178791A
CN114178791A CN202111531032.0A CN202111531032A CN114178791A CN 114178791 A CN114178791 A CN 114178791A CN 202111531032 A CN202111531032 A CN 202111531032A CN 114178791 A CN114178791 A CN 114178791A
Authority
CN
China
Prior art keywords
shell
thrust bearing
protector
bearing shell
face
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.)
Pending
Application number
CN202111531032.0A
Other languages
Chinese (zh)
Inventor
尚兴忠
陈爱民
陈金磊
赵冬青
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.)
Shandong Baoshida Petroleum Equipment Manufacturing Co ltd
Original Assignee
Shandong Baoshida Petroleum Equipment Manufacturing Co ltd
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 Shandong Baoshida Petroleum Equipment Manufacturing Co ltd filed Critical Shandong Baoshida Petroleum Equipment Manufacturing Co ltd
Publication of CN114178791A publication Critical patent/CN114178791A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Sliding-Contact Bearings (AREA)

Abstract

The invention provides a thrust bearing shell or protector shell processing technology, which comprises the following processing steps: 1) honing an inner hole of the thrust bearing shell or the protector shell to a required size; 2) clamping one end of the thrust bearing shell or the protector shell by using a lathe chuck, aligning the other end face of the thrust bearing shell or the protector shell, polishing and removing burrs at the end face, and turning around the other end after finishing one end; 3) using a centre to push and push inner holes at two ends of the bearing shell or the protector shell, and turning an outer circle by a lathe; 4) and clamping the excircle part of the thrust bearing shell or the protector shell by using a double-end numerical control lathe, and simultaneously processing the rabbet parts and the thread parts at two ends of the thrust bearing shell or the protector shell. The invention ensures the requirements of the form and position tolerance of the shell (the coaxiality tolerance is less than or equal to 0.02mm, and the end face parallelism tolerance is less than or equal to 0.01 mm), has high processing efficiency and saves raw materials; the working efficiency is high, the operation is simple, the learning is easy, and the processing difficulty is low.

Description

Machining process of thrust bearing shell or protector shell
Technical Field
The invention relates to the field of oil pumping downhole equipment, in particular to a thrust bearing shell or protector shell machining process.
Background
The working environment of the pumping down-hole equipment is complex and the conditions are severe; the quality of the oil can directly affect the yield of the oil well. Therefore, the machining precision of the parts of the underground equipment is high, and the requirements on the shape and position tolerance are very strict. For example, the position tolerance requirements of the thrust bearing shell and the protector shell are very strict, the end face parallelism tolerance of two ends of the shell is less than or equal to 0.01mm, the coaxiality tolerance requirements of the axes of the spigot part and the thread part of the two ends of the shell and the axis of the inner hole of the shell are less than or equal to 0.02mm, and therefore a set of reasonable processing technology is required in the processing process of the shell.
At present, one end of a thrust bearing shell or a protector shell is clamped by a chuck of a lathe to be machined (the end face is turned, the spigot is turned, the thread is turned), and the other end of the shell is machined after the machining process is finished.
Disclosure of Invention
The invention aims to solve the defects in the prior art and provides a machining process of a thrust bearing shell or a protector shell.
The new technical scheme of the invention is as follows:
a processing technology for a thrust bearing shell or a protector shell comprises inner hole honing, end face deburring, double-top turning and double-end turning, and comprises the following processing steps:
1) honing an inner hole of the thrust bearing shell or the protector shell to a required size;
2) clamping one end of the thrust bearing shell or the protector shell by using a lathe chuck, aligning the other end face of the thrust bearing shell or the protector shell, polishing and removing burrs at the end face, and turning around the other end after finishing one end;
3) using a centre to push and push inner holes at two ends of the bearing shell or the protector shell, and turning an outer circle by a lathe;
4) and clamping the excircle part of the thrust bearing shell or the protector shell by using a double-end numerical control lathe, and simultaneously processing the rabbet parts and the thread parts at two ends of the thrust bearing shell or the protector shell.
After the end face is trimmed in the step 2), the verticality tolerance of the end face is not more than 0.05 mm.
The spigot parts and the thread parts at the two ends of the thrust bearing shell or the protector shell and the inner hole have the coaxiality tolerance of less than 0.02 mm.
The parallelism tolerance of two end faces of the thrust bearing shell or the protector shell is less than 0.01 mm.
The invention has the following beneficial effects: the invention ensures the requirements of the form and position tolerance of the shell (the coaxiality tolerance is less than or equal to 0.02mm, and the end face parallelism tolerance is less than or equal to 0.01 mm), has high processing efficiency and saves raw materials; the working efficiency is high, the operation is simple, the learning is easy, and the processing difficulty is low.
Detailed Description
A processing technology for a thrust bearing shell or a protector shell comprises inner hole honing, end face deburring, double-top turning and double-end turning, and comprises the following processing steps:
1) honing an inner hole of the thrust bearing shell or the protector shell to a required size;
2) clamping one end of the thrust bearing shell or the protector shell by using a lathe chuck, aligning the other end face of the thrust bearing shell or the protector shell, polishing and removing burrs at the end face, and turning around the other end after finishing one end;
3) using a centre to push and push inner holes at two ends of the bearing shell or the protector shell, and turning an outer circle by a lathe;
4) and clamping the excircle part of the thrust bearing shell or the protector shell by using a double-end numerical control lathe, and simultaneously processing the rabbet parts and the thread parts at two ends of the thrust bearing shell or the protector shell.
After the end face is trimmed in the step 2), the verticality tolerance of the end face is not more than 0.05 mm.
The spigot parts and the thread parts at the two ends of the thrust bearing shell or the protector shell and the inner hole have the coaxiality tolerance of less than 0.02 mm.
The parallelism tolerance of two end faces of the thrust bearing shell or the protector shell is less than 0.01 mm.
Example (b):
honing an inner hole to phi 89-0.100+0.179 mm by using a deep hole honing machine, blanking length 6050+1mm by using a band sawing machine, end face verticality is less than or equal to 1mm, clamping one end of a shell by using a lathe clamping jaw, holding a center frame by the other end, flattening two end faces, polishing an inner opening by using oilstone to remove burrs, cleaning the inner openings at two ends of the shell, checking whether the burrs exist, and wiping two centers of a lathe completely; and (3) double-top turning of the outer circle to phi 101.60+0.3mm, adopting a 35-degree diamond outer circle turning tool, wherein the rotating speed of a lathe spindle is 640r/min, and the feed rate is F0.2 (attention is paid to the processing roughness, the outer circle is smooth and the like). Transferring to a double-head numerical control lathe, placing the shell with the outer circle in a main shaft hole, positioning the left side by using a tool rest positioning tool, and clamping the exposed shell with 75mm by using a hydraulic chuck (the outer circle of the shell is cleaned before each clamping, and the clamp of the machine tool is cleaned); aligning the end face, keeping the total length 601 +/-0.1 mm, ensuring the roughness of the end face to be less than or equal to Ra1.6, ensuring the verticality of the end face to be less than or equal to 0.05mm, ensuring the parallelism of the two end faces to be less than or equal to 0.013 mm, and chamfering the outer part of the end face by 0.5 multiplied by 45 degrees; the vehicle rabbet is phi 92+0.08+0.32 multiplied by 20 +/-0.1 mm, the rabbet roughness is less than or equal to Ra1.6, the coaxiality is less than or equal to phi 0.02, the root part is chamfered by 30 degrees, the end part is chamfered by R1, and the fillet roughness is less than or equal to Ra1.6; turning 3.603-18UNF-3B internal threads, ensuring that the effective length of the threads is 30mm, and ensuring that the coaxiality tolerance of the axis of the internal threads and the reference shaft A is less than or equal to phi 0.08; and (3) requiring the go gauge to go to the no-go gauge, detecting the go gauge and the no-go gauge in time, and adjusting in time when the go gauge is not go or the no-go gauge is not go.

Claims (4)

1. The utility model provides a footstep bearing casing or protector casing processing technology, includes hole honing, neat terminal surface burring, two top turning excircle and double-end car processing, its characterized in that:
the processing technology comprises the following steps:
1) honing an inner hole of the thrust bearing shell or the protector shell to a required size;
2) clamping one end of the thrust bearing shell or the protector shell by using a lathe chuck, aligning the other end face of the thrust bearing shell or the protector shell, polishing and removing burrs at the end face, and turning around the other end after finishing one end;
3) using a centre to push and push inner holes at two ends of the bearing shell or the protector shell, and turning an outer circle by a lathe;
4) and clamping the excircle part of the thrust bearing shell or the protector shell by using a double-end numerical control lathe, and simultaneously processing the rabbet parts and the thread parts at two ends of the thrust bearing shell or the protector shell.
2. The process of claim 1, wherein the step of machining the thrust bearing housing or the protector housing comprises the steps of: after the end face is trimmed in the step 2), the verticality tolerance of the end face is not more than 0.05 mm.
3. The process of claim 1, wherein the step of machining the thrust bearing housing or the protector housing comprises the steps of: the spigot parts and the thread parts at the two ends of the thrust bearing shell or the protector shell and the inner hole have the coaxiality tolerance of less than 0.02 mm.
4. The process of claim 1, wherein the step of machining the thrust bearing housing or the protector housing comprises the steps of: the parallelism tolerance of two end faces of the thrust bearing shell or the protector shell is less than 0.01 mm.
CN202111531032.0A 2021-09-15 2021-12-15 Machining process of thrust bearing shell or protector shell Pending CN114178791A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN2021110787992 2021-09-15
CN202111078799 2021-09-15

Publications (1)

Publication Number Publication Date
CN114178791A true CN114178791A (en) 2022-03-15

Family

ID=80605095

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202111531032.0A Pending CN114178791A (en) 2021-09-15 2021-12-15 Machining process of thrust bearing shell or protector shell

Country Status (1)

Country Link
CN (1) CN114178791A (en)

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8601639D0 (en) * 1985-01-24 1986-02-26 Bosch Gmbh Robert Rotationally symmetrical housing
DD292162A5 (en) * 1986-05-06 1991-07-25 Kombinat Waelzlager Und Normteile,De METHOD FOR PRODUCING PREFERRED BELT STORAGE RINGS FROM TUBE MATERIAL
US20080169709A1 (en) * 2005-04-25 2008-07-17 Tae Wook Lee Spindle Motor and Fabricating Method Thereof
CN103372754A (en) * 2012-04-13 2013-10-30 于强 Thrust bearing production process
CN103909433A (en) * 2014-04-04 2014-07-09 沈阳华扬机械有限公司 Machining fixture and method of eccentric bushings for cone crushers
CN104043802A (en) * 2014-06-30 2014-09-17 南车戚墅堰机车车辆工艺研究所有限公司 Mould and method for manufacturing bimetal plain thrust sliding bearing blank and manufacturing method thereof
CN104084759A (en) * 2014-06-23 2014-10-08 河南伟彤科技股份有限公司 Device and method for processing cylinder barrel blank of hydraulic cylinder
CN105252223A (en) * 2015-11-11 2016-01-20 宝塔实业股份有限公司 Machining method of extra-large bearing cone rolling bodies with supporting column holes

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8601639D0 (en) * 1985-01-24 1986-02-26 Bosch Gmbh Robert Rotationally symmetrical housing
DD292162A5 (en) * 1986-05-06 1991-07-25 Kombinat Waelzlager Und Normteile,De METHOD FOR PRODUCING PREFERRED BELT STORAGE RINGS FROM TUBE MATERIAL
US20080169709A1 (en) * 2005-04-25 2008-07-17 Tae Wook Lee Spindle Motor and Fabricating Method Thereof
CN103372754A (en) * 2012-04-13 2013-10-30 于强 Thrust bearing production process
CN103909433A (en) * 2014-04-04 2014-07-09 沈阳华扬机械有限公司 Machining fixture and method of eccentric bushings for cone crushers
CN104084759A (en) * 2014-06-23 2014-10-08 河南伟彤科技股份有限公司 Device and method for processing cylinder barrel blank of hydraulic cylinder
CN104043802A (en) * 2014-06-30 2014-09-17 南车戚墅堰机车车辆工艺研究所有限公司 Mould and method for manufacturing bimetal plain thrust sliding bearing blank and manufacturing method thereof
CN105252223A (en) * 2015-11-11 2016-01-20 宝塔实业股份有限公司 Machining method of extra-large bearing cone rolling bodies with supporting column holes

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
杨敬娜等: "工程机械用液压缸加工工艺分析", 《山东工业技术》 *

Similar Documents

Publication Publication Date Title
CN104625602A (en) Method for machining thin-wall bearing housing part
JP5155847B2 (en) Eccentric hole machining method by machine tool
CN101537509A (en) Method and tool for machining step deep holes
CN105643032A (en) Machining method for radial high-precision small square holes of rotary part
CN112621412A (en) Surface treatment equipment with chip collection function for bearing production
CN109986305A (en) A kind of prestress forming method for grinding of non-circular " three-section wave shape " raceway of thin-walled
CN116493882A (en) Method for processing thin-wall retaining sleeve type part by using special tool
CN114227176B (en) Bearing pad processing method
CN114589464A (en) Method for machining inner hole of high-precision long and thin cylindrical part
CN109877543A (en) A kind of processing method of hydraulic cylinder body
CN114178791A (en) Machining process of thrust bearing shell or protector shell
CN110900450A (en) Accurate quick flexible many heart eccentric shaft grinding fixture
CN102785064A (en) Method for processing cross axle
CN115488403A (en) Device and method for machining cross teeth of locomotive driving hollow shaft
CN115255838A (en) Manufacturing process and method of threading and rolling thread rolling wheel
CN111571132B (en) Thin-wall bearing outer ring turning method and outer ring end surface groove symmetry measuring method of thin-wall bearing
CN112589501A (en) Numerical control machine tool tail end bearing block and machining process thereof
CN114434227B (en) Boring and grinding device for improving precision of outer cylindrical surface of part by taking inner hole as reference
CN102528076A (en) Optimizing process for molding and processing oversized copper cage
CN105522209A (en) Machining method for large herringbone gear keyway
CN216681780U (en) Cup-shaped grinding wheel for grinding narrow-groove blind hole on hard and brittle material workpiece
CN212094347U (en) Lathe for machining thrust surface of camshaft
CN214722163U (en) Novel pendulum-type compressor rotor processing frock
CN114799359B (en) Gear shaping processing technology for small-size blind hole and small-modulus straight bevel gear
CN217167882U (en) Worm grinder device

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
RJ01 Rejection of invention patent application after publication

Application publication date: 20220315

RJ01 Rejection of invention patent application after publication