CN106735384A - Rotor of steam turbo generator shaft coupling is to group using pin-and-hole processing method - Google Patents

Rotor of steam turbo generator shaft coupling is to group using pin-and-hole processing method Download PDF

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Publication number
CN106735384A
CN106735384A CN201611014264.8A CN201611014264A CN106735384A CN 106735384 A CN106735384 A CN 106735384A CN 201611014264 A CN201611014264 A CN 201611014264A CN 106735384 A CN106735384 A CN 106735384A
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CN
China
Prior art keywords
hole
pin
boring
shaft coupling
measurement
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
CN201611014264.8A
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Chinese (zh)
Inventor
刘秋丽
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.)
Shaanxi Gaohua Zhiben Chemical Technology Co Ltd
Original Assignee
Shaanxi Gaohua Zhiben Chemical Technology 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 Shaanxi Gaohua Zhiben Chemical Technology Co Ltd filed Critical Shaanxi Gaohua Zhiben Chemical Technology Co Ltd
Priority to CN201611014264.8A priority Critical patent/CN106735384A/en
Publication of CN106735384A publication Critical patent/CN106735384A/en
Pending legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23BTURNING; BORING
    • B23B35/00Methods 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

Abstract

Rotor of steam turbo generator shaft coupling of the present invention is related to field of machining to group pin-and-hole processing method, and in particular to rotor of steam turbo generator shaft coupling is comprised the following steps to group using pin-and-hole processing method:Heavy boring, by each pin-and-hole elder generation's heavy boring to desired size;Half right boring, carries out once half right boring, and diameter tolerance control is within 0.05mm after each pin hole boring;Measurement position degree, measures each pin-and-hole to beeline, pin-and-hole internal diameter between shaft coupling seam, each pin-and-hole, records measured value;Amendment, according to measurement data, global analysis pin-and-hole offsets relative to the position of seam, adjusts coordinate, then carry out a right boring, mono- section of 30 40mm is bored in each pin-and-hole leading portion, the present invention is simple to operate, easy to process, and can guarantee that the crudy and machining accuracy of workpiece, improve production efficiency, reduces production cost.

Description

Rotor of steam turbo generator shaft coupling is to group using pin-and-hole processing method
Technical field
The present invention relates to field of machining, and in particular to rotor of steam turbo generator shaft coupling is to group pin-and-hole processing side Method.
Background technology
Have on rotor of steam turbo generator shaft coupling one group with turbine rotor to group pin-and-hole, by pin-and-hole load join Connecting bolt is by generator amature and turbine rotor to group, conjunction.To ensure smooth, the essence of generator amature and turbine rotor Really assemble, the dimensional tolerance, position degree and surface roughness to pin-and-hole have all done strict requirements, this group of diameter of pin-and-hole is public Difference is general within according to 0.05mm, position degree within 0.05-0.10mm, surface roughness Ra more than 1.6.
To ensure the machining accuracy of pin-and-hole, the conventional machining process of specific purpose tool drill jig is had been used up in the past.In recent years, respectively Generator manufacturing firm needs not turning off the new product for sending different size in a short time, to adapt to market needs.New product Rotor coupling pin-and-hole size is different, needs to obtain through refining various sizes of drill jig if using traditional handicraft.Because of drill jig manufacture Cycle is long, and manufacturing expense is higher, certainly will take the generator product entirety manufacturing cycle, and improves cost of goods manufactured, special Be not the product urgent for some durations, the design and manufacture of drill jig can even turn into one of restriction manufacturing schedule it is unfavorable because Element.
The content of the invention
In order to solve the above problems, the present invention provides a kind of simple to operate, easy to process, and can guarantee that the processing matter of workpiece Amount and machining accuracy, improve production efficiency reduce the rotor of steam turbo generator shaft coupling of production cost to group pin-and-hole processing side Method.
Rotor of steam turbo generator shaft coupling of the present invention is comprised the following steps to group using pin-and-hole processing method:
The first step, heavy boring, by each pin-and-hole elder generation's heavy boring to desired size;
Second step, half right boring carries out once half right boring, and diameter tolerance control is within 0.05mm after each pin hole boring;
3rd step, measurement position degree measures each pin-and-hole to beeline, pin-and-hole internal diameter between shaft coupling seam, each pin-and-hole, record Measured value;
4th step, amendment, according to measurement data, global analysis pin-and-hole offsets relative to the position of seam, adjusts coordinate, then carry out one Secondary right boring, mono- section of 30-40mm is bored in each pin-and-hole leading portion, can meet the measurement of inside micrometer, and each hole is measured again to only Mouthful, between each hole, the internal diameter of hole, whether the coordinate after checking adjustment adjustment accurate, it is such as not all right adjust again, measurement, until each measurement Numerical value meets position degree requirement, i.e., each hole internal diameter dimensional discrepancy within 0.05mm, beeline, each pin between each pin-and-hole Hole to shaft coupling seam deviation within 0.05mm;
5th step, right boring:Complete last right boring;
6th step, checks, after right boring completion, more than measurement each numerical value, judges that position degree, pin-and-hole internal diameter size are qualified again Afterwards, record data.
The present invention is simple to operate, easy to process, and can guarantee that the crudy and machining accuracy of workpiece, improves production effect Rate, reduces production cost.
Specific embodiment
Rotor of steam turbo generator shaft coupling of the present invention is comprised the following steps to group using pin-and-hole processing method:
The first step, heavy boring, by each pin-and-hole elder generation's heavy boring to desired size;
Second step, half right boring carries out once half right boring, and diameter tolerance control is within 0.05mm after each pin hole boring;
3rd step, measurement position degree measures each pin-and-hole to beeline, pin-and-hole internal diameter between shaft coupling seam, each pin-and-hole, record Measured value;
4th step, amendment, according to measurement data, global analysis pin-and-hole offsets relative to the position of seam, adjusts coordinate, then carry out one Secondary right boring, mono- section of 30-40mm is bored in each pin-and-hole leading portion, can meet the measurement of inside micrometer, and each hole is measured again to only Mouthful, between each hole, the internal diameter of hole, whether the coordinate after checking adjustment adjustment accurate, it is such as not all right adjust again, measurement, until each measurement Numerical value meets position degree requirement, i.e., each hole internal diameter dimensional discrepancy within 0.05mm, beeline, each pin between each pin-and-hole Hole to shaft coupling seam deviation within 0.05mm;
5th step, right boring:Complete last right boring;
6th step, checks, after right boring completion, more than measurement each numerical value, judges that position degree, pin-and-hole internal diameter size are qualified again Afterwards, record data.
The present invention is simple to operate, easy to process, and can guarantee that the crudy and machining accuracy of workpiece, improves production effect Rate, reduces production cost.

Claims (1)

1. a kind of rotor of steam turbo generator shaft coupling is to group using pin-and-hole processing method, it is characterised in that comprise the following steps:
The first step, heavy boring, by each pin-and-hole elder generation's heavy boring to desired size;
Second step, half right boring carries out once half right boring, and diameter tolerance control is within 0.05mm after each pin hole boring;
3rd step, measurement position degree measures each pin-and-hole to beeline, pin-and-hole internal diameter between shaft coupling seam, each pin-and-hole, record Measured value;
4th step, amendment, according to measurement data, global analysis pin-and-hole offsets relative to the position of seam, adjusts coordinate, then carry out one Secondary right boring, mono- section of 30-40mm is bored in each pin-and-hole leading portion, can meet the measurement of inside micrometer, and each hole is measured again to only Mouthful, between each hole, the internal diameter of hole, whether the coordinate after checking adjustment adjustment accurate, it is such as not all right adjust again, measurement, until each measurement Numerical value meets position degree requirement, i.e., each hole internal diameter dimensional discrepancy within 0.05mm, beeline, each pin between each pin-and-hole Hole to shaft coupling seam deviation within 0.05mm;
5th step, right boring:Complete last right boring;
6th step, checks, after right boring completion, more than measurement each numerical value, judges that position degree, pin-and-hole internal diameter size are qualified again Afterwards, record data.
CN201611014264.8A 2016-11-18 2016-11-18 Rotor of steam turbo generator shaft coupling is to group using pin-and-hole processing method Pending CN106735384A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201611014264.8A CN106735384A (en) 2016-11-18 2016-11-18 Rotor of steam turbo generator shaft coupling is to group using pin-and-hole processing method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611014264.8A CN106735384A (en) 2016-11-18 2016-11-18 Rotor of steam turbo generator shaft coupling is to group using pin-and-hole processing method

Publications (1)

Publication Number Publication Date
CN106735384A true CN106735384A (en) 2017-05-31

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201611014264.8A Pending CN106735384A (en) 2016-11-18 2016-11-18 Rotor of steam turbo generator shaft coupling is to group using pin-and-hole processing method

Country Status (1)

Country Link
CN (1) CN106735384A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111842975A (en) * 2020-07-30 2020-10-30 哈尔滨电机厂有限责任公司 Method for machining connecting pin hole of steam end coupler of rotor of large steam turbine generator
CN113102804A (en) * 2021-04-07 2021-07-13 常州宝菱重工机械有限公司 Method for setting dislocation machining hole on reference positioning point

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111842975A (en) * 2020-07-30 2020-10-30 哈尔滨电机厂有限责任公司 Method for machining connecting pin hole of steam end coupler of rotor of large steam turbine generator
CN111842975B (en) * 2020-07-30 2022-09-02 哈尔滨电机厂有限责任公司 Method for machining connecting pin hole of steam end coupler of rotor of large steam turbine generator
CN113102804A (en) * 2021-04-07 2021-07-13 常州宝菱重工机械有限公司 Method for setting dislocation machining hole on reference positioning point
CN113102804B (en) * 2021-04-07 2022-05-17 常州宝菱重工机械有限公司 Method for setting dislocation machining hole on reference positioning point

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Application publication date: 20170531

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