CN107931641A - Large-size machine engine base machining method for finely boring - Google Patents

Large-size machine engine base machining method for finely boring Download PDF

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Publication number
CN107931641A
CN107931641A CN201711144956.9A CN201711144956A CN107931641A CN 107931641 A CN107931641 A CN 107931641A CN 201711144956 A CN201711144956 A CN 201711144956A CN 107931641 A CN107931641 A CN 107931641A
Authority
CN
China
Prior art keywords
engine base
seam allowance
boring
iron core
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.)
Withdrawn
Application number
CN201711144956.9A
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Chinese (zh)
Inventor
张淑芬
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 Qiyuan Technology Development Co Ltd
Original Assignee
Shaanxi Qiyuan Technology Development 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 Qiyuan Technology Development Co Ltd filed Critical Shaanxi Qiyuan Technology Development Co Ltd
Priority to CN201711144956.9A priority Critical patent/CN107931641A/en
Publication of CN107931641A publication Critical patent/CN107931641A/en
Withdrawn legal-status Critical Current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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23BTURNING; BORING
    • B23B41/00Boring or drilling machines or devices specially adapted for particular work; Accessories specially adapted therefor

Abstract

Large-size machine engine base machining method for finely boring of the present invention is related to field of machining, and in particular to large-size machine engine base machining method for finely boring, comprises the following steps:Positioned on boring machine with high accuracy positioning tire with foot plane and footing hole, engine base both ends end face and the first seam allowance are beaten with dial gauge, second seam allowance, bounce at iron core, it is engine base centering by adjusting positioning fetal position and adjustment fine adjustment screw, ensure the first seam allowance of engine base, second seam allowance, iron core has enough processing capacities, the present invention is positioned with high-precision tire plate with foot plane and footing hole, it accurately ensure that engine base center high dimensional accuracy, and it ensure that the depth of parallelism of engine base center and foot plane, and disposable clamping can be completed to finish in production process, it can ensure the concentricity of engine base seam allowance and iron core, it ensure that bounce requirement of the end face of machine base to seam allowance, the dimensional accuracy and roughness precision of engine base is greatly improved, improve production efficiency, it is suitable for mass production.

Description

Large-size machine engine base machining method for finely boring
Technical field
The present invention relates to field of machining, and in particular to large-size machine engine base machining method for finely boring.
Background technology
The serial and other large-size machine engine base both ends end faces of Chang Feng electricity, seam allowance and iron core processing carry out on vertical lathe. By end face of machine base and inner circle it is rough turn after stay certain surplus, with smart car seam allowance tire position smart car to drawing size, then on milling machine With seam allowance tire positioning milling, bore footing etc..Its machining process is:Rough turn-smart car-milling, bore footing-plane keyway-drilling.If The serial and other large-size machine engine base of wind-powered electricity generation uses above-mentioned processing method, and since seam allowance tire positioning accuracy is poor, it is fixed to be easy to cause Position precision is not allowed, and in addition engine base shape and weight are larger, and especially overall length is too long, and clamping is difficult under engine base upright state, is stablized Property it is poor, be easy to cause turning stress distribution inequality.Therefore engine base overall dimensional accuracy and bounce precision are not easy to meet product figure Paper requirement, in addition, easily there is the forward and backward footing face tilt phenomenon of engine base when milling, brill footing.
The content of the invention
To solve the above-mentioned problems, the present invention is provided one kind and is positioned with high-precision tire plate with foot plane and footing hole, smart It really ensure that engine base center high dimensional accuracy, and ensure that the depth of parallelism of engine base center and foot plane, and production process In disposable clamping can complete to finish, it is ensured that the concentricity of engine base seam allowance and iron core, ensure that end face of machine base to seam allowance Bounce requirement, the dimensional accuracy and roughness precision of engine base is greatly improved, improves production efficiency, it is suitable for mass production Large-size machine engine base machining method for finely boring.
Large-size machine engine base machining method for finely boring of the present invention, comprises the following steps:
The first step, is positioned with foot plane and footing hole with high accuracy positioning tire on boring machine, engine base both ends end is beaten with dial gauge Face and the first seam allowance, the second seam allowance, the bounce at iron core, are looked for by adjusting positioning fetal position and adjustment fine adjustment screw for engine base Just, ensure that the first seam allowance of engine base, the second seam allowance, iron core there are enough processing capacities, then positioning tire be fixed on boring table, At platen press seat footing piece, engine base is compressed;
Second step, is wanted using at boring machine tool special boring the first seam allowance of engine base end face, the first seam allowance and iron core up to product drawing Size is sought, again clamping lathe tool turning engine base the second seam allowance end face and the second seam allowance, reach the second seam allowance diameter and engine base overall length Product drawing desired size, the first seam allowance of engine base, the second seam allowance and both ends end face need boring 2 times, boring 1 are only needed at engine base iron core It is secondary;
3rd step, by clamp loose, engine base, which is hung, goes to next procedure, and when the boring of engine base batch is processed, its positioning tire is non-dismountable, It need to continue to be fixed on boring table, until can pull down after the completion of batch machining;
4th step, during right boring engine base, only initial workpiece alignment time is slightly long, can be directly mounted at and has fixed before remaining engine base right boring Tire plate on, survey the bounce at engine base both ends end face, the first seam allowance, the second seam allowance and iron core respectively with dial gauge, pass through fine setting Screw, which slightly adjusts, can reach right boring centering required precision.
The present invention is positioned with high-precision tire plate with foot plane and footing hole, accurately ensure that the high size essence in engine base center Degree, and ensure that the depth of parallelism of engine base center and foot plane, and disposable clamping can be completed to finish in production process, It can ensure the concentricity of engine base seam allowance and iron core, ensure that bounce requirement of the end face of machine base to seam allowance, machine is greatly improved The dimensional accuracy and roughness precision of seat, improve production efficiency, suitable for mass production.
Embodiment
Large-size machine engine base machining method for finely boring of the present invention, comprises the following steps:
The first step, is positioned with foot plane and footing hole with high accuracy positioning tire on boring machine, engine base both ends end is beaten with dial gauge Face and the first seam allowance, the second seam allowance, the bounce at iron core, are looked for by adjusting positioning fetal position and adjustment fine adjustment screw for engine base Just, ensure that the first seam allowance of engine base, the second seam allowance, iron core there are enough processing capacities, then positioning tire be fixed on boring table, At platen press seat footing piece, engine base is compressed;
Second step, is wanted using at boring machine tool special boring the first seam allowance of engine base end face, the first seam allowance and iron core up to product drawing Size is sought, again clamping lathe tool turning engine base the second seam allowance end face and the second seam allowance, reach the second seam allowance diameter and engine base overall length Product drawing desired size, the first seam allowance of engine base, the second seam allowance and both ends end face need boring 2 times, boring 1 are only needed at engine base iron core It is secondary;
3rd step, by clamp loose, engine base, which is hung, goes to next procedure, and when the boring of engine base batch is processed, its positioning tire is non-dismountable, It need to continue to be fixed on boring table, until can pull down after the completion of batch machining;
4th step, during right boring engine base, only initial workpiece alignment time is slightly long, can be directly mounted at and has fixed before remaining engine base right boring Tire plate on, survey the bounce at engine base both ends end face, the first seam allowance, the second seam allowance and iron core respectively with dial gauge, pass through fine setting Screw, which slightly adjusts, can reach right boring centering required precision.
The present invention is positioned with high-precision tire plate with foot plane and footing hole, accurately ensure that the high size essence in engine base center Degree, and ensure that the depth of parallelism of engine base center and foot plane, and disposable clamping can be completed to finish in production process, It can ensure the concentricity of engine base seam allowance and iron core, ensure that bounce requirement of the end face of machine base to seam allowance, machine is greatly improved The dimensional accuracy and roughness precision of seat, improve production efficiency, suitable for mass production.

Claims (1)

1. a kind of large-size machine engine base machining method for finely boring, it is characterised in that comprise the following steps:
The first step, is positioned with foot plane and footing hole with high accuracy positioning tire on boring machine, engine base both ends end is beaten with dial gauge Face and the first seam allowance, the second seam allowance, the bounce at iron core, are looked for by adjusting positioning fetal position and adjustment fine adjustment screw for engine base Just, ensure that the first seam allowance of engine base, the second seam allowance, iron core there are enough processing capacities, then positioning tire be fixed on boring table, At platen press seat footing piece, engine base is compressed;
Second step, is wanted using at boring machine tool special boring the first seam allowance of engine base end face, the first seam allowance and iron core up to product drawing Size is sought, again clamping lathe tool turning engine base the second seam allowance end face and the second seam allowance, reach the second seam allowance diameter and engine base overall length Product drawing desired size, the first seam allowance of engine base, the second seam allowance and both ends end face need boring 2 times, boring 1 are only needed at engine base iron core It is secondary;
3rd step, by clamp loose, engine base, which is hung, goes to next procedure, and when the boring of engine base batch is processed, its positioning tire is non-dismountable, It need to continue to be fixed on boring table, until can pull down after the completion of batch machining;
4th step, during right boring engine base, initial workpiece alignment time is slightly long, and the tire plate fixed is directly installed on before remaining engine base right boring On, survey the bounce at engine base both ends end face, the first seam allowance, the second seam allowance and iron core respectively with dial gauge, by fine adjustment screw slightly Adjust and can reach right boring centering required precision.
CN201711144956.9A 2017-11-17 2017-11-17 Large-size machine engine base machining method for finely boring Withdrawn CN107931641A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711144956.9A CN107931641A (en) 2017-11-17 2017-11-17 Large-size machine engine base machining method for finely boring

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711144956.9A CN107931641A (en) 2017-11-17 2017-11-17 Large-size machine engine base machining method for finely boring

Publications (1)

Publication Number Publication Date
CN107931641A true CN107931641A (en) 2018-04-20

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201711144956.9A Withdrawn CN107931641A (en) 2017-11-17 2017-11-17 Large-size machine engine base machining method for finely boring

Country Status (1)

Country Link
CN (1) CN107931641A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108838452A (en) * 2018-09-14 2018-11-20 上海特波电机有限公司 Plane processing motor foot tooling

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108838452A (en) * 2018-09-14 2018-11-20 上海特波电机有限公司 Plane processing motor foot tooling

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Application publication date: 20180420