CN1676247A - Method for processing magnesium alloy scurf using lathe - Google Patents

Method for processing magnesium alloy scurf using lathe Download PDF

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Publication number
CN1676247A
CN1676247A CN 200510009871 CN200510009871A CN1676247A CN 1676247 A CN1676247 A CN 1676247A CN 200510009871 CN200510009871 CN 200510009871 CN 200510009871 A CN200510009871 A CN 200510009871A CN 1676247 A CN1676247 A CN 1676247A
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CN
China
Prior art keywords
magnesium alloy
lathe
scurf
bar
alloy scurf
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
CN 200510009871
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Chinese (zh)
Inventor
吉泽升
洪艳
赵密
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Harbin University of Science and Technology
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Harbin University of Science and Technology
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 Harbin University of Science and Technology filed Critical Harbin University of Science and Technology
Priority to CN 200510009871 priority Critical patent/CN1676247A/en
Publication of CN1676247A publication Critical patent/CN1676247A/en
Pending legal-status Critical Current

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Abstract

The present invention provides a method for processing magnesium alloy filings by utilizing turning machine. Said invention adopts triangular tool blade to cut the magnesium alloy rod on the turning machine. Its operation is simple, and its processing cost is low.

Description

A kind of method of utilizing the machined into magnesium alloy scurf
Technical field:
The present invention relates to the method for metal material field of machining, particularly a kind of processing magnesium alloy scurf.
Background technology:
Advantages such as magnesium alloy is little owing to its density, specific strength is high, processing characteristics is superior, it is used more and more widely.The forming technique of magnesium alloy roughly has compression casting, extrusion modling, semisolid moulding.Wherein the semisolid moulding is divided into rheocasting, thixotroping casting and thixotropic injection moulding, wherein the raw material of thixotropic injection make-up machine needs is the magnesium alloy scurf (grain) of 3~6mm, at present, on the market magnesium alloy scurf that is specifically applied to the thixotropic injection make-up machine is arranged seldom at home; Magnesium alloy scurf in the market, powder are mainly pulverized by pulverizer and are made then, its size all is as unit with order, and particle and powder are processed into by milling machine, and there is complex procedures in this processing method, be not easy operation, processing cost height and gained magnesium closes the big or small uppity drawback of bits.
Summary of the invention:
There is drawback not easy to operate, that cost is high at existing in the present invention by the milling machine processing magnesium alloy scurf, thereby provide a kind of technology to operate and can conveniently control the method for utilizing the machined into magnesium alloy scurf of magnesium alloy scurf size simply, easily, magnesium alloy bar is carried out machining on lathe, lathe adopts triangular blade that magnesium alloy bar is cut.Utilize the method for the invention cutting magnesium alloy scurf to have advantage simple to operate, that processing cost is low, can realize, be convenient to the application of existing equipment, and utilize lathe to carry out processing magnesium alloy scurf to make tool wear little, be beneficial to and apply at engine lathe.
The specific embodiment:
The specific embodiment one: present embodiment is, magnesium alloy bar is carried out machining on lathe, lathe adopts triangular blade that magnesium alloy bar is cut, in the working angles, control lathe rotating speed is 400-560 rev/min, the diameter of selecting magnesium alloy bar for use is 50~200mm, and length is 200~700mm.
The specific embodiment two: model is cut into bulk for the AZ91D magnesium alloy ingot adopts anodontia torch, in the protective atmosphere smelting furnace, melt, pour into the magnesium alloy bar of diameter 100mm, length 500mm, magnesium alloy bar one end is clamped on the machine chuck, the other end withstands with tailstock tool is top; Then model is contained on the right avertence cutter lathe tool knife bar for the 31303c5 triangular blade, adopts the CA6140 lathe to process; Regulate the lathe parameter, 420 rev/mins of control lathe rotating speeds, feed 0.2mm, cutter groove width 5mm, cutting-in a p=3mm.Size by above processing method gained magnesium alloy scurf is as follows after tested: long 5mm, wide 3mm, thickness 0.2mm.
The specific embodiment three: model is cut into bulk for the AM60B magnesium alloy ingot adopts anodontia torch, in the protective atmosphere smelting furnace, melt, pour into the magnesium alloy bar of diameter 60mm, length 250mm, magnesium alloy bar one end is clamped on the machine chuck, the other end withstands with tailstock tool is top; Then model is contained on the right avertence cutter lathe tool knife bar for the 31003c triangular blade, adopts the CA6140 lathe to process; Regulate the lathe parameter, 450 rev/mins of control lathe rotating speeds, feed 0.5mm, cutter groove width 2.4mm, cutting-in a p=4mm.Size by above processing method gained magnesium alloy scurf is as follows after tested: long 4mm, wide 2.4mm, thickness 0.5mm.
The specific embodiment four: model is cut into bulk for the AM20 magnesium alloy ingot adopts anodontia torch, in the protective atmosphere smelting furnace, melt, pour into the magnesium alloy bar of diameter 180mm, length 650mm, magnesium alloy bar one end is clamped on the machine chuck, the other end withstands with tailstock tool is top; Then model is contained on the right avertence cutter lathe tool knife bar for the 31303c triangular blade, adopts the CA6140 lathe to process; Regulate the lathe parameter, 500 rev/mins of control lathe rotating speeds, feed 0.3mm, cutter groove width 3.4mm, cutting-in a p=3mm.Size by above processing method gained magnesium alloy scurf is as follows after tested: long 5mm, wide 3mm, thickness 0.3mm.
The specific embodiment five: model is cut into bulk for the AS21 magnesium alloy ingot adopts anodontia torch, in the protective atmosphere smelting furnace, melt, pour into the magnesium alloy bar of diameter 140mm, length 400mm, magnesium alloy bar one end is clamped on the machine chuck, the other end withstands with tailstock tool is top; Then model is contained on the left avertence cutter lathe tool knife bar for the 31303c5 triangular blade, adopts the CA6140 lathe to process; Regulate the lathe parameter, 540 rev/mins of control lathe rotating speeds, feed 0.2mm, cutter groove width 5mm, cutting-in a p=4mm.Size by above processing method gained magnesium alloy scurf is as follows after tested: long 5mm, wide 4mm, thickness 0.2mm.
The specific embodiment six: model is cut into bulk for the AE42 magnesium alloy ingot adopts anodontia torch, in the protective atmosphere smelting furnace, melt, pour into the magnesium alloy bar of diameter 200mm, length 700mm, magnesium alloy bar one end is clamped on the machine chuck, the other end withstands with tailstock tool is top; Be that 31603c6 or 31905c triangular blade are contained on the left avertence cutter lathe tool knife bar then with model, adopt the CA6140 lathe to process; Regulate the lathe parameter, 450 rev/mins of control lathe rotating speeds, feed 0.2mm, cutter groove width 6.0 or 5.4mm, cutting-in a p=4mm.Size by above processing method gained magnesium alloy scurf is as follows after tested: length 6.0 or 5.4mm, wide 3.5mm, thickness 0.3mm.
The concrete model of used triangular blade is as follows among the present invention:
Model TYpe Basic size Dimension (mm)
Right Right Left side Left Blade inscribed circle (φ D) Tol. Blade thickness (C) ± 0.13 Blade endoporus (φ d) ± 0.13 Cutter groove width (α) ≈
????31003C ????31003CZ ?10±0.08 ????4.5 ???4.2 2.4
????31303C ????31303CZ ?13±0.13 ????5.5 ???5.2 3.4
????31303C5 ????31303C5Z ?13±0.13 ????5.5 ???5.2 5.0
????31603C ????31603CZ ?16±0.18 ????7.0 ???6.2 4.4
????31603C6 ????31603C6Z ?16±0.18 ????7.0 ???6.2 6.0
????31905C ????31905CZ ?19±0.18 ????8.5 ???7.2 5.4
In addition, can also make the magnesium alloy scurf of plurality of specifications by adjusting feed and cutting-in, this kind magnesium alloy scurf is mainly used in the moulding of magnesium alloy semi solid state thixotropic injection.

Claims (3)

1, a kind of method of utilizing the machined into magnesium alloy scurf is characterized in that magnesium alloy bar is carried out machining on lathe, and lathe adopts triangular blade that magnesium alloy bar is cut.
2, a kind of method of utilizing the machined into magnesium alloy scurf according to claim 1, it is characterized in that controlling the lathe rotating speed is 400-560 rev/min.
3, a kind of method of utilizing the machined into magnesium alloy scurf according to claim 1 and 2 is characterized in that selecting the diameter of magnesium alloy bar for use is 50~200mm, and length is 200~700mm.
CN 200510009871 2005-03-31 2005-03-31 Method for processing magnesium alloy scurf using lathe Pending CN1676247A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 200510009871 CN1676247A (en) 2005-03-31 2005-03-31 Method for processing magnesium alloy scurf using lathe

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 200510009871 CN1676247A (en) 2005-03-31 2005-03-31 Method for processing magnesium alloy scurf using lathe

Publications (1)

Publication Number Publication Date
CN1676247A true CN1676247A (en) 2005-10-05

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN 200510009871 Pending CN1676247A (en) 2005-03-31 2005-03-31 Method for processing magnesium alloy scurf using lathe

Country Status (1)

Country Link
CN (1) CN1676247A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101484262B (en) * 2006-05-03 2012-05-30 普渡研究基金会 Method of producing nanocrystalline chips
CN103184419A (en) * 2013-03-19 2013-07-03 昆山海普电子材料有限公司 Production method of aluminum-neodymium alloy target material

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101484262B (en) * 2006-05-03 2012-05-30 普渡研究基金会 Method of producing nanocrystalline chips
CN103184419A (en) * 2013-03-19 2013-07-03 昆山海普电子材料有限公司 Production method of aluminum-neodymium alloy target material
CN103184419B (en) * 2013-03-19 2015-04-29 昆山海普电子材料有限公司 Production method of aluminum-neodymium alloy target material

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