Titanium alloys such as A-110AT, B-120VCA, C-120AV, and 6-6-2AVT, which have been used to manufacture structural components for the aerospace industry, are difficult to machine when compared to aluminum and even some steel alloys. Tool wear for high-speed tool steel and carbide cutters takes place rapidly, necessitating the use of low cutting speeds and feeds to obtain a reasonable cutter life. In this study, the means used toward achieving an objective of increased producibility and reduced costs for titanium alloys was through an intensive machinability investigation of the machining characteristics. Control of pertinent machining variables, such as cutting speed, feed rate, tool material, tool geometry, machine tool setup, and cutting fluid, was rigorously maintained. Comparative cost analyses of the actual cutting operation and the attendant cutting tool costs were made concurrently with the study to obtain conditions which provided the best metal removal rate with reasonable cutter life at the lowest cost.
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February 1966
This article was originally published in
Journal of Engineering for Industry
Research Papers
Modern Metals Machining Technology
Robert L. Vaughn
Robert L. Vaughn
Producibility Methods, Lockheed-California Company, A Division of Lockheed Aircraft Corporation, Burbank, Calif.
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Robert L. Vaughn
Producibility Methods, Lockheed-California Company, A Division of Lockheed Aircraft Corporation, Burbank, Calif.
J. Eng. Ind. Feb 1966, 88(1): 65-71
Published Online: February 1, 1966
Article history
Received:
March 8, 1965
Online:
December 8, 2011
Citation
Vaughn, R. L. (February 1, 1966). "Modern Metals Machining Technology." ASME. J. Eng. Ind. February 1966; 88(1): 65–71. https://doi.org/10.1115/1.3670894
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