Mechanical Engineering ETDs

Author

Holt J. Gay

Publication Date

5-28-1957

Abstract

There has been an increasing need for a better steel insert or bushing between aluminum and steel bolts in the last few years with the rapid growth of the aircraft and missile industries. The steel insert or bushing threaded internally and externally, by increasing the area of contact with the aluminum raises the strength of the bolt fastening combination approximately 300 per cent or causes a 125,000 PSI bolt to fail rather than 40,000 PSI aluminum to fail. In addition, galling and seizing are practically eliminated. A bolt installed and removed just a few times in aluminum is likely to tear out the aluminum thread due to the inherent gulling and seizing tendency.

Degree Name

Mechanical Engineering

Level of Degree

Masters

Department Name

Mechanical Engineering

First Committee Member (Chair)

C.T. Grace

Second Committee Member

R.C. Dove

Third Committee Member

R.D. Ford

Document Type

Thesis

Language

English

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