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A Mechanism for Precise Linear and Angular Adjustment Utilizing FlexuresThis paper describes the design and development of a mechanism for precise linear and angular adjustment. This work was in support of the development of a mechanical extensometer for biaxial strain measurement. A compact mechanism was required which would allow angular adjustments about perpendicular axes with better than 10(exp -3) degree resolution. The approach adopted was first to develop a means of precise linear adjustment. To this end, a mechanism based on the toggle principle was built with inexpensive and easily manufactured parts. A detailed evaluation showed that the resolution of the mechanism was better than 1 micron and that adjustments made by using the device were repeatable. In the second stage of this work, the linear adjustment mechanisms were used in conjunction with a simple arrangement of flexural pivots and attachment blocks to provide the required angular adjustments. A series of experiments conducted with an autocollimator showed that the resolution of the mechanisms was better than 10(exp -3) degrees. Also, the mechanism met all requirements regarding size, weight, and mechanical simplicity. Attempts to use the mechanism in conjunction with the biaxial extensometer under development proved unsuccessful. Any form of in situ adjustment was found to cause erratic changes in instrument output. These changes were due to problems with the suspension system. However, the subject mechanism performed well in its own right and appeared to have potential for use in other applications. One important advantage of flexure based mechanisms is that they can be designed to operate independently of screw threads. This raises the possibility that they can be used for precise linear and angular adjustment in a space environment.
Document ID
20020073842
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ellis, J. R.
(Akron Univ. Akron, OH United States)
Date Acquired
August 20, 2013
Publication Date
May 1, 1986
Publication Information
Publication: 20th Aerospace Mechanisms Symposium
Subject Category
Mechanical Engineering
Funding Number(s)
CONTRACT_GRANT: N-7405-eng-26
CONTRACT_GRANT: NAG3-379
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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