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  • 1
    Publication Date: 2016-06-07
    Description: In order to improve the design procedure of constant-torque springs used in aerospace applications, several new analysis techniques have been developed. These techniques make it possible to accurately construct a torque-rotation curve for any general constant-torque spring configuration. These new techniques allow for friction in the system to be included in the analysis, an area of analysis that has heretofore been unexplored. The new analysis techniques also include solutions for the deflected shape of the spring as well as solutions for drum and roller support reaction forces. A design procedure incorporating these new capabilities is presented.
    Keywords: Mechanical Engineering
    Type: 30th Aerospace Mechanisms Symposium; 205-220; NASA-CP-3328
    Format: application/pdf
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