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Development of A Precision, Six-Axis Laboratory DynamometerThis paper describes the design, fabrication, test, and operation of a unique six axis force/torque dynamometer The specimen table used to hold components under test is supported in a full six axis kinematic mount. Support struts fabricated from high strength steel with special integral two axis flexures link the specimen table to the load cell transducers. Realtime force/torque coordinate transform, root mean squared calculation, and data averaging, and color six axis display with controllable scaling are provided by a specially programmed desktop computer. The extensive structural analysis and design optimization required to obtain a stiff, well damped, lightweight structure is described in detail. Geometric optimization of the kinematic mount and fabrication details of the struts are also described.
Document ID
19920015846
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
P. J. Champagne
(Lockheed Missiles and Space Company (United States) Sunnyvale, United States)
S. A. Cordova
(Lockheed Missiles and Space Company (United States) Sunnyvale, United States)
M. S. Jacoby
(Lockheed Missiles and Space Company (United States) Sunnyvale, United States)
K. R. Lorell
(Lockheed Missiles and Space Company (United States) Sunnyvale, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1992
Publication Information
Publication: NASA. Goddard Space Flight Center, The 26th Aerospace Mechanisms Symposium
Subject Category
Instrumentation And Photography
Meeting Information
Meeting: The 26th Aerospace Mechanisms Symposium
Location: Greenbelt, MD
Country: US
Start Date: May 13, 1992
End Date: May 13, 1992
Sponsors: National Aeronautics and Space Administration
Accession Number
92N25089
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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