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A Conversion of Wheatstone Bridge to Current-Loop Signal Conditioning for Strain GagesCurrent loop circuitry replaced Wheatstone bridge circuitry to signal-condition strain gage transducers in more than 350 data channels for two different test programs at NASA Dryden Flight Research Center. The uncorrected test data from current loop circuitry had a lower noise level than data from comparable Wheatstone bridge circuitry, were linear with respect to gage-resistance change, and were uninfluenced by varying lead-wire resistance. The current loop channels were easier for the technicians to set up, verify, and operate than equivalent Wheatstone bridge channels. Design choices and circuit details are presented in this paper in addition to operational experience.
Document ID
19970024858
Acquisition Source
Armstrong Flight Research Center
Document Type
Technical Memorandum (TM)
Authors
Anderson, Karl F.
(NASA Dryden Flight Research Center Edwards, CA United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1995
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
NASA-TM-104309
H-2049
NAS 1.15:104309
Meeting Information
Meeting: Strain Gage
Location: El Segundo, CA
Country: United States
Start Date: February 7, 1995
End Date: February 8, 1995
Sponsors: Society of Engineering Science
Accession Number
97N24573
Funding Number(s)
PROJECT: RTOP 505-70-XX
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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