NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
High Accuracy Temperature Measurements Using RTDs with Current Loop ConditioningTo measure temperatures with a greater degree of accuracy than is possible with thermocouples, RTDs (Resistive Temperature Detectors) are typically used. Calibration standards use specialized high precision RTD probes with accuracies approaching 0.001 F. These are extremely delicate devices, and far too costly to be used in test facility instrumentation. Less costly sensors which are designed for aeronautical wind tunnel testing are available and can be readily adapted to probes, rakes, and test rigs. With proper signal conditioning of the sensor, temperature accuracies of 0.1 F is obtainable. For reasons that will be explored in this paper, the Anderson current loop is the preferred method used for signal conditioning. This scheme has been used in NASA Lewis Research Center's 9 x 15 Low Speed Wind Tunnel, and is detailed.
Document ID
19970017434
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hill, Gerald M.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1997
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
NASA-TM-107416
E-10653
NAS 1.15:107416
Report Number: NASA-TM-107416
Report Number: E-10653
Report Number: NAS 1.15:107416
Meeting Information
Meeting: International Instrumentation Symposium
Location: Orlando, Florida
Country: United States
Start Date: May 4, 1997
End Date: May 8, 1997
Sponsors: Instrument Society of America
Accession Number
97N19696
Funding Number(s)
PROJECT: RTOP 523-91-93
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available