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Performance tests of a gas blending system based on mass-flow controllersThe system provides many of the gas mixtures required for calibrating analytical instruments used in engine exhaust gas analysis and is capable of blending from one to four additive gases with either of two carrier gases in concentrations from 20 ppm to 50%. Two mixtures can be flowing simultaneously. Performance tests were made to determine the stability accuracy of the system while it was in limited use for a period of 2 years. The accuracy of the blender was measured by comparing binary mixtures from the blender with National Bureau of Standards standard reference materials. Analytical instruments were used to make these comparisons. The expected accuracy of 2% was obtained in some of the tests, by the majority showed a systematic biAs of -5%. Although these tests revealed subtle instabilities in the flow controllers that contributed to the random scatter of data, the accuracy of wet test meters and bubble flowmeters used for calibration is marginal for this purpose. A simple procedure is recommended that should enable the full potential of the system to be realized.
Document ID
19810020708
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Evans, A., Jr.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1981
Subject Category
Propellants And Fuels
Report/Patent Number
NASA-TP-1896
E-629
Accession Number
81N29246
Funding Number(s)
PROJECT: RTOP 505-32-82
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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