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Fluidic hydrogen detector production prototype developmentA hydrogen gas sensor that can replace catalytic combustion sensors used to detect leaks in the liquid hydrogen transfer systems at Kennedy Space Center was developed. A fluidic sensor concept, based on the principle that the frequency of a fluidic oscillator is proportional to the square root of the molecular weight of its operating fluid, was utilized. To minimize sensitivity to pressure and temperature fluctuations, and to make the sensor specific for hydrogen, two oscillators are used. One oscillator operates on sample gas containing hydrogen, while the other operates on sample gas with the hydrogen converted to steam. The conversion is accomplished with a small catalytic converter. The frequency difference is taken, and the hydrogen concentration computed with a simple digital processing circuit. The output from the sensor is an analog signal proportional to hydrogen content. The sensor is shown to be accurate and insensitive to severe environmental disturbances. It is also specific for hydrogen, even with large helium concentrations in the sample gas.
Document ID
19760026387
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Roe, G. W.
(McDonnell-Douglas Astronautics Co. Titusville, FL, United States)
Wright, R. E.
(McDonnell-Douglas Astronautics Co. Titusville, FL, United States)
Date Acquired
September 3, 2013
Publication Date
April 16, 1976
Subject Category
Instrumentation And Photography
Report/Patent Number
L0341
NASA-CR-147984
Report Number: L0341
Report Number: NASA-CR-147984
Accession Number
76N33475
Funding Number(s)
CONTRACT_GRANT: NAS10-8764
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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