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Calibration Systems and Turbine-Type Flow Transducers for Cryogenic Flow Measurements

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Advances in Cryogenic Engineering

Part of the book series: Advances in Cryogenic Engineering ((ACRE,volume 8))

Abstract

In rocket engine development, it is not unusual to require accuracies or precisions beyond the capabilities of existing measurement techniques. This need for improved measurements has been the underlying motive for the development of various cryogenic flow calibration systems. This paper will discuss the Pratt’& Whitney Aircraft liquid-hydrogen and liquid-oxygen flow calibration systems and will review performance characteristics of the turbine-type flowmeters that have been tested.

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References

  1. J. W. Ladd, Advances in Cryogenic Engineering, Vol. 6, K. D. Timmerhaus (ed.), Plenum Press, New York (1961), p. 388.

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  2. R. B. Scott, NBS Report No. 6752 (March 8, 1961).

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  3. H. M. Roder and Robert D. Goodwin, “Provisional Thermodynamic Functions for Para-hydrogen,”: NBS Technical Note 130 (December 1961).

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  4. J. Grey, “The Turbine Flowmeter for Cryogenic Liquids,” ISA Preprint 111–59 (September 1959).

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  5. M. R. Shafer and F. W. Ruegg, Trans. ASME, Vol. 80, 1369 (1958).

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  6. M. R. Shafer, “Performance Characteristics of Turbine Flowmeters,” ASME Paper No. 61-WA-25 (1961).

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  7. J. A. Brennan, W. A. Wilson, R. Radebaugh, and B. W. Birmingham, “Testing of Ball Bearings with Five Different Separator Materials at 9200 RPM in Liquid Nitrogen,” ASME Paper No. 61-LUBS-18 (1961).

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© 1963 Springer Science+Business Media New York

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Bucknell, R.L. (1963). Calibration Systems and Turbine-Type Flow Transducers for Cryogenic Flow Measurements. In: Timmerhaus, K.D. (eds) Advances in Cryogenic Engineering. Advances in Cryogenic Engineering, vol 8. Springer, Boston, MA. https://doi.org/10.1007/978-1-4757-0528-7_43

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  • DOI: https://doi.org/10.1007/978-1-4757-0528-7_43

  • Publisher Name: Springer, Boston, MA

  • Print ISBN: 978-1-4757-0530-0

  • Online ISBN: 978-1-4757-0528-7

  • eBook Packages: Springer Book Archive

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