This paper describes the procedure developed by Cooper-Bessemer for large-bore gas engines to calculate the knock rating of gas fuel blends and to predict with accuracy the required engine build to use that fuel with optimum detonation margin. Engine prototype test work has included fuel sensitivity tests mapped as a function of compression ratio, fuel air ratio, ignition advance, combustion air temperature, and engine rating. Success in predicting production engine operation for a given application involving a particular fuel blend has been gratifying. The basic reference method blend selected was normal butane in methane. Details are included in the paper to illustrate the problems in making sensitivity correlations between small-bore fuel research engines and large-bore production engines.
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October 1985
Research Papers
A Procedure for Calculating Fuel Gas Blend Knock Rating for Large-Bore Gas Engines and Predicting Engine Operation
F. S. Schaub,
F. S. Schaub
Research and Development, Energy Services Group of Cooper Industries, Research and Development Laboratory, Mount Vernon, OH 43050
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R. L. Hubbard
R. L. Hubbard
Research and Development, Energy Services Group of Cooper Industries, Research and Development Laboratory, Mount Vernon, OH 43050
Search for other works by this author on:
F. S. Schaub
Research and Development, Energy Services Group of Cooper Industries, Research and Development Laboratory, Mount Vernon, OH 43050
R. L. Hubbard
Research and Development, Energy Services Group of Cooper Industries, Research and Development Laboratory, Mount Vernon, OH 43050
J. Eng. Gas Turbines Power. Oct 1985, 107(4): 922-930 (9 pages)
Published Online: October 1, 1985
Article history
Received:
November 12, 1984
Online:
October 15, 2009
Citation
Schaub, F. S., and Hubbard, R. L. (October 1, 1985). "A Procedure for Calculating Fuel Gas Blend Knock Rating for Large-Bore Gas Engines and Predicting Engine Operation." ASME. J. Eng. Gas Turbines Power. October 1985; 107(4): 922–930. https://doi.org/10.1115/1.3239837
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