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.
Skip Nav Destination
Article navigation
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
Search for other works by this author on:
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
Download citation file:
Get Email Alerts
Cited By
How Do Interfacial Shear and Gravity Affect the Oil Film Characteristics Near an Aero-Engine Bearing?
J. Eng. Gas Turbines Power
System Parameter Identification of a Colored-Noise-Driven Rijke Tube Simulator
J. Eng. Gas Turbines Power
Gas Turbine Compressor Washing Economics and Optimisation Using Genetic Algorithm
J. Eng. Gas Turbines Power
Related Articles
Factors Determining Antiknocking Properties of Gaseous Fuels in Spark-Ignition Gas Engines
J. Eng. Gas Turbines Power (October,2016)
Characteristics of Auto-Ignition in Internal Combustion Engines Operated With Gaseous Fuels of Variable Methane Number
J. Energy Resour. Technol (July,2017)
Homogeneous Charge Compression Ignition Operation With Natural Gas: Fuel Composition Implications
J. Eng. Gas Turbines Power (July,2003)
The Operational Mixture Limits in Engines Fueled With Alternative Gaseous Fuels
J. Energy Resour. Technol (September,2006)
Related Chapters
The Impact of Plant Economics on the Design of Industrial Energy Systems
Industrial Energy Systems
Historical Development of the Windmill
Wind Turbine Technology: Fundamental Concepts in Wind Turbine Engineering, Second Edition
Lay-Up and Start-Up Practices
Consensus on Operating Practices for Control of Water and Steam Chemistry in Combined Cycle and Cogeneration