This paper describes a new software approach to the preliminary design of aircraft engine turbines. A hybrid artificial intelligence and numerical-optimization-based design shell called Engineous was used to capture some basic turbine preliminary design knowledge, manipulate turbine design parameters, execute a turbine performance prediction program and its preprocessors, and analyze results. Engineous automatically supplements incomplete human design knowledge with symbolic and numerical search techniques when needed. This approach produced designs with higher predicted performance gains than the existing manual design process in a tenth of the turnaround time and has yielded new insights into turbine design. A comparison of turbine designs obtained by designers and by Engineous is presented here along with an overview of Engineous system architecture.
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January 1992
Research Papers
Turbine Preliminary Design Using Artificial Intelligence and Numerical Optimization Techniques
S. S. Tong,
S. S. Tong
Corporate Research and Development, General Electric Company, Schenectady, NY 12301
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B. A. Gregory
B. A. Gregory
GE Aircraft Engine, Cincinnati, OH 45215
Search for other works by this author on:
S. S. Tong
Corporate Research and Development, General Electric Company, Schenectady, NY 12301
B. A. Gregory
GE Aircraft Engine, Cincinnati, OH 45215
J. Turbomach. Jan 1992, 114(1): 1-7 (7 pages)
Published Online: January 1, 1992
Article history
Received:
January 16, 1990
Online:
June 9, 2008
Citation
Tong, S. S., and Gregory, B. A. (January 1, 1992). "Turbine Preliminary Design Using Artificial Intelligence and Numerical Optimization Techniques." ASME. J. Turbomach. January 1992; 114(1): 1–7. https://doi.org/10.1115/1.2927986
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