The prop-fan concept offers the potential for significant fuel savings without reducing aircraft performance from the levels of current turbofan aircraft. To enhance industry acceptance of the concept there is a need to accelerate current research and development activities. One method of accomplishing both industry acceptance and accelerated research and development is by means of flight research vehicles. This paper describes how flight research vehicles could be used in an advanced turboprop, or prop-fan, program. The technology status of prop-fan development will be reviewed and deficiencies will be identified. Methods for solving prop-fan problems using the test-bed aircraft philosophy will be discussed. Based on defined problem areas which must be addressed if the prop-fan is to become an accepted propulsion system, test-bed program objectives and priorities will be established, and the design requirements for a prop-fan research vehicle will be formulated. Suitable configurations will be examined and analyzed.
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ASME 1981 International Gas Turbine Conference and Products Show
March 9–12, 1981
Houston, Texas, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7961-0
PROCEEDINGS PAPER
The Role of Flight Research Vehicles in Prop-Fan Technology Development
E. S. Bradley,
E. S. Bradley
The Lockheed-Georgia Co., Marietta, GA
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B. H. Little, Jr.
B. H. Little, Jr.
The Lockheed-Georgia Co., Marietta, GA
Search for other works by this author on:
E. S. Bradley
The Lockheed-Georgia Co., Marietta, GA
B. H. Little, Jr.
The Lockheed-Georgia Co., Marietta, GA
Paper No:
81-GT-216, V001T01A016; 11 pages
Published Online:
April 15, 2015
Citation
Bradley, ES, & Little, BH, Jr. "The Role of Flight Research Vehicles in Prop-Fan Technology Development." Proceedings of the ASME 1981 International Gas Turbine Conference and Products Show. Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery. Houston, Texas, USA. March 9–12, 1981. V001T01A016. ASME. https://doi.org/10.1115/81-GT-216
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