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Study of research and development requirements of small gas-turbine combustorsA survey is presented of the major small-engine manufacturers and governmental users. A consensus was undertaken regarding small-combustor requirements. The results presented are based on an evaluation of the information obtained in the course of the study. The current status of small-combustor technology is reviewed. The principal problems lie in liner cooling, fuel injection, part-power performance, and ignition. Projections of future engine requirements and their effect on the combustor are discussed. The major changes anticipated are significant increases in operating pressure and temperature levels and greater capability of using heavier alternative fuels. All aspects of combustor design are affected, but the principal impact is on liner durability. An R&D plan which addresses the critical combustor needs is described. The plan consists of 15 recommended programs for achieving necessary advances in the areas of liner thermal design, primary-zone performance, fuel injection, dilution, analytical modeling, and alternative-fuel utilization.
Document ID
19800009776
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Demetri, E. P.
(Little (Arthur D.), Inc. Cambridge, MA, United States)
Topping, R. F.
(Little (Arthur D.), Inc. Cambridge, MA, United States)
Wilson, R. P., Jr.
(Little (Arthur D.), Inc. Cambridge, MA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1980
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-159796
ADL-83381-2
Report Number: NASA-CR-159796
Report Number: ADL-83381-2
Accession Number
80N18040
Funding Number(s)
CONTRACT_GRANT: NAS3-21980
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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