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Energy efficient engine combustor test hardware detailed design reportThe combustor for the Energy Efficient Engine is an annular, two-zone component. As designed, it either meets or exceeds all program goals for performance, safety, durability, and emissions, with the exception of oxides of nitrogen. When compared to the configuration investigated under the NASA-sponsored Experimental Clean Combustor Program, which was used as a basis for design, the Energy Efficient Engine combustor component has several technology advancements. The prediffuser section is designed with short, strutless, curved-walls to provide a uniform inlet airflow profile. Emissions control is achieved by a two-zone combustor that utilizes two types of fuel injectors to improve fuel atomization for more complete combustion. The combustor liners are a segmented configuration to meet the durability requirements at the high combustor operating pressures and temperatures. Liner cooling is accomplished with a counter-parallel FINWALL technique, which provides more effective heat transfer with less coolant.
Document ID
19850002642
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Zeisser, M. H.
(United Technologies Corp. East Hartford, CT, United States)
Greene, W.
(United Technologies Corp. East Hartford, CT, United States)
Dubiel, D. J.
(United Technologies Corp. East Hartford, CT, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1982
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-167945
NAS 1.26:167945
PWA-5594-197
Report Number: NASA-CR-167945
Report Number: NAS 1.26:167945
Report Number: PWA-5594-197
Accession Number
85N10950
Funding Number(s)
CONTRACT_GRANT: NAS3-20646
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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