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Lean, Premixed-Prevaporized (LPP) combustor conceptual design studyFour combustion systems were designed and sized for the energy efficient engine. A fifth combustor was designed for the cycle and envelope of the twin-spool, high bypass ratio, high pressure ratio turbofan engine. Emission levels, combustion performance, life, and reliability assessments were made for these five combustion systems. Results of these design studies indicate that cruise NOx emission can be reduced by the use of lean, premixed-prevaporaized combustion and airflow modulation.
Document ID
19790023187
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Dickman, R. A.
(General Electric Co. Cincinnati, OH, United States)
Dodds, W. J.
(General Electric Co. Cincinnati, OH, United States)
Ekstedt, E. E.
(General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1979
Subject Category
Inorganic And Physical Chemistry
Report/Patent Number
NASA-CR-159629
R79AEG376
Report Number: NASA-CR-159629
Report Number: R79AEG376
Accession Number
79N31358
Funding Number(s)
CONTRACT_GRANT: NAS3-21255
PROJECT: RTOP 511-55-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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