NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
The E3 combustors: Status and challengesThe design, fabrication, and initial testing of energy efficient engine combustors, developed for the next generation of turbofan engines for commercial aircraft, are described. The combustor designs utilize an annular configuration with two zone combustion for low emissions, advanced liners for improved durability, and short, curved-wall, dump prediffusers for compactness. Advanced cooling techniques and segmented construction characterize the advanced liners. Linear segments are made from castable, turbine-type materials.
Document ID
19810019557
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sokolowski, D. E. (NASA Lewis Research Center Cleveland, OH, United States)
Rohde, J. E. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1981
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-82684
E-904
Report Number: NASA-TM-82684
Report Number: E-904
Meeting Information
Meeting: Joint Propulsion Conf.
Location: Colorado Springs, CO
Country: United States
Start Date: July 27, 1981
End Date: July 29, 1981
Sponsors: AIAA, ASME, SAE
Accession Number
81N28095
Funding Number(s)
PROJECT: RTOP 535-01-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available