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NASA NTRS · Conference Paper
Pollution reduction technology program for turboprop engines
Attribution
This is the abstract and citation. Full text lives at NASA NTRS — we link out rather than host. All credit to the authors and Legacy CDMS.
Abstract
Verbatim from NASA NTRS. Not paraphrased, not summarized.
The reduction of CO, HC, and smoke emissions while maintaining acceptable NO(x) emissions without affecting fuel consumption, durability, maintainability, and safety was accomplished. Component combustor concept screening directed toward the demonstration of advanced combustor technology required to meet the EPA exhaust emissions standards for class P2 turboprop engines was covered. The combustion system for the Allison 501-D22A engine was used, and three combustor design concepts - reverse flow, prechamber, and staged fuel were evaluated.
Author
- Tomlinson, J. G. Detroit Diesel Allison
Citation: Tomlinson, J. G. (2016). Pollution reduction technology program for turboprop engines. Legacy CDMS. NASA NTRS ID 19780003126. https://ntrs.nasa.gov/citations/19780003126 ↗