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Pollution reduction technology program for turboprop engines
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Tomlinson, J. G. |
| Copyright Year | 1977 |
| Description | 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. |
| File Size | 1062284 |
| Page Count | 23 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19780003126 |
| Archival Resource Key | ark:/13960/t3324r096 |
| Language | English |
| Publisher Date | 1977-10-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Systems Engineering Exhaust Gases Pollution Control Project Management Air Pollution Turboprop Engines Aircraft Engines Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
