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Pollution reduction technology program for small jet aircraft engines, phase 2
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Mongia, H. C. Bruce, T. W. Kuhn, T. E. Davis, F. G. |
| Copyright Year | 1978 |
| Description | A series of iterative combustor pressure rig tests were conducted on two combustor concepts applied to the AiResearch TFE731-2 turbofan engine combustion system for the purpose of optimizing combustor performance and operating characteristics consistant with low emissions. The two concepts were an axial air-assisted airblast fuel injection configuration with variable-geometry air swirlers and a staged premix/prevaporization configuration. The iterative rig testing and modification sequence on both concepts was intended to provide operational compatibility with the engine and determine one concept for further evaluation in a TFE731-2 engine. |
| File Size | 17315865 |
| Page Count | 188 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19780025161 |
| Archival Resource Key | ark:/13960/t8hf2n69s |
| Language | English |
| Publisher Date | 1978-09-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Exhaust Gases Pollution Control Emission Turbofan Engines Combustion Engine Tests Combustion Efficiency Jet Engines Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
