A Third-Generation Swirl-Venturi Lean Direct Injection Combustor with a Prefilming Pilot InjectorThis paper presents experimental results for a low-NOxaero gas turbine combustor, in particular, a third-generationswirl-venturi lean direct injection (SV-LDI-3) combustor conceptcalled V4. The purpose of testing was three-fold. First,to evaluate the combustor against the 80% NOx reduction goalset by NASA’s AATT project. Second, to compare V4 to a previousSV-LDI-3 combustor concept called V3, especially at lowpower conditions. Third, to examine the accuracy of a type ofcorrelation equation frequently used by engine systems analysisgroups to estimate NOx emissions. All three testing goals weremet. For the first testing goal, with an estimated NOx reductionof 85%-90%, SV-LDI-3 V4 surpassed the AATT goal. For thesecond goal, however, V4 did not perform better than V3 at lowpower conditions. For the third goal, it was found that a majorassumption of the correlation equations — a simple dependenceon combustor inlet pressure — did not hold.
Document ID
20190026568
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Tacina, K. M. (NASA Glenn Research Center Cleveland, OH, United States)
Podboy, D. P. (NASA Glenn Research Center Cleveland, OH, United States)
Lee, F. P. (Woodward FST, Inc. Zeeland, MI, United States)
Dam, B. (Woodward FST, Inc. Zeeland, MI, United States)