System and method for reducing combustion dynamics in a turbomachine
a turbomachine and combustion dynamics technology, applied in the field of turbomachines, can solve the problems of combustion screech, high cycle fatigue (hcf) of downstream turbomachine components, and low frequency dynamic fields that have a negative impact on various turbomachine components
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[0015]The terms “axial” and “axially” as used in this application refer to directions and orientations extending substantially parallel to a center longitudinal axis of a centerbody of a burner tube assembly. The terms “radial” and “radially” as used in this application refer to directions and orientations extending substantially orthogonally to the center longitudinal axis of the centerbody. The terms “upstream” and “downstream” as used in this application refer to directions and orientations relative to an axial flow direction with respect to the center longitudinal axis of the centerbody.
[0016]With initial reference to FIG. 1, a turbomachine constructed in accordance with exemplary embodiments of the invention is generally indicated at 2. Turbomachine 2 includes a compressor 4 and a combustor assembly 5 having at least one combustor 6 provided with an injection nozzle assembly housing 8. Turbomachine 2 also includes a turbine 10 and a common compressor / turbine shaft 12. In one ex...
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