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Title: Combustion oscillation control by cyclic fuel injection

Journal Article · · Journal of Engineering for Gas Turbines and Power
DOI:https://doi.org/10.1115/1.2815580· OSTI ID:522391
; ;  [1]; ;  [2]
  1. Morgantown Energy Technology Center, WV (United States)
  2. Solar Turbines, Inc., San Diego, CA (United States)

A number of recent articles have demonstrated the use of active control to mitigate the effects of combustion instability in afterburner and dump combustor applications. In these applications, cyclic injection of small quantities of control fuel has been proposed to counteract the periodic heat release that contributes to undesired pressure oscillations. This same technique may also be useful to mitigate oscillations in gas turbine combustors, especially in test rig combustors characterized by acoustic modes that do not exist in the final engine configuration. To address this issue, the present paper reports on active control of a subscale, atmospheric pressure nozzle.combustor arrangement. The fuel is natural gas. Cyclic injection of 14 percent control fuel in a premix fuel nozzle is shown to reduce oscillating pressure amplitude by a factor of 0.30 (i.e., {minus}10 dB) at 300 Hz. Measurement of the oscillating heat release is also reported.

Sponsoring Organization:
USDOE
OSTI ID:
522391
Report Number(s):
CONF-950629-; ISSN 0742-4795; TRN: IM9739%%112
Journal Information:
Journal of Engineering for Gas Turbines and Power, Vol. 119, Issue 2; Conference: 40. International gas turbine and aeroengine congress and exposition, Houston, TX (United States), 5-8 Jun 1995; Other Information: PBD: Apr 1997
Country of Publication:
United States
Language:
English