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U.S. Department of Energy
Office of Scientific and Technical Information

Combustor oscillating pressure stabilization and method

Patent ·
OSTI ID:871766

High dynamic pressure oscillations in hydrocarbon-fueled combustors typically occur when the transport time of the fuel to the flame front is at some fraction of the acoustic period. These oscillations are reduced to acceptably lower levels by restructuring or repositioning the flame front in the combustor to increase the transport time. A pilot flame front located upstream of the oscillating flame and pulsed at a selected frequency and duration effectively restructures and repositions the oscillating flame in the combustor to alter the oscillation-causing transport time.

Research Organization:
EG & G TECH SVCS OF WV INC
DOE Contract Number:
AC21-90MC26328
Assignee:
United States of America as represented by United States (Washington, DC)
Patent Number(s):
US 5791889
OSTI ID:
871766
Country of Publication:
United States
Language:
English

References (7)

Practical active control system for combustion oscillations journal May 1990
Active control for gas turbine combustors journal January 1991
A review of active control of combustion instabilities journal January 1993
Active control of reheat buzz journal July 1988
Combustion instabilities coupled by pressure waves and their active control journal January 1992
Active control of unsteady combustion-induced oscillations journal September 1992
Closed-loop amplitude modulation control of reacting premixed turbulent jet journal December 1991