Variable volume combustor with an air bypass system [electronic resource].
- Published:
- Washington, D.C. : United States. Dept. of Energy, 2017.
Oak Ridge, Tenn. : Distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy - Additional Creators:
- General Electric Company
United States. Department of Energy
United States. Department of Energy. Office of Scientific and Technical Information - Access Online:
- www.osti.gov
- Summary:
- The present application provides a combustor for use with flow of fuel and a flow of air in a gas turbine engine. The combustor may include a number of micro-mixer fuel nozzles positioned within a liner and an air bypass system position about the liner. The air bypass system variably allows a bypass portion of the flow of air to bypass the micro-mixer fuel nozzles.
- Subject(s):
- Note:
- Published through SciTech Connect.
02/07/2017.
"9,562,687"
"13/760,101"
Thomas Edward Johnson; Willy Steve Ziminsky; Heath Michael Ostebee; Christopher Paul Keener. - Funding Information:
- FC26-05NT42643
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