Two-branch mixing passage and method to control combustor pulsations
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United States of America Patent
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Jan 3, 2017
Grant Date -
Sep 25, 2014
app pub date -
May 9, 2014
filing date -
Oct 24, 2005
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Abstract
A gas turbine engine combustion system including a mixing duct that separates into at least two branch passages for the delivery of a fuel and working fluid to distinct locations within a combustion chamber. The residence time for the fuel and working fluid within each of the two branch passages is distinct.
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