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Device to lower NOx in a gas turbine engine combustion system [electronic resource].

Published
Washington, D.C. : United States. Dept. of Energy, 2015.
Oak Ridge, Tenn. : Distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy
Additional Creators
United States. Department of Energy and United States. Department of Energy. Office of Scientific and Technical Information
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Summary
An emissions control system for a gas turbine engine including a flow-directing structure (24) that delivers combustion gases (22) from a burner (32) to a turbine. The emissions control system includes: a conduit (48) configured to establish fluid communication between compressed air (22) and the combustion gases within the flow-directing structure (24). The compressed air (22) is disposed at a location upstream of a combustor head-end and exhibits an intermediate static pressure less than a static pressure of the combustion gases within the combustor (14). During operation of the gas turbine engine a pressure difference between the intermediate static pressure and a static pressure of the combustion gases within the flow-directing structure (24) is effective to generate a fluid flow through the conduit (48).
Report Numbers
E 1.99:8,959,888
8,959,888
Subject(s)
Note
Published through SciTech Connect.
02/24/2015.
"8,959,888"
"13/305,120"
Laster, Walter; Schilp, Reinhard; Wiebe, David.
Siemens Energy, Inc., Orlando, FL (United States)
Funding Information
FC26-05NT42644
View MARC record | catkey: 23492044