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Title: Flow conditioner for fuel injector for combustor and method for low-NO.sub.x combustor

An injector for a gas turbine combustor including a catalyst coated surface forming a passage for feed gas flow and a channel for oxidant gas flow establishing an axial gas flow through a flow conditioner disposed at least partially within an inner wall of the injector. The flow conditioner includes a length with an interior passage opening into upstream and downstream ends for passage of the axial gas flow. An interior diameter of the interior passage smoothly reduces and then increases from upstream to downstream ends.
Authors:
; ;
Publication Date:
OSTI Identifier:
1092904
Report Number(s):
8,528,334
12/015,366
DOE Contract Number:
FC26-05NT42647
Resource Type:
Patent
Research Org:
Solar Turbines Inc. (San Diego, CA)
Sponsoring Org:
USDOE
Country of Publication:
United States
Language:
English
Subject:
33 ADVANCED PROPULSION SYSTEMS