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Methods and systems to facilitate reducing NO.sub.x emissions in combustion systems

Patent ·
OSTI ID:1015311

A method for assembling a gas turbine combustor system is provided. The method includes providing a combustion liner including a center axis, an outer wall, a first end, and a second end. The outer wall is orientated substantially parallel to the center axis. The method also includes coupling a transition piece to the liner second end. The transition piece includes an outer wall. The method further includes coupling a plurality of lean-direct injectors along at least one of the liner outer wall and the transition piece outer wall such that the injectors are spaced axially apart along the wall.

Research Organization:
General Electric Company (Schenectady, NY)
Sponsoring Organization:
USDOE
DOE Contract Number:
FC26-05NT42643
Assignee:
General Electric Company (Schenectady, NY)
Patent Number(s):
7,886,545
Application Number:
US Patent Application 11/741,502
OSTI ID:
1015311
Country of Publication:
United States
Language:
English

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