发明授权
US07827777B2 Combustor with reduced carbon monoxide emissions 有权
燃烧器减少一氧化碳排放

Combustor with reduced carbon monoxide emissions
摘要:
A combustor arrangement for a gas turbine engine (31) has a split line (42) and a plurality of burners (20,37) arranged in an annular ring (40). The burners (46) of the combustor on either side of the split line (42) have a separation distance of at least two times the average separation distance between burners (48) distant from the split line (42).
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