发明授权
US6006523A Gas turbine combustor with angled tube section 失效
燃气轮机燃烧器具有倾斜的管段

Gas turbine combustor with angled tube section
摘要:
A combustor inner tube 102 or a burner 101 provided on the upstream side of a tail pipe 103 having a straight or substantially straight axis is disposed at an angle with respect to the axis of tail pipe 103, by which a secondary flow is produced in combustion gas. Thereby, low-temperature gas at the outer peripheral portion is mixed with high-temperature gas at the central portion so that the gas temperature distribution is made uniform.
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