发明申请
US20080184708A1 Gas Turbine Combustor 有权
燃气轮机燃烧器

Gas Turbine Combustor
摘要:
A gas turbine combustor includes a pilot burner, a plurality of main burners disposed around the main burners on the radially outer side. Each of the main burners (2) includes an extension tube disposed at the downstream end. The outlet of the extension tube is shaped to have a radial edge which is parallel to the radial direction. In this manner, occurrence of flashback is effectively prevented.
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