发明申请
US20130255262A1 Combustor with Non-Circular Head End 有权
非圆形头端燃烧器

Combustor with Non-Circular Head End
摘要:
The present application provides a combustor for use with a gas turbine engine. The combustor may include a head end with a non-circular configuration, a number of fuel nozzles positioned about the head end, and a transition piece extending downstream of the head end.
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