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Either stall or surge may result in combustor blowout .

不管是喘振或者爆音，都将引起燃烧室的熄火。

The first phase , which focused on the combustor and high-pressure turbine , was completed in september 2009 .

第一阶段致力于燃烧室和高压涡轮的测试已于2009年12月完成。

A trapped vortex combustor for gas turbine engines .

燃气轮机的截流涡流式燃烧器。

Combustor design practice of aero engine .

航空发动机燃烧室设计实务。

Refer to part 4 for combustor cooling techniques .

参见第4章燃烧室冷却技术。