The annular multi-hole radial jets have important effect on combustorliner.
环向径向射流对燃烧室火焰筒内的流场有着重要的影响。
2
The sealing structure seals the gap around the combustorliner of the combustor and absorbs, the difference in thermal expansion between the combustorliner and the surrounding structure.
密封结构密封围绕燃烧室燃烧班轮差距，吸收，在燃烧室之间的衬垫及周围结构的热膨胀差异。
3
The formation mechanism of bulging and cracking of combustor inner liner and his influence on gas turbine exhaust temperature dispersity was analyzed.