摘要
简要分析了某重型燃气轮机的气冷叶片、叶尖间隙、整体蜂窝外环和后支承环组件等涡轮部件结构设计的一些独特设计思路和方法。
Some unique design concepts and methods of turbine structure design, which included air cooling blade, blade-tip clearance, integral honeycomb outer ring and rearing supporting ring assemblies were analyzed briefly far a heavy duty gas turbine.
出处
《航空发动机》
2010年第2期13-15,58,共4页
Aeroengine
关键词
涡轮
结构设计
重型燃气轮机
整体蜂窝外环
“矩阵型”肋:强化换热
turbine
structure design
heavy duty gas turbine
integral honeycomb outer ring
matrix type rib
strengthening regeneration
