1) tip of blade
叶片轮缘
2) turbine crown
涡轮叶片轮缘
3) trailing edge of turbine vane
涡轮叶片尾缘
1.
Two-dimensional numerical simulation study have been conducted on flow and heat transfer of cooling configuration for trailing edge of turbine vane, the effects of the length of trailing edge (L/H), outlet air angle (a), the ratio of the coolant to mainstream mass flow (M) and the coolant Reynolds number (Re) on cooling efficiency were investigated.
对叶片尾缘偏劈缝冷却结构的流动与换热进行了二维的数值模拟,研究了涡轮叶片尾缘无量纲长度L/H(即尾缘长度与冷气 流出口的高度比)、偏劈缝喷射角α、吹风比M及Reynolds数(Re)对涡轮叶片尾缘平均冷却效果的影响。
4) turbine blade trailing edge
涡轮叶片尾缘通道
1.
Effect of different clapboards structure in turbine blade trailing edge complex passages on heat transfer characteristics;
涡轮叶片尾缘通道中纵向肋对换热特性的影响
6) edge modified blade
修缘叶片
补充资料：MS6001系列燃气轮机一级空心涡轮叶片
MS6001系列燃气轮机一级空心涡轮叶片
Ms6()()l系列燃气轮机一级空心涡轮叶片 中同科学院金属研究所供稿
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条