Weight optimization principles for turbine blade shroud platform

被引：0
|
作者：
Belousov A.I. [1 ]
Nazdrachev S.V. [1 ]
机构：
[1] Samara State Aerospace University, shosse Moskovskoe 34, Samara
来源：
Russian Aeronautics (Iz VUZ) | 2016年 / 59卷 / 1期
关键词：
labyrinth seal; radial clearance losses; shroud platform; turbine efficiency;
D O I：
10.3103/S1068799816010086
中图分类号：
学科分类号：
摘要：
The paper describes the development of NK-family engine shrouded turbine blades. Weight optimization principles are formulated with account for strength and manufacturability limits. © 2016, Allerton Press, Inc.
引用
收藏
页码：51 / 57
页数：6
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