Optimization of a Welded Portion of the High Pressure Compressor Rotor

被引:0
|
作者
Sal’nikov A.V. [1 ]
机构
[1] P.I. Baranov Central Institute of Aviation Motors (CIAM), ul. Aviamotornaya 2, Moscow
来源
Russian Aeronautics | 2020年 / 63卷 / 01期
关键词
disk; high-pressure compressor rotor; labyrinth seal; lock joint; optimization; radial clearances;
D O I
10.3103/S1068799820010171
中图分类号
学科分类号
摘要
An integrated method for optimization of a welded portion of a high pressure compressor rotor as a single object is developed. The minimum mass criterion is used in the optimization method; limitations are imposed in accordance with strength and stiffness requirements. An example is given of optimization of a typical welded portion of a high pressure compressor rotor resulting in mass reduction and increase of cyclic durability. © 2020, Allerton Press, Inc.
引用
收藏
页码:117 / 125
页数:8
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