耐久性
鼓
助推器(火箭)
燃气轮机
涡轮机
航空发动机
结构工程
汽车工程
机械工程
材料科学
工程类
复合材料
航空航天工程
作者
А. Н. Архипов,Yu. A. Ravikovich,D. P. Kholobtsev,A.S. Shakhov
出处
期刊:Inventions
[Multidisciplinary Digital Publishing Institute]
日期:2022-06-23
卷期号:7 (3): 49-49
被引量:1
标识
DOI:10.3390/inventions7030049
摘要
A calculation-experimental study of durability of titanium booster drum of gas turbine engine (GTE) was carried out. A methodology of experimental estimation of titanium component life of GTE using structurally similar elements (SSE) has been proposed. A series of three-dimensional calculations by the finite element method of SSE cut out of the finished part was carried out to estimate the strength of the booster drum. A methodology for testing the durability of SSE in the low-cycle fatigue (LCF) area was developed, and statistical processing of the test results was performed. Tests of SSE allowed carrying out advanced-edge assessment of the durability of a full-size drum, taking into account the manufacturing technology.
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