Abstract

A method for constructing a solution to the problem of long-term durability and rigidity of gas turbine engine blades under thermomechanical load is considered. The solution is based on a three-component model of long-term deformation.

中文翻译：

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结构异构燃气轮机叶片的长期耐用性和刚性

摘要

考虑一种构造用于解决在热机械载荷下的燃气涡轮发动机叶片的长期耐久性和刚度问题的解决方案的方法。该解决方案基于长期变形的三分量模型。