非定常状态下燃气轮机叶片损伤诊断系统的外壳几何形状优化模型

Q3 Engineering
I. Andrianov, Elena K. Chepurnova
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引用次数: 1

摘要

燃气涡轮发动机叶片在非稳态状态下的损伤诊断问题一直是科学研究的热点。本文提出了一种更精确地计算裂纹检测系统参数的模型,该模型使用胶囊系统,其中在压力的影响下,有一种具有电离性质的物质。在研究中,得到了涡轮叶片旋转过程中由离心拉力作用引起的不均匀压力的确定关系。得到了裂缝打开时保证胶囊破裂所需的最小胶囊直径的计算关系式,从而保证了裂纹检测系统的有效运行。计算了不同涡轮叶片转速下胶囊内的压力和胶囊的几何形状。给出了在不考虑离心力作用的情况下计算胶囊内压力的误差估计。所获得的依赖关系将显著优化涡轮叶片损伤检测系统,提高燃气涡轮发动机的运行效率和安全性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Optimization Model of the Shell Capsules Geometry for a System for Diagnosing Damage to Gas Turbine Blades in Non-stationary
Scientific research is devoted to the problem of diagnosing damage in the blades of gas turbine engines in non-stationary conditions. The paper proposes a model for a more accurate calculation of the parameters of the crack detection system using a system of capsules, inside of which, under the influence of pressure, there is a substance exhibiting ionizing properties. In the study, the relations for determining the uneven pressure due to the action of centrifugal tensile forces during the rotation of the turbine blade are obtained. The relations for calculating the minimum required diameter of the capsule to ensure the rupture of the capsule when cracks are opened for the effective operation of the crack detection system are obtained. Calculations of the pressure inside the capsule and the geometry of the capsule at different speeds of rotation of the turbine blade are carried out. An estimate of the error in calculating the pressure inside the capsule is given in the case of not taking into account the action of centrifugal forces. The obtained dependences will significantly optimize the system for detecting damage to turbine blades, and increase the efficiency and safety of the operation of gas turbine engines.
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来源期刊
International Journal of Mechanics
International Journal of Mechanics Engineering-Computational Mechanics
CiteScore
1.60
自引率
0.00%
发文量
17
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