海军航空大学学报2024，Vol.39Issue(5)：557-566,10.DOI:10.7682/j.issn.2097-1427.2024.05.005
考虑加工误差及多工况影响的压气机叶型鲁棒性优化
Robustness Optimization of Compressor Blade Profile Considering Machining Errors and Multi-Working Conditions
摘要
Abstract
To address the engineering needs of compressor blade profiles operating at low losses over a wide angle of at-tack and a wide range of Mach number,and the insensitivity of blade performance to machining errors,a blade profile op-timization process considering machining errors and geometric parameters is established firstly.Then,based on the built-in surrogate model,a robust optimization design study of compressor blade profile is conducted for a specific compressor stator blade profile at design Mach numbers of 0.87(transonic flow)and 0.7(subsonic flow),taking into account machin-ing errors and multi-angle-of-attack conditions.The results show that the blade profile optimized for transonic flow condi-tions has greatly improved angle-of-attack characteristics,but slightly deteriorated for subsonic flow conditions.The blade profile optimized for subsonic flow conditions has greatly improved angle-of-attack characteristics for multiple low Mach number conditions,but deteriorated for transonic flow conditions.关键词
压气机叶型/多工况/加工误差/鲁棒性优化/气动性能Key words
compressor blade profile/multiple working conditions/machining error/robustness optimization/aerodynam-ic performance分类
军事科技引用本文复制引用
杨荣菲,沈法祥,龚志豪,王彬..考虑加工误差及多工况影响的压气机叶型鲁棒性优化[J].海军航空大学学报,2024,39(5):557-566,10.基金项目
航空科学基金(201907052001) （201907052001）
