航空学报2026，Vol.47Issue(1)：197-209,13.DOI:10.7527/S1000-6893.2024.32061
中介轴承-支承结构载荷及其对结构完整性影响
Loading of intermediate bearing-support structure and its impact on structural integrity
摘要
Abstract
In advanced aero-engines,a dual-rotor support scheme with an intermediate bearing is often employed to reduce the number of load-bearing frames and decrease the overall weight of the engine.However,the intermediate bearing-support structure system exhibits typical discontinuous characteristics and is influenced by the complex motion states of the dual rotors during operation,resulting in a harsh and variable load environment for the intermediate bearing-support structure system,which can easily lead to structural damage.Focusing on the intermediate bearing-support structure system,this study analyzes the impact of changes in rotor motion states on the load environment of the bearing-support structure system,and proposes design requirements for the bearing-support structure aimed at en-suring structural integrity.Research indicates that under different rotor motion states,the interactive effects of bearing component motions subject the structural system to complex load excitations such as impact excitation,rotor harmonic excitation,combined frequency excitation of dual-rotor speeds,and rotor-cage speed modulation frequency excitation.These excitations cause the constraint characteristics of the support structure to deviate from the design values until failure occurs.Therefore,it is necessary to consider the influence of different rotor motion states in the structural de-sign,and to verify and optimize the mechanical characteristics of the structure based on these considerations.关键词
中介轴承-支承结构/运动状态/支点动载荷/结构完整性/航空发动机Key words
intermediate bearing-support structure/motion state/dynamic load at support points/structural integ-rity/aero-engines分类
航空航天引用本文复制引用
陈雪骑,张作相,王东,马艳红,洪杰..中介轴承-支承结构载荷及其对结构完整性影响[J].航空学报,2026,47(1):197-209,13.基金项目
国家科技重大专项(J2022-Ⅳ-0004-0021,J2022-Ⅳ-0003-0020) National Science and Technology Major Project(J2022-Ⅳ-0004-0021,J2022-Ⅳ-0003-0020) （J2022-Ⅳ-0004-0021,J2022-Ⅳ-0003-0020）
