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发动机风扇盘转速谱编制方法

贾震 李晨迪 卫昆钰 董宏达 贺小帆

航空学报2026,Vol.47Issue(2):106-123,18.
航空学报2026,Vol.47Issue(2):106-123,18.DOI:10.7527/S1000-6893.2025.32110

发动机风扇盘转速谱编制方法

Speed spectrum development method for engine fan disk

贾震 1李晨迪 1卫昆钰 1董宏达 2贺小帆1

作者信息

  • 1. 北京航空航天大学航空科学与工程学院强度与结构完整性全国重点实验室,北京 102206
  • 2. 中国航空工业集团公司沈阳飞机设计研究所,沈阳 110000
  • 折叠

摘要

Abstract

The fan disk is a critical fracture-prone component in aero-engines.To ensure its operational safety and re-liability,it is essential to develop load spectra that accurately reflect operating conditions,which are crucial for fatigue life assessment.This study conducts statistical analysis of single-parameter loading on fan disks based on operational data from two mission types of a specific aero-engine,and develops a median speed spectrum through mission seg-ment analysis methodology.The load spectrum damage was calculated using the SWT(Smith-Watson-Topper)equa-tion and linear cumulative damage theory.Load spectrum similarity analysis was conducted with the DTW(Dynamic Time Warping)method.Based on group tests of TC17 titanium alloy simulated specimens,a damage analysis method based on load spectrum similarity was proposed.The damage of the fleet fan disk rotational speed spectrum was calculated to obtain a set of load spectrum damage samples.Goodness-of-fit tests indicate that the fan disk rota-tional speed spectrum damage follows a lognormal distribution.The damage corresponding to the median rotational speed spectrum closely approximates the median damage of the fleet rotational speed spectrum,validating the ratio-nality of the spectrum development methodology.This provides critical support for accurately assessing the safe ser-vice life of fan disks.

关键词

发动机风扇盘/转速谱/载荷谱编制/相对损伤/概率分布

Key words

engine fan disk/speed spectrum/load spectrum development/relative damage/probability distribution

分类

航空航天

引用本文复制引用

贾震,李晨迪,卫昆钰,董宏达,贺小帆..发动机风扇盘转速谱编制方法[J].航空学报,2026,47(2):106-123,18.

基金项目

国家科技重大专项(J09-Ⅳ-0017-0085) (J09-Ⅳ-0017-0085)

国家自然科学基金(12472341) (12472341)

航空科学基金(20240037051001) National Science and Technology Major Project of China(J09-Ⅳ-0017-0085) (20240037051001)

National Natural Science Foundation of China(12472341) (12472341)

Aeronautical Science Foundation of China(20240037051001) (20240037051001)

航空学报

1000-6893

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