Damage Analysis of a Reusable Rocket Engine Turbine Disk Considering the Ratcheting Effect

SUN Yujian; DU Dahua; WANG Jun; LI Binchao; XU Zili

doi:10.7652/xjtuxb202608021

您当前的位置：

首页 >

文章列表页 >

Damage Analysis of a Reusable Rocket Engine Turbine Disk Considering the Ratcheting Effect

更新时间：2026-07-28

- Damage Analysis of a Reusable Rocket Engine Turbine Disk Considering the Ratcheting Effect
- Journal of Xi'an Jiaotong University Vol. 60, Issue 8, Pages: 240-248(2026)
- 作者机构：
  
  西安交通大学复杂服役环境重大装备结构强度与寿命全国重点实验室，710049，西安
  西安交通大学航天航空学院，710049，西安
  西安航天动力研究所液体火箭发动机技术重点实验室，710100，西安
- 作者简介：
- 基金信息：
- DOI：10.7652/xjtuxb202608021
  CLC： V434.211
- Received：31 October 2025，
  
  Online First：09 December 2025，
  
  Published：10 August 2026
- 稿件说明：
移动端阅览
SUN Yujian, DU Dahua, WANG Jun, et al. Damage Analysis of a Reusable Rocket Engine Turbine Disk Considering the Ratcheting Effect[J]. Journal of Xi'an Jiaotong University, 2026, 60(8): 240-248.
DOI：

SUN Yujian, DU Dahua, WANG Jun, et al. Damage Analysis of a Reusable Rocket Engine Turbine Disk Considering the Ratcheting Effect[J]. Journal of Xi'an Jiaotong University, 2026, 60(8): 240-248. DOI： 10.7652/xjtuxb202608021.

摘要

针对可重复使用液体火箭发动机涡轮盘在多次启停工况下，由非对称循环应力引起塑性应变累积继而引发棘轮效应，从而严重影响结构寿命的问题，开展了涡轮盘在重复使用工况下的结构损伤分析。基于Chaboche随动强化模型，对涡轮盘在循环载荷下的力学响应进行表征，结合应力-应变演化规律系统分析了结构的棘轮行为。通过量化棘轮效应导致的损伤，结合线性累积损伤理论对结构损伤状态进行了评估。研究结果表明：多次启停工况中，涡轮盘出气侧叶型底部区域失效风险较高；棘轮损伤在初始循环周次最大，随后逐渐减小并趋于稳定；累积棘轮损伤在循环过程中呈非线性演化特征，损伤增量随着循环次数的增加逐渐减小；在10次循环中，随着棘轮应变增量减小，棘轮损伤的占比逐渐降低，疲劳损伤占比随循环次数逐渐提升至96%以上。该研究为可重复使用火箭发动机涡轮盘的结构损伤评估与寿命预测提供了理论分析基础。

Abstract

To address how the ratcheting effect—caused by cumulative plastic strain from asymmetric cyclic stresses under multiple start-stop cycles—seriously affects the structural life of reusable liquid rocket engine turbine disks

a structural damage analysis was conducted on turbine disks under reusable operating conditions. Based on the Chaboche kinematic hardening model

the mechanical response of the turbine disk under cyclic loading was characterized

and the ratcheting behavior of the structure was systematically analyzed in conjunction with the stressstrain evolution law. By quantifying the damage caused by the ratcheting effect

the structural damage state was assessed using the linear cumulative damage theory. The research results show that under multiple start-stop cycles

the trailing-edge blade root region is at a higher risk of failure. Ratcheting damage is greatest in the initial cycles and then gradually decreases before stabilizing. Cumulative ratcheting damage exhibits a nonlinear evolution with cycle number

as the damage increment gradually decreases over cycles. Over the 10 cycles considered

as the ratcheting strain increment decreases

the proportion of ratcheting damage gradually decreases

while the proportion of fatigue damage gradually increases to over 96% with cycle number. This study provides a theoretical basis for the structural damage assessment and life prediction of reusable rocket engine turbine disks.

关键词

Keywords

references

包为民.可重复使用运载火箭技术发展综述[J].航空学报，2023，44（23）：1-26.

Bao Weimin. A review of reusable launch vehicle technology development[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44 (23): 1-26.

刘敏华.猎鹰9号火箭发射及箭体复用的分析[J].宇航总体技术，2024，8（1）：20-27.

Liu Minhua. Analysis of falcon 9 launch and booster reuse[J]. Astronautical Systems Engineering Technology, 2024, 8 (1): 20-27.

王小军.中国航天运输系统未来发展展望[J].导弹与航天运载技术，2021（1）：1-6.

Wang Xiaojun. Future development of space transportation system of China[J]. Missiles and Space Vehicles, 2021 (1): 1-6.

李斌，张小平，高玉闪.我国可重复使用液体火箭发动机发展的思考[J].火箭推进，2017，43（1）：1-7.

Li Bin, Zhang Xiaoping, Gao Yushan. Consideration on development of reusable liquid rocket engine in China[J]. Journal of Rocket Propulsion, 2017, 43 (1): 1-7.

Hale J R, Klatt F P.SSME improvements for routine shuttle operations [C]//21st Joint Propulsion Conference. Reston, VA, USA:AIAA,1985:AIAA 19851163.

Tischer A E, Glover R C.Studies and analyses of the space shuttle main engine [EB/OL].（1987-12-31）[2025-06-20]. https://ntrs.nasa.gov/citations/19890009154.

吴锦涛，王珺，徐自力，等.高转速部分进气涡轮盘气流力及叶片振动响应研究[J].西安交通大学学报，2022，56（7）：108-117.

Wu Jintao, Wang Jun, Xu Zili, et al. Airflow force and vibration response for high speed partial-admission turbine disk[J]. Journal of Xi'an Jiaotong University, 2022, 56 (7): 108-117.

李康迪，王珺，徐自力，等.某型液体火箭发动机部分进气涡轮盘振动分析及改型设计[J].火箭推进，2023，49（1）：80-86.

Li Kangdi, Wang Jun, Xu Zili, et al. Vibration analysis and modification design of partial admission turbine disk for a liquid rocket engine[J]. Journal of Rocket Propulsion, 2023, 49 (1): 80-86.

黄朝晖，袁奇，张弘斌，等.某型火箭发动机涡轮转子流热固耦合强度及疲劳寿命分析[J].西安交通大学学报，2022，56（8）：73-84.

Huang Chaohui, Yuan Qi, Zhang Hongbin, et al. Analysis of fluid-thermal-solid coupling strength and fatigue life of a certain rocket engine turbine rotor[J]. Journal of Xi'an Jiaotong University, 2022, 56 (8)：73-84.

刘士杰，刘登丰，马晓秋，等.重复使用液体火箭发动机涡轮泵安全寿命预估方法[J].航空动力学报，2022，37（5）：1079-1089.

Liu Shijie, Liu Dengfeng, Ma Xiaoqiu, et al. Predicting method of safety life of reusable liquid rocket engine turbopump[J]. Journal of Aerospace Power, 2022, 37 (5): 1079-1089.

杜大华，王珺，王红建，等.液体火箭发动机涡轮盘低周疲劳寿命预测[J].火箭推进，2020，46（6）：16-24.

Du Dahua, Wang Jun, Wang Hongjian, et al. Low cycle fatigue life prediction of a liquid rocket engine turbine disk[J]. Journal of Rocket Propulsion, 2020, 46 (6): 16-24.

金平，吕俊杰，戚亚群，等.可重复使用液体火箭发动机寿命问题探讨[J].宇航总体技术，2023，7（4）：51-59.

Jin Ping, Lü Junjie, Qi Yaqun, et al. Discussion on the life of reusable liquid rocket engine[J]. Astronautical Systems Engineering Technology, 2023, 7 (4)：51-59.

姜金朋，刘志超，刘筑，等.火箭发动机涡轮典型结构形式对叶片低周疲劳寿命的影响研究[J].宇航总体技术，2020，4（5）：51-64.

Jiang Jinpeng, Liu Zhichao, Liu Zhu, et al. Effects of turbine structure on life of turbine blade for liquid rocket engine[J]. Astronautical Systems Engineering Technology, 2020, 4 (5): 51-64.

Wang Wei, Ma Yixin, Liu Bingyang, et al. Reliability analysis of reusable turbine rotor blisk:an application of parametric modelling method under multi-field coupling [J].Engineering Failure Analysis,2023, 152:107511.

Rezaiee-Pajand M, Sinaie S.On the calibration of the Chaboche hardening model and a modified hardening rule for uniaxial ratcheting prediction [J].International Journal of Solids and Structures,2009,46（16）：3009-3017.

Prager W.A new method of analyzing stresses and strains in work-hardening plastic solids[J].Journal of Applied Mechanics,1956,23（4）:493-496.

Frederick C O, Armstrong P J.A mathematical representation of the multiaxial Bauschinger effect [J]. Materials at High Temperatures,2007,24（1）:1-26.

Chaboche J L.Time-independent constitutive theories for cyclic plasticity [J].International Journal of Plasticity,1986,2（2）:149-188.

姜金朋，陈涛，金平，等.Chaboche随动硬化模型参数确定及棘轮效应[J].北京航空航天大学学报，2014，40（10）：1430-1435.

Jiang Jinpeng, Chen Tao, Jin Ping, et al. Parameter determination of Chaboche kinematic hardening models and ratcheting simulation[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40 (10): 1430-1435.

刘士杰，王召，刘继超，等.基于Chaboche硬化模型的304SS全寿命循环力学行为仿真分析[J].火箭推进，2022，48（3）：40-49.

Liu Shijie, Wang Zhao, Liu Jichao, et al. Simulation analysis of 304SS full-life cyclic mechanical behavior based on Chaboche hardening model[J]. Journal of Rocket Propulsion, 2022, 48 (3): 40-49.

Ren Peirong, Huang Weiqing, Yang Xiaoguang, et al. A modified constitutive model considering microstructure degradation of Ni-based superalloys and its application to microstructural damage calculation[J].Journal of Alloys and Compounds,2021,882:160605.

尚福林.塑性力学基础[M].3版.西安：西安交通大学出版社，2018.

闫晓军，聂景旭.涡轮叶片疲劳[M].北京：科学出版社，2014.

黄峻峰，贺尔铭，易金翔，等.再生冷却推力室热机疲劳寿命预测研究[J].西北工业大学学报，2022， 40（4）：723-731.

Huang Junfeng, He Erming, Yi Jinxiang, et al. Research on thermomechanical fatigue life prediction of regenerative cooling thrust chamber[J]. Journal of Northwestern Polytechnical University, 2022, 40 (4)：723-731.

Chandler W T.Materials for advanced rocket engine turbopump turbine blades [EB/OL].（1985-04-01）[2025-09-12]. https://ntrs.nasa.gov/citations/19850018561.

Views

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Study on Electrothermal Characteristics of Dendrite-Induced Internal Short Circuit in Lithium-Ion Batteries

Phase-Field Analysis Method for the Reliability of High-g Micro-Electro-Mechanical System Accelerometers

Laser Dispersion Interferometry Method for the Diagnosis of Corona Plasma Density in Electrical Explosion of Wires

AnIn-Situ Constructed ZnS/Graphene Electrochemical Sensor for Neurotransmitter Dopamine Detection

Binocular Vision-Based Synchronous Measurement Method for Rotational Errors

Related Author

SUN Yujian

DU Dahua

WANG Jun

LI Binchao

XU Zili

Related Institution

State Key Laboratory for Strength and Vibration of Mechanical Structures, Xi’an Jiaotong University

School of Aerospace Engineering, Xi’an Jiaotong University

Science and Technology on;Liquid Rocked Engine Laboratory, Xi’an Aerospace Propulsion Institute

⁰