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[1]张凭,李斌,高玉闪,等.重复使用火箭发动机推力室疲劳寿命研究进展[J].火箭推进,2024,50(01):12-27.[doi:10.3969/j.issn.1672-9374.2024.01.002]
　ZHANG Ping,LI Bin,GAO Yushan,et al.Research progress of fatigue life for the thrust chamber of reusable rocket engines[J].Journal of Rocket Propulsion,2024,50(01):12-27.[doi:10.3969/j.issn.1672-9374.2024.01.002]
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重复使用火箭发动机推力室疲劳寿命研究进展

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 50 期数: 2024年01期 页码: 12-27 栏目: 目次 出版日期: 2024-02-28
Title:
Research progress of fatigue life for the thrust chamber of reusable rocket engines
文章编号:
1672-9374(2024)01-0012-16
作者:
张凭1; 李斌2; 高玉闪1; 霍世慧1; 王振1
1.西安航天动力研究所 航天液体动力全国重点实验室,陕西 西安 710100; 2.航天推进技术研究院,陕西 西安 710100
Author(s):
ZHANG Ping1;  LI Bin2;  GAO Yushan1;  HUO Shihui1;  WANG Zhen1
1. National Key Laboratory of Aerospace Liquid Propulsion, Xi'an Aerospace Propulsion Institute, Xi'an 710100, China; 2.Academy of Aerospace Propulsion Technology, Xi'an 710100, China
关键词:
重复使用;  液体火箭发动机;  再生冷却推力室;  热-机械失效;  疲劳寿命预测
Keywords:
reusability;  liquid rocket engine;  regeneratively-cooled thrust chamber;  thermal-mechanical failure;  fatigue life prediction
分类号:
V434.3
DOI:
10.3969/j.issn.1672-9374.2024.01.002
文献标志码:
A
摘要:
再生冷却推力室内壁的热-机械疲劳失效严重影响重复使用液体火箭发动机的可靠性和使用寿命,疲劳分析在内壁损伤机理研究、寿命预测和结构优化设计中具有重要作用。简要回顾了推力室再生冷却结构热-机械疲劳分析方法的发展历程,重点围绕材料本构关系、热-力响应计算和疲劳寿命模型,对比梳理已有方法,讨论其特点及应用。基于研究进展与工程需求,从全服役周期瞬态载荷环境、材料本构关系、热-机械损伤模型及验证、基体与涂/镀层耦合失效分析和基于有限数据的工程方法等方面给出了进一步研究的方向和建议。
Abstract:
The thermal-mechanical fatigue failure of regeneratively-cooled thrust chamber wall seriously affects the reliability and service life of reusable liquid rocket engines. Fatigue analysis plays an important role in the study of damage mechanism, life time prediction and structural optimization. The development of thermal-mechanical fatigue analyzing method for the regenerative cooling structure of thrust chambers was briefly reviewed. Focusing on constitutive relations of material, calculation of thermal-mechanical response and fatigue life models, developed methods were summarized and compared, their characteristics and applications were discussed. Based on the research progress and engineering requirement, suggestions were given for further research, in terms of the transient load condition of full service period, constitutive relations, thermal-mechanical damage model and verification, matrix-coating-coupled failure analysis and limited-data-based engineering approach.

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备注/Memo

收稿日期:2022- 06- 28 修回日期:2022- 08- 15
基金项目:国家自然科学基金青年基金(52005385)
作者简介:张凭(1993—),男,博士,工程师,研究领域为液体火箭发动机高温组件疲劳寿命。

更新日期/Last Update: 1900-01-01