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¡¶»ð¼ýÍƽø¡·[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:

2024Äê01ÆÚ

Page:

12-27

Research Field:

Ä¿´Î

Publishing date:

Info

Title:

Research progress of fatigue life for the thrust chamber of reusable rocket engines

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

Keywords:

reusability;  liquid rocket engine;  regeneratively-cooled thrust chamber;  thermal-mechanical failure;  fatigue life prediction

PACS:

V434.3

DOI:

10.3969/j.issn.1672-9374.2024.01.002

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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