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[1]武晓欣,贾洁羽,邢理想,等.重复使用液体火箭发动机原位无损检测技术应用及展望[J].火箭推进,2024,50(01):46-56.[doi:10.3969/j.issn.1672-9374.2024.01.004]
　WU Xiaoxin,JIA Jieyu,XING Lixiang,et al.Application and prospect of in-situ nondestructive testing of reusable liquid rocket engine[J].Journal of Rocket Propulsion,2024,50(01):46-56.[doi:10.3969/j.issn.1672-9374.2024.01.004]
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重复使用液体火箭发动机原位无损检测技术应用及展望

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 50 期数: 2024年01期 页码: 46-56 栏目: 目次 出版日期: 2024-02-28
Title:
Application and prospect of in-situ nondestructive testing of reusable liquid rocket engine
文章编号:
1672-9374(2024)01-0046-11
作者:
武晓欣1; 贾洁羽2; 邢理想2; 朱安冬2; 宋澄2
1.西北工业大学,陕西 西安710072; 2.西安航天动力研究所,陕西 西安710100
Author(s):
WU Xiaoxin1;  JIA Jieyu2;  XING Lixiang2;  ZHU Andong2;  SONG Cheng2
1.Northwestern Polytechnical University, Xi'an 710072, China; 2.Xi'an Aerospace Propulsion Institute, Xi'an 710100, China
关键词:
重复使用液体火箭发动机;  原位无损检测;  智能化;  自动化
Keywords:
reusable liquid rocket engine;  in-situ NDT;  intelligence;  automation
分类号:
V43
DOI:
10.3969/j.issn.1672-9374.2024.01.004
文献标志码:
A
摘要:
重复使用航天运载器是国家战略科技的前沿,研制可重复使用液体火箭发动机成为这一趋势下的迫切需求。火箭返回后发动机是全箭重点检测和维护对象,通过无损检测技术手段在发动机原位状态下获得结构健康状态信息,快速判断产品寿命是否满足再次使用要求,对提高液体火箭发动机重复使用可靠性至关重要。综述了当前应用于航空航天领域的无损检测技术,对其在液体火箭发动机中的适用性进行了评估和分析。结合液体火箭发动机特点和重复使用无损检测应用场景,超声检测、数字图像测量、羽流光谱和快响应动态传感器等技术亟需开展研究,同时应开发自动化、智能化专用检测设备,形成快速使用维护处理与检测系统,实现液体火箭发动机便携高效、缺陷可视化和定量化等检测能力。
Abstract:
Reusable space launch vehicle is the cutting-edge of national strategic science and technology, and the development of reusable liquid rocket engines has become an urgent demand under this trend. After the rocket returns, the engine is a key inspection and maintenance object for the entire rocket. By using non-destructive testing technology to obtain structural health status information in the original state of the engine, which is crucial to quickly determine whether the product life meets the requirements for reuse and improve the reliability of liquid rocket engine reuse. The current non-destructive testing technologies applied in the aerospace field were reviewed, and their applicability in liquid rocket engines was evaluated and analyzed. Based on the characteristics of liquid rocket engines and the application scenarios of reusable non-destructive testing, there is an urgent need for research on technologies such as ultrasonic testing, digital image measurement, plume spectroscopy, and fast response dynamic sensors. At the same time, automated and intelligent specialized testing equipment should be developed to form a rapid use, maintenance, processing, and testing system, achieving portable, efficient, defect visualization, and quantification testing capabilities for liquid rocket engines.

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备注/Memo

收稿日期:2023- 06- 30 修回日期:2023- 07- 03
基金项目:国家重点实验室基金(6142704210102)
作者简介:武晓欣(1987—),男,硕士,高级工程师,研究领域为液体火箭发动机技术。

更新日期/Last Update: 1900-01-01