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[1]谭永华,赵剑,张武昆,等.融合增材制造的液体火箭发动机创新设计方法与应用[J].火箭推进,2023,49(04):1-16.
　TAN Yonghua,ZHAO Jian,ZHANG Wukun,et al.Innovative design method and application of liquid rocket engine integrated additive manufacturing[J].Journal of Rocket Propulsion,2023,49(04):1-16.
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融合增材制造的液体火箭发动机创新设计方法与应用

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 49 期数: 2023年04期 页码: 1-16 栏目: 目次 出版日期: 2023-08-25
Title:
Innovative design method and application of liquid rocket engine integrated additive manufacturing
文章编号:
1672-9374(2023)04-0001-16
作者:
谭永华1; 2; 3; 赵剑3; 张武昆3; 王珺3; 高玉闪3
(1.中国航天科技集团有限公司,北京 100048; 2.航天推进技术研究院,陕西 西安 710100; 3.西安航天动力研究所 液体火箭发动机技术重点实验室,陕西 西安 710100)
Author(s):
TAN Yonghua1; 2; 3;  ZHAO Jian3;  ZHANG Wukun3;  WANG Jun3;  GAO Yushan3
(1.China Aerospace Science and Technology Corporation, Beijing 100048, China; 2.Academy of Aerospace Propulsion Technology, Xi'an 710100, China; 3.Science and Technology on Liquid Rocket Engine Laboratory,Xi'an Aerospace Propulsion Institute, Xi'an 710100, China)
关键词:
液体火箭发动机;  增材制造;  融合创新设计;  结构功能一体化;  轻量化
Keywords:
liquid rocket engine;  additive manufacturing;  integrated innovative design;  combined structural and functional performance;  lightweight
分类号:
V43
文献标志码:
A
摘要:
增材制造技术在液体火箭发动机中应用的广度和深度不断增强。在发动机的设计层面,经历了由最初的“原位制造替代”到中间的“制造驱动设计”,再到“设计引领制造”3个设计理念阶段的变革。对融合增材制造的液体火箭发动机创新设计方法和准则进行了总结,包括结构优化设计技术、结构与功能一体化设计技术、复杂组件集成技术和基于增材制造工艺约束与材料性能的设计技术。以常平环和换热器等在发动机增材制造中应用很广泛的典型承载和热力组件为例,介绍了融合增材制造后产品的具体创新设计思路。对融合增材制造的液体火箭发动机创新设计方法和发展方向进行了总结与讨论。
Abstract:
The application of additive manufacturing(AM)technology in liquid rocket engine is increasingly extensive and deep. At the design level of the engine, it has undergone three design concept stages:from the initial “in-situ manufacturing substitution” to the “manufacturing-driven design”, and then to “design-led manufacturing”. The innovative design methods and criteria of liquid rocket engine for AM are summarized, including structural optimization design technology, structural and functional integration design technology, complex component integration technology and process constraints and material performance design technology based on AM.Taking some typical thermal and bearing components as examples, such as the gas generator injector, heat exchanger and so on, which are widely used in engine, the specific innovative design ideas of the product after combining AM are introduced. The innovative design methods and development directions of liquid rocket engine by AM are summarized and discussed.

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备注/Memo

收稿日期:2023-02-16; 修回日期:2023-04-08
基金项目:国家液体火箭发动机重点实验室基金项目(6142704220401,6142704210403,6142704220403)
作者简介:谭永华(1967—),男,博士,研究员,研究领域为液体火箭发动机技术。

更新日期/Last Update: 1900-01-01