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大推力氢氧发动机关键制造技术 被引量:9

Key manufacturing technology for large thrust LH_(2)/LOX cycle engine
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摘要 为了满足大推力、大尺寸220 tf补燃循环氢氧发动机的研制需求,针对补燃氢氧发动机推力室、预燃室、涡轮泵、阀门、管路等组合件,开展大推力氢氧发动机的工艺技术攻关,采用旋压成形、扩散钎焊、惯性摩擦焊、增材制造、粉末冶金、精密铸造等工艺技术,实现了220 tf补燃循环氢氧发动机复杂构件的制造;针对220 tf补燃循环氢氧发动机超大、超重零部组件,开展高精密装配技术研究,采用自动化装配、数字化装配及自动测量与定位等工艺技术,实现了超大超重零部组件的精密装配。通过工艺技术研究,研制出首台220 tf补燃循环氢氧发动机工程样机,提高了我国氢氧发动机整体制造水平,满足了我国新一代运载火箭的研制需求。 In order to meet the needs of large thrust and large size 220 tf staged combustion cycle LH_(2)/LOX engine,the research on process and technology of LH_(2)/LOX engine was carried out for thrust chamber,precombustion chamber,turbopump,valve,pipeline and other systems of LH_(2)/LOX engine.The key components of 220 tf staged combustion cycle LH_(2)/LOX engine were manufactured by using spinning forming,diffusion brazing,inertia friction welding,additive manufacturing,powder metallurgy and precision casting and other processes.The research on high precision assembly technology was carried out for the large and heavy components of the 220 tf thrust LH_(2)/LOX staged combustion cycle engine,the precision assembly of the large and heavy components was realized by using automatic assembly,digital assembly,automatic measurement,positioning and other process.Through the process and technology research,the first engineering prototype of 220 tf high-pressure staged combustion cycle LH_(2)/LOX engine was successfully developed,which improved the overall manufacturing level of LH_(2)/LOX engine and met the development requirements of a new generation of launch vehicle.
作者 孙纪国 何学青 阳代军 郑孟伟 徐坤和 SUN Jiguo;HE Xueqing;YANG Daijun;ZHENG Mengwei;XU Kunhe(Beijing Aerospace Propulsion Institute, Beijing 100076, China;Capital Aerospace Machinery Corporation Limited, Beijing 100076, China)
出处 《火箭推进》 CAS 2022年第2期117-126,共10页 Journal of Rocket Propulsion
基金 国家自然科学基金(U1537212)。
关键词 新一代运载火箭 氢氧发动机 关键制造技术 精密装配 工程样机 a new generation of launch vehicle LH_(2)/LOX engine key manufacturing technology precision assembly engineering prototype
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