首页> 外国专利> Combustor mixing head for liquid rocket engine comprising vertical separate plate and horizontal separate plate

Combustor mixing head for liquid rocket engine comprising vertical separate plate and horizontal separate plate

机译:用于液体火箭发动机的燃烧器混合头,包括垂直分隔板和水平分隔板

摘要

The present invention relates to a liquid rocket engine combustor head having vertical and horizontal separation plate separating plate , more specifically in the combustor head for liquid rocket engine is installed on the inlet side of the oxidant , the oxidant is a plurality of domes and the junction hole is formed in the distribution plate and perpendicular to the cylindrical inlet oxidant is passed through an oxidizer inlet; Surrounding the outer circumferential surface of the vertical separating plate provided with a horizontal separation plate of a plurality of disk-like holes are formed to the inlet oxidant is passed through the oxidant inlet . ; According to the present invention , LRE it is possible to prevent damage due to the increase in the local heat flux by the wall of the combustor to the oxidant is evenly distributed to the side of the inlet for the burner head .
机译:具有垂直和水平分隔板分隔板的液体火箭发动机燃烧器头技术领域本发明涉及一种具有垂直和水平分隔板分隔板的液体火箭发动机燃烧器头,更具体地讲,用于液体火箭发动机的燃烧器头安装在氧化剂的入口侧,氧化剂是多个圆顶和连接处在分配板上形成孔,垂直于圆柱形入口的氧化剂通过氧化剂入口。垂直分隔板的外周表面围绕设置有多个圆盘状孔的水平分隔板而形成,入口氧化剂穿过氧化剂入口。 ;根据本发明,LRE可以防止由于燃烧器的壁对氧化剂的局部热通量的增加而引起的损坏,该局部热通量均匀地分布在燃烧器头的入口侧。

著录项

  • 公开/公告号KR100925540B1

    专利类型

  • 公开/公告日2009-11-05

    原文格式PDF

  • 申请/专利权人

    申请/专利号KR20080022151

  • 申请日2008-03-10

  • 分类号F02K9/62;F02K9/60;F02K9/42;

  • 国家 KR

  • 入库时间 2022-08-21 19:11:33

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