首页> 外国专利> Injection element for a rocket engine comprises an inner element with a first outlet opening provided with a unit for splitting a fuel component into at least two media streams

Injection element for a rocket engine comprises an inner element with a first outlet opening provided with a unit for splitting a fuel component into at least two media streams

机译:用于火箭发动机的喷射元件包括具有第一出口的内部元件,该第一出口设有用于将燃料成分分成至少两个介质流的单元

摘要

Injection element (1) comprises an inner element (2) with a first outlet opening provided with a unit (9) for splitting a fuel component into at least two media streams. Preferred Features: The unit for splitting the medium flowing through the first outlet opening is formed by a plate (10) which closes the first outlet opening and has holes (11, 12). The plate has a central hole which is surrounded by further holes in the plate.
机译:喷射元件(1)包括具有第一出口的内部元件(2),该第一出口设有用于将燃料成分分成至少两个介质流的单元(9)。优选特征:用于分离流过第一出口的介质的单元由板(10)形成,该板封闭第一出口并且具有孔(11、12)。该板具有中心孔,该中心孔被板上的其他孔包围。

著录项

  • 公开/公告号DE102005049686A1

    专利类型

  • 公开/公告日2007-04-19

    原文格式PDF

  • 申请/专利权人 EADS SPACE TRANSPORTATION GMBH;

    申请/专利号DE20051049686

  • 发明设计人 MAEDING CHRIS UDO;HAGEMANN GERALD;

    申请日2005-10-14

  • 分类号F02K9/52;

  • 国家 DE

  • 入库时间 2022-08-21 20:29:41

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