首页> 外国专利> Turbofan engine for combustion chamber of turbine, has fuel-air-mixture that is introduced in flow direction towards compressor in core flow, where combustion chamber is supplied with core flow and is combusted in explosive manner

Turbofan engine for combustion chamber of turbine, has fuel-air-mixture that is introduced in flow direction towards compressor in core flow, where combustion chamber is supplied with core flow and is combusted in explosive manner

机译:用于涡轮机燃烧室的涡轮风扇发动机,具有燃料-空气混合物,该燃料-空气混合物在堆芯流中沿流向被引入压缩机,在燃烧室中,堆芯被供应并以爆炸性方式燃烧

摘要

The turbofan engine has a fuel-air-mixture that is introduced in flow direction towards a compressor (05) in a core flow, where a combustion chamber (16) is supplied with the core flow and is combusted in an explosive manner. The combustion chamber is arranged in a boiler (22) in a sectional manner and has an evaporation space, in which the water mist is generated and is vaporized to cool the wall of the combustion chamber.
机译:涡轮风扇发动机具有燃料-空气混合物,该燃料-空气混合物在堆芯中沿流动方向朝着压缩机(05)引入,其中燃烧室(16)被提供有堆芯并以爆炸性方式燃烧。燃烧室以分段的方式布置在锅炉(22)中,并具有蒸发空间,在该蒸发空间中产生水雾并使其汽化以冷却燃烧室的壁。

著录项

  • 公开/公告号DE102013112506A1

    专利类型

  • 公开/公告日2014-04-03

    原文格式PDF

  • 申请/专利权人 GRAETZER MARCO;

    申请/专利号DE201310112506

  • 发明设计人 GRAETZER MARCO;

    申请日2013-11-13

  • 分类号F02C3/30;F02K7/02;F02K3/04;F23R7;F02C7/16;

  • 国家 DE

  • 入库时间 2022-08-21 15:37:21

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