首页> 外国专利> Jet engines and gas turbine engines in which the compression rotary blades rotate in opposite directions and the combustion discharge rotary blades rotate in reverse respectively to strenn the compression and intensify combustion,

Jet engines and gas turbine engines in which the compression rotary blades rotate in opposite directions and the combustion discharge rotary blades rotate in reverse respectively to strenn the compression and intensify combustion,

机译:喷气发动机和燃气涡轮发动机,其中压缩旋转叶片朝相反的方向旋转,而燃烧排放旋转叶片分别反向旋转,以加强压缩并增强燃烧,

摘要

PROBLEM TO BE SOLVED: To provide a powerful jet engine not consuming fuel more than necessary.SOLUTION: A high-power jet engine is produced by reversely turning the compression revolution blades of a jet engine and a gas turbine engine individually backward so that the compressibility of air is enhanced to intensify the combustion of a fuel thereby to enhance combustion discharge.
机译:解决的问题:提供一种功能强大的喷气发动机,而不消耗过多的燃料。解决方案:通过使喷气发动机和燃气涡轮发动机的压缩旋转叶片分别反向旋转以产生可压缩性,从而生产出大功率喷气发动机。空气的燃烧被增强以增强燃料的燃烧,从而增强燃烧排放。

著录项

  • 公开/公告号JP6166201B2

    专利类型

  • 公开/公告日2017-07-19

    原文格式PDF

  • 申请/专利权人 竹田 眞司;

    申请/专利号JP20140050915

  • 发明设计人 竹田眞司;

    申请日2014-03-13

  • 分类号F02C3/067;F02K3/072;

  • 国家 JP

  • 入库时间 2022-08-21 13:56:37

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