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Aircraft reciprocating engine supercharging system, aircraft reciprocating engine and aircraft

机译:飞机往复式发动机增压系统,飞机往复式发动机及飞机

摘要

There is provided a supercharging system for an aircraft reciprocating engine, comprising: a plurality of compressors for supplying compressed air to the aircraft reciprocating engine; at least one turbine for obtaining rotational power for at least one of the plurality of compressors, and a plurality of motors for respectively providing rotational power to the plurality of compressors. An object of the present invention is to reduce turbo lag in a reciprocating engine for an aircraft in which multiple-stage supercharging is performed by the turbocharger.
机译:提供了一种用于飞机往复式发动机的增压系统,包括:多个压缩机,用于将压缩空气供应到飞机往复式发动机;用于获得多个压缩机中的至少一个的旋转功率的至少一个涡轮机,以及分别向多个压缩机提供旋转功率的多个电动机。本发明的目的是减少用于飞机的往复式发动机中的涡轮迟滞,在该飞机中,通过涡轮增压器执行多级增压。

著录项

  • 公开/公告号JP6655640B2

    专利类型

  • 公开/公告日2020-02-26

    原文格式PDF

  • 申请/专利权人 株式会社SUBARU;

    申请/专利号JP20180036410

  • 发明设计人 小谷 和彰;中里 展之;村田 巌;

    申请日2018-03-01

  • 分类号F02B37/04;B64D27/24;B64D27/04;F02D23;

  • 国家 JP

  • 入库时间 2022-08-21 11:32:22

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