首页> 外国专利> Twin-spool turbine for aircraft, has electrical generators driven through differential gear having two planet wheels driven by high and low pressure rotor shafts of high and low pressure bodies, and planet gear driven by wheels

Twin-spool turbine for aircraft, has electrical generators driven through differential gear having two planet wheels driven by high and low pressure rotor shafts of high and low pressure bodies, and planet gear driven by wheels

机译:用于飞机的双转子涡轮,具有通过差速器齿轮驱动的发电机,该差速器齿轮具有由高低压体的高低压转子轴驱动的两个行星轮,以及由齿轮驱动的行星轮

摘要

The turbine has electrical generators driven through a differential gear (30) having two planet wheels (31`, 32`) driven by high and low pressure rotor shafts (1, 2) of high and low pressure bodies. The wheels drive a planet gear (33) mounted in a casing (36). Transmission ratios between respective shafts and wheels are such that distribution of power between the bodies lies between 80 by 20 percent.
机译:该涡轮机具有通过差速器齿轮(30)驱动的发电机,该差速器齿轮具有两个行星齿轮(31`,32`),该两个行星齿轮由高压和低压体的高压和低压转子轴(1、2)驱动。车轮驱动安装在壳体(36)中的行星齿轮(33)。各个轴和车轮之间的传动比应使车身之间的动力分配在80%到20%之间。

著录项

  • 公开/公告号FR2863312A1

    专利类型

  • 公开/公告日2005-06-10

    原文格式PDF

  • 申请/专利权人 SNECMA MOTEURS;

    申请/专利号FR20030014429

  • 发明设计人 LARDELLIER ALAIN;

    申请日2003-12-09

  • 分类号F02C7/36;

  • 国家 FR

  • 入库时间 2022-08-21 21:58:20

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