首页> 外国专利> TURBOMOTOR COMPRISING A CONTROLLED MECHANICAL COUPLING DEVICE, HELICOPTER EQUIPPED WITH SUCH A TURBOMOTOR, AND METHOD OF OPTIMIZING THE SUPER-SLOWING SYSTEM WITH NULL POWER OF SUCH A HELICOPTER

TURBOMOTOR COMPRISING A CONTROLLED MECHANICAL COUPLING DEVICE, HELICOPTER EQUIPPED WITH SUCH A TURBOMOTOR, AND METHOD OF OPTIMIZING THE SUPER-SLOWING SYSTEM WITH NULL POWER OF SUCH A HELICOPTER

机译:包括受控制的机械耦合装置的涡轮机,装有这种涡轮机的直升机,以及用这种直升机的空功率优化超慢速系统的方法

摘要

The invention relates to a turbine engine comprising a gas generator (5) adapted to be rotated and a free turbine (6) driven in rotation by the gases of said gas generator, characterized in that it comprises a device (40). controlled mechanical coupling of said gas generator (5) and said free turbine (6) adapted to mechanically and commandably link said gas generator (5) and said free turbine (6) as soon as the rotational speed of said generator (5) ) gas reaches a predetermined threshold speed.
机译:涡轮发动机技术领域本发明涉及一种涡轮发动机,其包括适于旋转的气体发生器(5)和由所述气体发生器的气体驱动旋转的自由涡轮(6),其特征在于,其包括装置(40)。所述气体发生器(5)和所述自由涡轮机(6)的受控的机械联接,适于一旦所述发生器(5)的气体的转速机械地且可命令地将所述气体发生器(5)和所述自由涡轮机(6)连接起来。达到预定的阈值速度。

著录项

  • 公开/公告号FR3019223A1

    专利类型

  • 公开/公告日2015-10-02

    原文格式PDF

  • 申请/专利权人 TURBOMECA;

    申请/专利号FR20140052654

  • 申请日2014-03-27

  • 分类号F02C7/36;

  • 国家 FR

  • 入库时间 2022-08-21 14:54:08

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