首页> 外国专利> REGULATION SYSTEM FOR CONTROLLING THE VIBRATORY BEHAVIOR AND/OR THE TWISTING STABILITY OF A DRIVETRAIN, A ROTORCRAFT FITTED WITH SUCH A REGULATION SYSTEM, AND AN ASSOCIATED REGULATION METHOD

REGULATION SYSTEM FOR CONTROLLING THE VIBRATORY BEHAVIOR AND/OR THE TWISTING STABILITY OF A DRIVETRAIN, A ROTORCRAFT FITTED WITH SUCH A REGULATION SYSTEM, AND AN ASSOCIATED REGULATION METHOD

机译:用于控制动力传动系统的振动行为和/或扭转稳定性的调节系统,装有这种调节系统的旋翼机以及相关的调节方法

摘要

A regulation system for controlling the vibratory behavior in twisting and/or the twisting stability of a drivetrain of a rotorcraft, the regulation system comprising two regulation loops that are interleaved one in the other, the two regulation loops being arranged “in cascade” relative to each other to regulate firstly a first speed of rotation NG of a gas generator of at least one turboshaft engine driving said drivetrain in rotation, and secondly a second speed of rotation NTL of a free turbine of the engine(s).
机译:一种用于控制旋翼飞行器的动力系的扭转和/或扭转稳定性中的振动行为的调节系统,该调节系统包括彼此交错的两个调节环,两个调节环相对于“级联”布置。彼此调节以首先调节驱动所述动力传动系统旋转的至少一个涡轮轴发动机的气体发生器的第一转速NG,其次调节发动机的自由涡轮的第二转速NTL。

著录项

  • 公开/公告号US2018370620A1

    专利类型

  • 公开/公告日2018-12-27

    原文格式PDF

  • 申请/专利权人 AIRBUS HELICOPTERS;

    申请/专利号US201816007473

  • 发明设计人 ANTHONY LEONARD;

    申请日2018-06-13

  • 分类号B64C27;B64D31/06;B64D35/02;F02C9/28;

  • 国家 US

  • 入库时间 2022-08-21 12:08:38

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