首页> 外国专利> Method and device for we shall now describe the defects of at least one rotor of a 371 a rotary wing, in particular a helicopter, and for adjust this rotor

Method and device for we shall now describe the defects of at least one rotor of a 371 a rotary wing, in particular a helicopter, and for adjust this rotor

机译:现在,我们将描述方法和装置,该装置将描述371旋翼,尤其是直升机的至少一个旋翼的缺陷,并调整该旋翼

摘要

A first reference helicopter, without any faults, has its rotors (6,10) adjusted to minimize vibration, then a first series of measurements are made to create a neuronal network of the relationships between accelerations representative of vibrations and adjustment parameters. Then the neuronal network is used with a further helicopter to detect possible defects and adjust the operating parameters to minimize rotor vibrations. An Independent claim is included for a device for detecting faults in helicopter rotors.
机译:第一架参考直升机,没有任何故障,对其转子(6,10)进行了调整,以使振动最小化,然后进行第一系列测量,以创建代表振动的加速度与调整参数之间的关系的神经网络。然后,神经网络与另一架直升飞机一起使用,以检测可能的缺陷并调整运行参数,以使转子振动最小化。包括用于检测直升机旋翼中的故障的设备的独立权利要求。

著录项

  • 公开/公告号FR2824395B1

    专利类型

  • 公开/公告日2004-09-10

    原文格式PDF

  • 申请/专利权人 EUROCOPTER;

    申请/专利号FR20020003312

  • 发明设计人 ROGELIO FERRER;

    申请日2002-03-18

  • 分类号G01H1/00;G01M17/00;G06F15/76;B64C27/32;

  • 国家 FR

  • 入库时间 2022-08-21 22:39:42

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