首页> 外国专利> Rotor carrier structure with a damper device for avoiding unstable coupling between resonant vibration modes

Rotor carrier structure with a damper device for avoiding unstable coupling between resonant vibration modes

机译:具有减震装置的转子支架结构,用于避免共振振动模式之间的不稳定耦合

摘要

A carrier structure for a rotor and a method of preventing the coupling of the vibration modes of a carrier structure of a flying machine with the vibration modes of a rotor are provided. The carrier structure has an airframe and a mounting structure suitable for being engaged with the rotor. A vibration-damper mechanism is fitted to the mounting structure and has a resonator that includes a weight element, a damper, and a first deformable member. The weight element is a flapping weight element and is carried by the mounting structure via the first deformable member. The first deformable member allows the weight element to move with respect to the mounting structure and restrains the mobility of the weight element. The damper is interposed between the weight element and the mounting structure for damping the movement of the weight element.
机译:提供了一种用于转子的支架结构以及防止飞行器的支架结构的振动模式与转子的振动模式耦合的方法。载体结构具有机身和适于与转子接合的安装结构。减振机构装配到安装结构并具有谐振器,该谐振器包括配重元件,阻尼器和第一可变形构件。配重元件是拍打配重元件,并且经由第一可变形构件由安装结构承载。第一可变形构件允许配重元件相对于安装结构移动并且限制配重元件的移动性。阻尼器插入在配重元件和安装结构之间,用于阻尼配重元件的运动。

著录项

  • 公开/公告号US8820674B2

    专利类型

  • 公开/公告日2014-09-02

    原文格式PDF

  • 申请/专利权人 PAUL CRANGA;

    申请/专利号US20100969691

  • 发明设计人 PAUL CRANGA;

    申请日2010-12-16

  • 分类号B64C27/00;

  • 国家 US

  • 入库时间 2022-08-21 16:03:26

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