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Helicopter vibration control system and circular force generation systems for canceling vibrations 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-027/00
  • F16F-015/22
  • G05D-019/02
출원번호 US-0728688 (2015-06-02)
등록번호 US-9776712 (2017-10-03)
발명자 / 주소
  • Jolly, Mark R.
  • Altieri, Russell E.
  • Badre-Alam, Askari
  • Ivers, Douglas E.
  • Swanson, Doug A.
  • Mellinger, Daniel
  • Meyers, Andrew D.
출원인 / 주소
  • LORD Corporation
대리인 / 주소
    Miller, Richard G.
인용정보 피인용 횟수 : 0  인용 특허 : 128

초록

A rotary wing aircraft including a vehicle vibration control system. The vehicle vibration control system includes a rotary wing aircraft member sensor for outputting rotary wing aircraft member data correlating to the relative rotation of the rotating rotary wing hub member rotating relative to the

대표청구항

1. A vehicle, said vehicle having a nonrotating vehicle body and a rotating machine member, said vehicle including a vehicle vibration control system, said vehicle vibration control system including a vehicle vibration control system controller,a vehicle rotating machine member sensor for inputting

이 특허에 인용된 특허 (128)

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