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특허 상세정보

MyON담기
내보내기 페이스북 공유 카카오톡 공유

Rotorcraft autopilot system, components and methods

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-027/68    B64C-013/18    B64C-027/57    B64C-013/30   
출원번호 US-0415469 (2017-01-25)
등록번호 US-10059441 (2018-08-28)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Pritzkau Patent Group LLC
인용정보 피인용 횟수 : 0  인용 특허 : 41
초록
▼

An autopilot actuator includes first and second motors each including a rotatable motor output shaft such that either one or both of the motors can drive an actuator output shaft. An autopilot main unit enclosure is removably mounted to the helicopter proximate to a cyclic control and commonly houses autopilot actuators as well as main autopilot electronics. A cyclic vibration isolator is removably supported by an actuator shaft for co-rotation and coupled to the cyclic control to attenuate a cyclic vibration frequency at the actuator shaft while output ...

대표
청구항
▼

1. An autopilot system for a helicopter, comprising: an autopilot display unit that is mounted in an instrument console of the helicopter at least for displaying autopilot flight data to a pilot of the helicopter;an autopilot main unit enclosure that is removably mounted to the helicopter proximate to a cyclic control of the helicopter and which defines a main unit interior;a set of actuators supported within the main unit interior including a pitch actuator having a pitch actuator output shaft and a roll actuator having a roll actuator output shaft such...

이 특허에 인용된 특허 (41)

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