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특허 상세정보

Air vehicle flight mechanism and control method for non-sinusoidal wing flapping

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-033/02    B64C-039/00   
출원번호 US-0581976 (2017-04-28)
등록번호 US-10065737 (2018-09-04)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Yedidsion, Pejman
인용정보 피인용 횟수 : 0  인용 특허 : 55
초록

A flapping wing driving apparatus includes at least one crank gear capstan rotatably coupled to a crank gear, the at least one crank gear capstan disposed radially offset from a center of rotation of the crank gear; a first wing capstan coupled to a first wing, the first wing capstan having a first variable-radius drive pulley portion; and a first drive linking member configured to drive the first wing capstan, the first drive linking member windably coupled between the first variable-radius drive pulley portion and one of the at least one crank gear cap...

대표
청구항

1. A flapping wing method, comprising: rotating a crank capstan about an axis of rotation; andpulling a first drive cable with the crank capstan, the first drive cable windably coupled to a variable-radius drive pulley portion fixed on a rotatable first wing capstan to cause the rotatable first wing capstan to rotate, the rotatable first wing capstan coupled to a first wing;wherein the first wing capstan is configured to non-constantly, angularly rotate responsive to a constant angular rotation of the crank capstan. 2. The method according to claim 1, fu...

이 특허에 인용된 특허 (55)

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