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특허 상세정보

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내보내기 페이스북 공유 카카오톡 공유

Rotatable control surface assembly for an unmanned aerial vehicle

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/38    B64C-009/06    B64C-009/36    B64C-039/02   
출원번호 US-0014399 (2016-02-03)
등록번호 US-10124880 (2018-11-13)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Withrow & Terranova, PLLC
인용정보 피인용 횟수 : 0  인용 특허 : 42
초록
▼

A control surface assembly for an unmanned aerial vehicle (UAV) is disclosed. The control surface assembly has a fin configured to be rotatably coupled to a fuselage of the UAV, with a control surface member rotatably coupled to the fin. A control surface linkage is configured to be coupled between the control surface member and an actuator disposed in the fuselage. The fin is rotatable with respect to the fuselage between a stowed configuration and a deployed configuration. In the deployed configuration, the control surface linkage is configured to rota...

대표
청구항
▼

1. A control surface assembly for an unmanned aerial vehicle (UAV) comprising: a fin configured for rotatable coupling to a fuselage, the fin rotatable between a stowed configuration and a deployed configuration;a control surface member rotatably coupled to the fin; anda control surface linkage coupled to the control surface member, the control surface linkage configured for actuation by an actuator disposed in the fuselage, wherein: in the deployed configuration, the control surface linkage is configured to rotate the control surface member with respect...

이 특허에 인용된 특허 (42)

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