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특허 상세정보

Split spiroid

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-023/06   
출원번호 US-0719925 (2015-05-22)
등록번호 US-9434470 (2016-09-06)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Rutan & Tucker, LLP
인용정보 피인용 횟수 : 0  인용 특허 : 61
초록

The spiroid wing tip according to embodiments of the invention including a continuous segmental assembly having a closed loop frontal profile comprising a lower near vertical segment, a horizontal segment, a vertical segment, a second horizontal upper segment, and a near vertical segment. Accordingly to some embodiments of the invention, the spiroid profile is lowered with respect to the wing chord plane, such that a portion of the spiroid wing tip extends below the wing chord plane.

대표
청구항

1. A spiroid wing tip designed for attachment to an aircraft wing having an aircraft wing leading edge and an aircraft wing trailing edge, the spiroid wing tip comprising: an enclosed loop, comprising: a beginning section including a leading edge generally continuous with the aircraft wing leading edge;an ending section having a trailing edge swept rearward with respect to the aircraft wing trailing edge; andmiddle section between the beginning section and the ending section, the middle section including a portion extending above a chord plane of the air...

이 특허에 인용된 특허 (61)

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