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특허 상세정보

Aircraft skin lap splice

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-001/12   
미국특허분류(USC) 244/132 ; 244/131 ; 403/41
출원번호 US-0933255 (1992-08-21)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 38  인용 특허 : 0
초록

Fuselage skin lap splice for aircraft formed of metal or composite skin panels. The adjacent skin panels comprise an outer skin and an inner skin, having contacting overlapping longitudinal edge portions, and a plurality of fasteners connecting such overlapping edge portions. A plurality of outwardly extending fingers are integrally connected along the edge portion of the inner skin and at least one longitudinal row of fasteners passes through the fingers and connects the outer skin and the fingers. Preferably the fingers are lollipopped, that is, have o...

대표
청구항

In a skin lap splice between adjacent skin panels of aircraft which comprises an outer skin having a longitudinal edge portion and an inner skin having a longitudinal edge portion, said edge portions being in contact and overlapping, and a plurality of first longitudinal rows of fasteners connecting said edge portions; the improvement which comprises means on said inner skin adjacent the longitudinal edge portion thereof and forming a part of said inner skin to provide flexibility at said longitudinal edge portion of said inner skin, and at least one sec...

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  29. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G.. Splice joints for composite aircraft fuselages and other structures. USP2014108869403.
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