发明名称 Modular foil
摘要 The modular foil includes a wing and a fuselage extending in a longitudinal direction and bearing the wing. The fuselage includes a central segment, a first segment bearing a first portion of the wing, and being removable from the central segment, and an assembling device to connect the central segment with the first segment in the longitudinal direction. The central segment and the first segment are connected end to end. The assembling device includes a pair formed by a male connector and a female connector cooperating through a specific interlocking. The male connector includes at least one outer inclined wall, complementary and cooperating with an internal inclined wall born by the female connector for an optimal interlocking between the central segment and the first segment. There is a locking device along the longitudinal axis of the fuselage ensuring locking in at least one direction of the longitudinal axis.
申请公布号 US9278739(B2) 申请公布日期 2016.03.08
申请号 US201514701268 申请日期 2015.04.30
申请人 F. ONE 发明人 Salles Raphael
分类号 B63B1/24;B63B35/79;B63B35/71 主分类号 B63B1/24
代理机构 Craft Chu PLLC 代理人 Chu Andrew W.;Craft Chu PLLC
主权项 1. Foil comprising: a wing, having a first portion and a second portion; and a fuselage extending in a longitudinal direction and bearing said wing, said fuselage comprising: a central segment;a first segment bearing said first portion of said wing and being removable from said central segment; andassembling means for said central segment and said first segment in said longitudinal direction, wherein said central segment and said first segment are connected end to end by the assembling means, said assembling means comprising a pair formed by a male connector and a female connector cooperating through a specific interlocking, male and female connectors being located at a central segment extremity and at a first segment extremity, wherein said male connector comprises at least one outer inclined wall, being complementary and cooperating with an internal inclined wall born by said female connector, said outer inclined wall of said male connector and said internal inclined wall of said female connector providing an interlocking between said central segment and said first segment, further comprising: locking means, extending along said longitudinal axis of said fuselage and cooperating with said male connector and said female connector the male and female connectors being locked in at least one direction of said longitudinal axis.
地址 Perols FR