发明名称 COMPOSITE MATERIAL STRUCTURE AND AIRCRAFT WING PROVIDED THEREWITH
摘要 Provided is a composite material structure enabled to be reduced in weight. The composite material structure includes a front section (3a) extending in one direction and formed as a composite material made of fiber reinforced plastics, a rear section (3c) separated from the front section (3a) by a predetermined space, extending in the one direction, and formed as a composite material made of fiber reinforced plastics, and access panels (5) provided between the front section (3a) and the rear section (3c) and having a dimension in the one direction shorter than the front section (3a) and the rear section (3c). The access panels (5) are fixed to the front section (3a) and the rear section (3c) in an orthogonal direction substantially orthogonal to the one direction and set to be displaceable in the one direction and are removable.
申请公布号 US2013216766(A1) 申请公布日期 2013.08.22
申请号 US201213881521 申请日期 2012.01.26
申请人 TANAKA YUYA;SUZUKI HIDEYUKI;KANAYAMA YUTAKA;SATO KAZUKI;HATANO MASATAKE;SAITO SATORU;WATANABE AKIHISA;ABE RYO 发明人 TANAKA YUYA;SUZUKI HIDEYUKI;KANAYAMA YUTAKA;SATO KAZUKI;HATANO MASATAKE;SAITO SATORU;WATANABE AKIHISA;ABE RYO
分类号 B64C3/26;B32B7/04 主分类号 B64C3/26
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