发明名称 Rotor blade in flat design
摘要 A rotor blade (1), in particular of a main rotor of a rotary-wing aircraft, made of fibre-reinforced plastic comprising a blade section (10) and a connecting section (12) for fastening the rotor blade (1) to a drive device (18) which comprises a sleeve-shaped connecting device (14), is further developed in that the connecting device (14) comprises flat fibre layers (S1 to S18) running substantially in the plane of extension of the connecting section (12).
申请公布号 KR101199456(B1) 申请公布日期 2012.11.09
申请号 KR20100047418 申请日期 2010.05.20
申请人 发明人
分类号 B29C70/10;B29C70/20;B64C27/46;B64C27/473 主分类号 B29C70/10
代理机构 代理人
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