发明名称 BLADE AND METHOD OF FABRICATING SAID BLADE
摘要 <p>PURPOSE: A blade and a manufacturing method thereof are provided to obtain optimal strength and to make a part for connecting to a hub to be exposed. CONSTITUTION: A blade comprises a coupling part, an airfoil element, and a torsion force transmission member(40). The airfoil element has a spar longitudinally extended from an attachment part(21) toward the end part. The attachment part surrounds a centrifugal force transmission bushing with a through-pin. The torsion force transmission member comprises a first half shell(41) and a second half shell(42). The first and second half shells surround the attachment part.</p>
申请公布号 KR20120088579(A) 申请公布日期 2012.08.08
申请号 KR20120008568 申请日期 2012.01.27
申请人 EUROCOPTER 发明人 BIANCHI LAURENT;ISIDORE NICOLAS;GAFFIERO JACQUES;MICHEL BERNARD
分类号 B64C11/20;B21K3/04;B64C11/26 主分类号 B64C11/20
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