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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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