发明名称 |
Blade and method for manufacturing said blade |
摘要 |
<p>The blade has a twisting force transmission element (40) provided with half-shells (41, 42) that surround an attachment zone (21) of a spar of an airfoil element. Each half-shell has a first set of portions (43', 43'') providing visual access to a centrifugal force transmission bushing when the airfoil element is removed from a fitting and a second set of portions (44', 44'') co-operated with a torsion box surrounding a distal zone of the spar. The transmission element is secured to the fitting in rotation around a torsion axis of the blade. An independent claim is also included for a method for fabricating a blade.</p> |
申请公布号 |
EP2481670(A1) |
申请公布日期 |
2012.08.01 |
申请号 |
EP20120000518 |
申请日期 |
2012.01.26 |
申请人 |
EUROCOPTER |
发明人 |
BIANCHI, LAURENT;GAFFIERO, JACQUES;MICHEL, BERNARD;ISIDORE, NICOLAS |
分类号 |
B64C11/26;B64C27/48 |
主分类号 |
B64C11/26 |
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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