发明名称 |
Helicopter rear rotor blade mounting assembly |
摘要 |
The rear rotor blade comprises a root (3) rotating in the rotor hub (4E) enabling the blade to rotate around its pitch axis (P-P). A torsionally deformable resilient fastener attaches the root to the hub. The blade root is hollow so as to comprise an internal cavity (12). The fastener comprises a stop (15) housed in the cavity acting as a limited ball joint centered on the pitch axis. A rigid tie rod (6) connects the stop to the rotor hub
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申请公布号 |
FR2775951(A1) |
申请公布日期 |
1999.09.17 |
申请号 |
FR19980003172 |
申请日期 |
1998.03.16 |
申请人 |
MOUILLE RENE |
发明人 |
MOUILLE RENE |
分类号 |
B64C27/82;B64C27/35;B64C27/45;B64C27/48;(IPC1-7):B64C27/48 |
主分类号 |
B64C27/82 |
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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