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
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
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