发明名称 Blade hub for rotor of helicopter
摘要 The blades are attached to the hub by flexures instead of the usual hinges. The rotor mast or drive shaft (4) has a flange (3) at the top, forming the rotor head. A flexible rotor head plate (2) is bolted (V2) to the rigid rotor head. It is of cruciform shape, with the inner ends of the rotor blades (5) bolted (V1) to the ends - for a four-bladed rotor. The inner ends of the rotor blades fit over the ends (2.1,2.3) of the flexible rotor head plate (2). A flexible spider plate (1) with four arms (1.1,1.3) is fitted over the inner ends of the rotor blades, and is held by the bolts which fasten the blades to the flexible rotor head plate. The center of the cruciform spider plate is thicker than the arms.
申请公布号 DE19837802(C1) 申请公布日期 1999.10.28
申请号 DE19981037802 申请日期 1998.08.20
申请人 EUROCOPTER DEUTSCHLAND GMBH 发明人 PFALLER, RUPERT;ENENKL, BERNHARD
分类号 B64C27/32;B64C27/33;B64C27/48;(IPC1-7):B64C27/33 主分类号 B64C27/32
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