发明名称 Rotary-wing aircraft rotors with manually folding blades and electrical connection installation
摘要 On the rotor, between each blade and the member for linking with the hub, an electrical connecting cable comprises a first section of which one part is held above that one of the two blade pins which is the pivot pin about which the blade can be folded by pivoting, once the other blade pin has been removed. This holding is provided by a cradle formed in a cable support connected to the pivot pin, and by a collar articulated to one edge of the cradle and which can be folded down into the closed position onto the opposite edge of the cradle, to which this collar can be connected detachably by at least one detachable retaining element. The section of cable is manually released from the collar and from the cradle before the removal of the removable pin, which precedes folding, so that this section of cable deforms naturally, following the pivoting of the blade. While the blade has been deployed, the releasable part of this section is once again retained in the cradle above the pivot pin by the closing of the collar.
申请公布号 US2002081201(A1) 申请公布日期 2002.06.27
申请号 US20010992355 申请日期 2001.11.19
申请人 MONDET JEAN;MAZET STEPHANE 发明人 MONDET JEAN;MAZET STEPHANE
分类号 B64C27/50;B64D15/12;(IPC1-7):B64C27/39;F01D7/00 主分类号 B64C27/50
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