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 detachable pin whose withdrawal allows the folding of the blade by pivoting about the other blade pin forming a pivot pin, by holding means tied to this detachable pin, in the flight position of the blade. This section of cable is released from its holding means before the withdrawal of the latter and of the detachable blade pin, which precedes the folding, in such a way that this section of cable deforms naturally on following the pivoting of the blade. After deployment of the blade, a part of the section of cable is again held in the holding means, in the flight position of the blade.
申请公布号 US2002081202(A1) 申请公布日期 2002.06.27
申请号 US20010992683 申请日期 2001.11.19
申请人 CERTAIN NICOLAS;COISSET ERIC 发明人 CERTAIN NICOLAS;COISSET ERIC
分类号 B64C27/50;B64D15/12;(IPC1-7):F01D7/00;B64C27/39 主分类号 B64C27/50
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