发明名称 PROPELLER BLADE; BLADE FOR HELICOPTER TAIL ROTOR IN PARTICULAR
摘要 attachment units for securing propeller blades to hub. SUBSTANCE: blade for helicopter tail rotor has inner recess in root. Device for connecting the root of blade to rotor hub has rigid rod and flexible stop consisting of many laminar members located between two members of reinforcement in such way that stop may work as ball joint of limited action centered relative to axis of change of pitch. Rigid rod connects flexible stop with rotor hub inside blade root. EFFECT: reduced torsion loads at low radial overall dimensions of rotor hub. 14 cl, 6 dwg
申请公布号 RU2190559(C2) 申请公布日期 2002.10.10
申请号 RU19990127298 申请日期 1999.03.16
申请人 MUJ RENE 发明人 MUJ RENE
分类号 B64C27/82;B64C27/35;B64C27/45;B64C27/48;(IPC1-7):B64C27/35 主分类号 B64C27/82
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