发明名称 CONSTANT SPEED TRANSMISSION ROTOR FOR AIRCRAFT
摘要 PROBLEM TO BE SOLVED: To provide a rotor for an aircraft having a constant speed transmission. SOLUTION: The rotor for the aircraft has a drive shaft 2 and many blades 3 and a constant speed transmission 5 connecting the blades to the shaft. The transmission has a hub 4; a driving member 6 integrated with the shaft; a driven member 7 integrated with the hub; and many torque transmitters 11. Each torque transmitter is connected to a first attachment 56 and a second attachment 57. The first attachment and the second attachment are respectively held by the driving member and the driven member.
申请公布号 JP2002337796(A) 申请公布日期 2002.11.27
申请号 JP20020026961 申请日期 2002.02.04
申请人 AGUSTA SPA 发明人 CARAMASCHI VITTORIO
分类号 B64C27/22;B64C27/32;B64C27/35;B64C29/02;B64D35/04;(IPC1-7):B64D35/04 主分类号 B64C27/22
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