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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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