发明名称 SUPPORT AND DRIVE DEVICE OF ROTOR SHAFT
摘要 <P>PROBLEM TO BE SOLVED: To provide a device of supporting and driving a rotor of a helicopter which absorbs vibration with low frequency and comparatively high energy. <P>SOLUTION: The support and drive device of the rotor shaft includes a bearing damper which contains a plurality of fluidly communicating oil cylinders disposed around circumference of the rotor so as to dampen vibration of the rotor. The device is provided with a flexible diaphragm coupling to transmit drive torque. The device improves in capacity corresponding to off register by the flexible diaphragm coupling. <P>COPYRIGHT: (C)2007,JPO&INPIT
申请公布号 JP2006300339(A) 申请公布日期 2006.11.02
申请号 JP20060200178 申请日期 2006.07.24
申请人 PRATT & WHITNEY CANADA CORP 发明人 MITROVIC LAZAR
分类号 F16F15/023;F16H1/14;B64C27/12;B64C27/14;F16C27/04;F16C32/06;F16C35/067;F16D3/74;F16F9/14;F16F9/22;F16F15/02;F16H1/28;F16H1/48 主分类号 F16F15/023
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