发明名称 STEERING SYSTEM AND AIRCRAFT
摘要 PROBLEM TO BE SOLVED: To provide a steering system allowing less flutter of a steering wing with respect to a base than conventional. SOLUTION: The steering system comprises a plurality of actuation systems including an actuation system 120 having a mode selector valve 133 provided with a plurality of ports for selecting a mode with the change of a communicating condition between the ports. A different communicating condition exists between the communicating condition adopted by the mode selector valve 133 of the actuation system 120 out of the plurality of actuation systems and the communicating condition adopted by the mode selector valve of at least one of other actuation systems. COPYRIGHT: (C)2004,JPO
申请公布号 JP2004042823(A) 申请公布日期 2004.02.12
申请号 JP20020204310 申请日期 2002.07.12
申请人 TS CORPORATION 发明人 KAMIMURA TOSHIO;ITO KOJI
分类号 B64C13/16;B64C13/00;F15B20/00;(IPC1-7):B64C13/16 主分类号 B64C13/16
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