发明名称 Actuation system, helicopter using the same, and controlling method therefor
摘要 An actuation system includes a pump assembly configured to form a pump chamber; an actuator having first and second chambers and a movable member and configured to convert pressures applied to the first and second chambers into a movement of the movable member; and a valve section. A controller controls the valve section to open a first flow path between the pump chamber and the first chamber and close a second flow path between the pump chamber with the second chamber, during a discharge period during which the pump chamber is pressurized, in a first mode; to close the first flow path and open the second flow path during an intake period during which the pump chamber is depressurized, in the first mode; to close the first flow path and open the second flow path during the discharge period in a second mode; and to open the first flow path and close the second flow path during the intake period in the second mode.
申请公布号 US2008304967(A1) 申请公布日期 2008.12.11
申请号 US20080153889 申请日期 2008.05.27
申请人 MORI SHIGEYUKI;SAITO HIROSHI;NAKAYAMA SHUICHI;SHIMOYAMA KUNIMITSU 发明人 MORI SHIGEYUKI;SAITO HIROSHI;NAKAYAMA SHUICHI;SHIMOYAMA KUNIMITSU
分类号 B64C11/32 主分类号 B64C11/32
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