发明名称 |
Hydraulic actuator system for aircraft |
摘要 |
A hydraulic actuator system 1 is provided for driving a movable portion attached to a wing 5 of an airplane. A plurality of first system hydraulic actuators 2 and a plurality of second system hydraulic actuators 3 are included and are connected to the movable portion. The first system hydraulic actuators 2 are attached to the wing 5 and connected to a first hydraulic pressure source, whereas the second system hydraulic actuators 3 are attached to the wing to be in parallel to the first system hydraulic actuators 2 and are connected to a second hydraulic pressure source. The first system hydraulic actuators 2 and the second system hydraulic actuators 3 are alternately provided at a predetermined part of the wing 5.
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申请公布号 |
EP2476613(A2) |
申请公布日期 |
2012.07.18 |
申请号 |
EP20120151009 |
申请日期 |
2012.01.13 |
申请人 |
NABTESCO CORPORATION |
发明人 |
SUZUKI, KAZUYUKI;ITOH, KOJI |
分类号 |
B64C13/40;B64C9/02 |
主分类号 |
B64C13/40 |
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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