| 发明名称 |
AIRCRAFT FLIGHT CONTROL USER INTERFACE FLUID LINKAGE SYSTEM |
| 摘要 |
A user interface fluid linkage system includes first and second user interfaces that are linked by a single, constant volume fluid line. The system includes identically configured, but oppositely mounted hydraulic fluid chambers to link motion between the first and second user interfaces.
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| 申请公布号 |
US2009159756(A1) |
申请公布日期 |
2009.06.25 |
| 申请号 |
US20070960326 |
申请日期 |
2007.12.19 |
| 申请人 |
HONEYWELL INTERNATIONAL, INC. |
发明人 |
CHRISTENSEN DONALD J.;HANLON JAMES CASEY |
| 分类号 |
B64C13/04 |
主分类号 |
B64C13/04 |
| 代理机构 |
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