| 发明名称 |
AIRCRAFT HYDRAULIC PUMP CONTROL SYSTEM |
| 摘要 |
A control system for an aircraft's electrically driven hydraulic pump. An electronic motor controller having closed loop feedback is utilized to directly control the prime mover speed in response to pump loading.
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| 申请公布号 |
CA2213457(C) |
申请公布日期 |
2005.05.24 |
| 申请号 |
CA19962213457 |
申请日期 |
1996.03.13 |
| 申请人 |
THE BOEING COMPANY |
发明人 |
NOZARI, FARHAD |
| 分类号 |
F04B1/32;F04B49/06;(IPC1-7):F04B49/06;F04B17/03 |
主分类号 |
F04B1/32 |
| 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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