| 发明名称 |
GROUND MODE CONTROL OF AIRCRAFT PROPELLER SPEED AND PITCH |
| 摘要 |
A ground mode pitch position logic and control is shown and described in this invention. A method for scheduling and limiting the pitch actuator reference signal in accordance with the actuator commanded schedule, propeller overspeed and propeller underspeed.
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| 申请公布号 |
CA2014181(A1) |
申请公布日期 |
1990.10.11 |
| 申请号 |
CA19902014181 |
申请日期 |
1990.04.09 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SCHNEIDER, ROY W.;DIVALENTIN, EUGENIO |
| 分类号 |
B64D31/06;B64C11/30;F02C9/58;(IPC1-7):G05D1/08 |
主分类号 |
B64D31/06 |
| 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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