| 发明名称 |
ROTORCRAFT LOAD FACTOR ENHANCER |
| 摘要 |
Rotorcraft Load Factor Enhancer Rotor speed is maintained at a reference speed by a closed-loop fuel control system. Load factor potential is enhanced by increasing the reference speed as a function of the helicopter pitch rate when undergoing positive pitch rate maneuvers. |
| 申请公布号 |
CA1246717(A) |
申请公布日期 |
1988.12.13 |
| 申请号 |
CA19840458431 |
申请日期 |
1984.07.09 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
COOPER, DEAN E.;HOWLETT, JAMES J. |
| 分类号 |
B64C27/14;B64C27/00;B64C27/12;B64D31/00;B64D31/06;G05D1/08;H02P23/00 |
主分类号 |
B64C27/14 |
| 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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