| 发明名称 |
CONTROL SYSTEM FOR PLURAL ENGINES |
| 摘要 |
<p>Two gas turbine helicopter engines are coupled together for isochronous operation to supply a common load. A control circuit assures that the power delivered to the common load is equally divided between the two engines. The torque of each engine is detected and the torques are compared to established control signals for the engines.</p> |
| 申请公布号 |
CA1098997(A) |
申请公布日期 |
1981.04.07 |
| 申请号 |
CA19780303075 |
申请日期 |
1978.05.11 |
| 申请人 |
SUNDSTRAND CORPORATION |
发明人 |
GLENNON, TIMOTHY F.;FAULKNER, DENNIS T. |
| 分类号 |
F02D41/14;B64C27/68;F02C6/02;F02C9/42;F02D25/00;(IPC1-7):05D15/01 |
主分类号 |
F02D41/14 |
| 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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