发明名称 |
Fuel control for a multi-engine gas turbine installation |
摘要 |
An electronic control for a multi-engine gas turbine installation includes two channels each containing a low wins gate with a signal error input and an acceleration limit input, the output of the low wins gate being applied via a high wins gate to an electronic integrator the output of which is compared with a speed signal to provide fuel control for speed governing. For balancing the two channels a difference amplifier provides an output containing information related to the output of one or other low wins gate and the difference between the values of a given parameter of each engine. This acts to control this difference both during steady running and acceleration.
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申请公布号 |
US4100731(A) |
申请公布日期 |
1978.07.18 |
申请号 |
US19760746347 |
申请日期 |
1976.12.01 |
申请人 |
LUCAS INDUSTRIES LIMITED |
发明人 |
JANES, RODERICK STEWART;LLOYD, MAURICE EDWARD |
分类号 |
F02C9/42;(IPC1-7):F02C9/02;F02C9/08 |
主分类号 |
F02C9/42 |
代理机构 |
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代理人 |
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主权项 |
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