发明名称 |
Aircraft engine management system |
摘要 |
An aircraft jet engine management system has a digital electronic control unit (DECU) which measures turbine blade temperature (TBT) and controls the engine in such a way as not normally to exceed a TBT normal datum, there being an over-ride facility which responds to special circumstances as represented by one or more pilot-independent inputs to the DECU to allow temporary over-ride of the TBT limitation program, at least cut-off of the over-ride being pilot-independent.
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申请公布号 |
US5345386(A) |
申请公布日期 |
1994.09.06 |
申请号 |
US19920986743 |
申请日期 |
1992.12.08 |
申请人 |
ROLLS ROYCE PLC. |
发明人 |
MULLEN, STUART I.;SUMMERFIELD, LESLIE R. |
分类号 |
F02C9/28;(IPC1-7):G06F15/48;G06G7/70 |
主分类号 |
F02C9/28 |
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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