发明名称 |
PARTIAL ENGINE AND DRIVESHAFT FAILURE DETECTION MONITOR FOR A MULTI-ENGINE AIRCRAFT |
摘要 |
An engine failure monitor (50) for use with a multi-engine aircraft having at least two engines detects conditions indicative of a partial (700) or total (400) engine failure, including turbine shaft failures (600). In response to an engine failure, suitable inputs (134, 138, 712) are provided to an electronic engine control for operating the remaining engine. Additionally, indications indicative of the engine failure (132, 710) are provided to the cockpit. |
申请公布号 |
WO9410619(A1) |
申请公布日期 |
1994.05.11 |
申请号 |
WO1993US09508 |
申请日期 |
1993.10.05 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
RICE, ROBERT, W.;SWEET, DAVID, H. |
分类号 |
B64D31/00;B64D31/12;F02C3/10;F02C6/02;F02C7/00;G07C3/00;(IPC1-7):G05D13/64 |
主分类号 |
B64D31/00 |
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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