发明名称 |
Embedded engine diagnostic system |
摘要 |
<p>An engine diagnostic system includes a plurality of sensors (4). One of the plurality of sensors includes a speed sensor generating a speed value indicative of aircraft speed. A processor (2) is coupled to the sensors and stores prior mission data and current mission data in a data memory (12) when the speed value is within a predetermined velocity range. A fault indicator (6) is provided which is visible from the exterior of the aircraft. The processor detects a presence or absence of a fault in response to the prior mission data and current mission data and activates the fault indicator in response to the presence of a fault. <IMAGE></p> |
申请公布号 |
EP1089239(A2) |
申请公布日期 |
2001.04.04 |
申请号 |
EP20000306462 |
申请日期 |
2000.07.28 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
BROGAN, CHRISTOPHER JOHN;PURSELL, BRYSON MARION;MATCHETT, STEVEN JOSEPH |
分类号 |
G01M15/14;B64D45/00;B64F5/00;F01D17/00;F02C9/00;F02C9/28;F02C9/44;G07C3/00;(IPC1-7):G07C3/00 |
主分类号 |
G01M15/14 |
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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