发明名称 |
AIRCRAFT ENGINE MAINTENANCE SYSTEM |
摘要 |
A computerised aircraft engine maintenance planning system for maintaining an aircraft engine fleet comprising a plurality of aircraft engines, each engine in the fleet comprising an engine health monitoring system configured to provide data indicative of an incipient fault for a respective engine. The planning system comprises:
a fault forwarding sub-system configured to receive indications of incipient faults from respective engine health monitoring systems, the fault forwarding system being configured to identify two or more engines having linked incipient faults; anda queuing sub-system configured to assign each engine identified as having an incipient fault to a virtual maintenance queue position;wherein the queuing sub-system is configured to group engines having linked incipient faults to adjacent queue positions. |
申请公布号 |
US2016207639(A1) |
申请公布日期 |
2016.07.21 |
申请号 |
US201514964143 |
申请日期 |
2015.12.09 |
申请人 |
ROLLS-ROYCE PLC |
发明人 |
ELLIS Sean;VYAS Parag;NNAEKEZIE Richardson;MOXON Matthew;INCELEME Ekin |
分类号 |
B64F5/00;G07C5/00;G07C5/08;B64D45/00 |
主分类号 |
B64F5/00 |
代理机构 |
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代理人 |
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主权项 |
1. A computerised aircraft engine maintenance planning system for maintaining an aircraft engine fleet comprising a plurality of aircraft engines, each engine in the fleet comprising an engine health monitoring system configured to provide data indicative of an incipient fault for a respective engine, the planning system comprising:
a fault forwarding sub-system configured to receive indications of incipient faults from respective engine health monitoring systems, the fault forwarding system being configured to identify two or more engines having linked incipient faults; and a queuing sub-system configured to assign each engine identified as having an incipient fault to a virtual maintenance queue position; wherein the queuing sub-system is configured to group engines having linked incipient faults to adjacent queue positions. |
地址 |
London GB |