Fault hardware-based aero-engine narrowly-defined EBOM structure design method

Fault hardware-based aero-engine narrowly-defined EBOM structure design method

The invention belongs to the field of aero-engine design, and relates to a fault hardware-based aero-engine narrowly-defined EBOM structure design method, which comprises the following steps of: setting a narrowly-defined EBOM structure, nearly setting the EBOM into an object-unit-fault hardware thr...

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Hauptverfasser: CHE YANXIN, JIA RUIQI, LI ZHIQIANG, ZHAO HUIMIN
Format: Patent
Sprache:chi ; eng
Schlagworte:
CALCULATING
COMPUTING
COUNTING
ELECTRIC DIGITAL DATA PROCESSING
PHYSICS
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creator CHE YANXIN
JIA RUIQI
LI ZHIQIANG
ZHAO HUIMIN
description The invention belongs to the field of aero-engine design, and relates to a fault hardware-based aero-engine narrowly-defined EBOM structure design method, which comprises the following steps of: setting a narrowly-defined EBOM structure, nearly setting the EBOM into an object-unit-fault hardware three-layer structure, then defining fault hardware, traversing fault information of all hardware, and finally designing a narrowly-defined EBOM structure. Fault hardware conforming to the fault hardware definition is found out, and the fault hardware is connected with the corresponding unit body; carrying out minimum splitting on data in the fault hardware; and finally, synchronously identifying all fault components contained in any fault hardware, and synchronously migrating data information associated with all the found fault components into the corresponding fault hardware. The number of hardware needing to be controlled can be greatly reduced, the control working efficiency is improved, and the control quality is
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subjects CALCULATING
COMPUTING
COUNTING
ELECTRIC DIGITAL DATA PROCESSING
PHYSICS
title Fault hardware-based aero-engine narrowly-defined EBOM structure design method
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