Performance Reliability Prediction of Complex System Based on the Condition Monitoring Information

Table 1

Key performance monitoring parameters for some aircraft engine.

Monitoring point	DEGT	GWFM	GPCN25	DPOIL	ZVBIF	ZVB2R	TSI/FH	PDD
1	4.69	2.66	1.83	−3.76	0.31	0.51	3282	0.0975
2	−0.63	4.91	2.00	−5.74	0.43	0.76	3754	0.0459
3	−5.66	3.70	1.95	−3.00	0.29	0.38	2640	0.1078
4	5.25	4.06	2.00	−5.55	0.89	0.65	4740	0.1176
5	−3.94	4.25	1.72	−8.82	0.50	0.46	1707	0.1305
⋮	⋮	⋮	⋮	⋮	⋮	⋮	⋮	⋮
16	17.41	6.03	2.08	9.26	0.29	0.33	6688	0.1892
17	3.17	4.41	2.24	9.39	0.97	0.61	1477	0.1725
18	−3.19	2.00	1.68	13.10	0.00	0.89	6376	0.1572
19	7.52	2.78	1.04	−3.24	0.45	0.99	5021	0.1665
20	4.43	3.77	2.30	−5.96	0.52	0.48	7160	0.1285