DocumentCode :
954835
Title :
Aging in wire insulation under multifactor stress
Author :
Bruning, A.M. ; Campbell, F.J.
Author_Institution :
Lectromechanical Design Co., Herndon, VA, USA
Volume :
28
Issue :
5
fYear :
1993
fDate :
10/1/1993 12:00:00 AM
Firstpage :
729
Lastpage :
754
Abstract :
A fundamentally based chemical-thermodynamic multifactor stress aging functional relation requiring experimentally based constants is developed. The specific example presented is that of 120-V aromatic-polyimide-insulated wire. The stresses of water, temperature, and mechanical strain are included and electrical stress is considered. The results for over 2000 specimens are fitted to the theoretical trends. For a single independent variable function, the resulting relation reduces to the classical Arrhenius curve. The three independent variable relations presented here are applied to data from laboratory aging experiments that simulate insulation deterioration occurring in actual aircraft service. The results used in age categorization of US Navy aircraft are taken from wire specimens taken from active aircraft. The paradigm does not use ab initio based constants because of uncertainties in the theoretical development, two forms of which are presented
Keywords :
ageing; cable insulation; insulated wires; insulation testing; life testing; military equipment; organic insulating materials; polymer films; 120 V; US Navy aircraft; age categorization; aircraft service; aromatic-polyimide-insulated wire; chemical-thermodynamic multifactor stress aging functional relation; classical Arrhenius curve; electrical stress; insulation deterioration simulation; insulation life; insulation testing; mechanical strain; polymer insulation; wire insulation ageing; Aging; Cable insulation; Capacitive sensors; Chemicals; Laboratories; Military aircraft; Stress; Temperature; Uncertainty; Wire;
fLanguage :
English
Journal_Title :
Electrical Insulation, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9367
Type :
jour
DOI :
10.1109/14.237739
Filename :
237739
Link To Document :
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