Decomposition behaviour of Kevlar 49 fibres:: Part I.: At T ≈ Td

被引:16
作者
Iyer, RV [1 ]
Vijayan, K [1 ]
机构
[1] Natl Aerosp Labs, Div Mat Sci, Bangalore 560017, Karnataka, India
关键词
Kevlar; 49; decomposition; crystallinity; weight loss; hollowness; surface damages;
D O I
10.1007/BF02745614
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The structural changes which accompany decomposition of Kevlar 49 fibres at T= 500 degrees C and 550 degrees C, respectively, have been elucidated. At both these temperatures, cumulative thermal exposures of specific durations, t(cum)(T), are required to result in decomposition. The conspicuous features which characterize isothermal decomposition of the fibres are: (i) progressive reduction and an eventual total loss in fibre crystallinity, (ii) progressive loss in weight, (iii) introduction of surface damages, (iv) introduction of hollowness, and (v) deterioration in tensile properties.
引用
收藏
页码:1013 / 1023
页数:11
相关论文
共 22 条
[1]   TENSILE RECOIL MEASUREMENT OF COMPRESSIVE STRENGTH FOR POLYMERIC HIGH-PERFORMANCE FIBERS [J].
ALLEN, SR .
JOURNAL OF MATERIALS SCIENCE, 1987, 22 (03) :853-859
[2]   The wave-lengths of the silver, molybdenum, copper, iron and chromium K alpha(1) lines [J].
Bearden, JA .
PHYSICAL REVIEW, 1933, 43 (02) :92-97
[3]   STRUCTURAL CHARACTERISTICS OF ARAMID FIBER VARIANTS [J].
DOBB, MG ;
ROBSON, RM .
JOURNAL OF MATERIALS SCIENCE, 1990, 25 (1B) :459-464
[4]  
DOBB MG, 1977, J POLYM SCI POL PHYS, V15, P2201, DOI 10.1002/pol.1977.180151212
[5]   EFFECTS OF ANNEALING ON THE CRYSTALLINITY AND MICROPARACRYSTALLITE SIZE OF KEVLAR 49 FIBERS [J].
HINDELEH, AM ;
ABDO, SM .
POLYMER, 1989, 30 (02) :218-224
[6]  
IYER RV, 1998, UNPUB J MATER SCI
[7]  
IYER RV, 1994, POLYM SCI RECENT ADV, V1, P362
[8]  
KALASHNIK AT, 1978, POLYM SCI USSR, V19, P3173
[9]   TENSILE FATIGUE BEHAVIOR OF PARA-ORIENTED ARAMID FIBERS AND THEIR FRACTURE MORPHOLOGY [J].
KONOPASEK, L ;
HEARLE, JWS .
JOURNAL OF APPLIED POLYMER SCIENCE, 1977, 21 (10) :2791-2815
[10]  
MEREDITH R, 1975, TEXT PROGR, V7