STUDIES ON PHASE SEPARATION OF POLYESTERIMIDE-MODIFIED EPOXY RESIN. II. EFFECT OF CURING TEMPERATURE ON PHASE SEPARATION AND ADHESIVE PROPERTY

2001 ◽  
Vol 38 (10) ◽  
pp. 1019-1031 ◽  
Author(s):  
Yan Luo ◽  
Hua Li ◽  
Shanjun Li
2003 ◽  
Vol 36 (20) ◽  
pp. 7746-7751 ◽  
Author(s):  
Wenjun Gan ◽  
Yingfeng Yu ◽  
Minghai Wang ◽  
Qingsheng Tao ◽  
Shanjun Li

2014 ◽  
Vol 633-634 ◽  
pp. 387-390
Author(s):  
Yang Huang ◽  
Ling Tian

Based on a certain type of aircraft structure repair adhesive was studied, the curing temperature of aircraft structure repair commonly used adhesive process of high, long curing time, curing thermal stress problem, with epoxy resin as basic material, by adding elastic toughening Ding Jin g rubber, curing agent and silane coupling agent modification on Toughening of epoxy resin. The mechanical properties of adhesive were analyzed through the cyclic loading test and tensile shear test, and the best ratio of modified epoxy resin adhesive. The adhesive prepared at 80 °C for 90 min after curing shear strength can reach 35MPa, which can meet the aircraft structure damage daily emergency repair requirements.


Author(s):  
W. G. Liu ◽  
T. L. Yu ◽  
W. Y. Chen ◽  
J. C. Chen

1992 ◽  
Vol 28 (5) ◽  
pp. 505-512 ◽  
Author(s):  
Costas G. Delides ◽  
David Hayward ◽  
Richard A. Pethrick ◽  
Argyris S. Vatalis

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