Experimental Study of a Certain Type of Aircraft Structure Repair Adhesive
2014 ◽
Vol 633-634
◽
pp. 387-390
Keyword(s):
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.
2011 ◽
Vol 415-417
◽
pp. 35-38
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Keyword(s):
2016 ◽
Vol 54
(4)
◽
pp. 501
Keyword(s):
2005 ◽
Vol 2005.18
(0)
◽
pp. 369-370
2015 ◽
Vol 9
(12)
◽
pp. 1143-1147
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Keyword(s):
2001 ◽
Vol 38
(10)
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pp. 1019-1031
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Keyword(s):
2014 ◽
Vol 48
◽
pp. 75-79
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2017 ◽
Vol 91
◽
pp. 61-69
◽
2005 ◽
Vol 2005.1
(0)
◽
pp. 403-404
2021 ◽
Vol 1802
(2)
◽
pp. 022046
2009 ◽
Vol 114
(2)
◽
pp. 811-817
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Keyword(s):