Preparation method of polyimide composite material for fasteners
A polyimide and composite material technology, which is applied in the field of preparation of polyimide composite materials for fasteners, can solve problems such as high cost and difficult forming and processing, and achieves low porosity, good mechanical properties and stable performance. Effect
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Embodiment 1
[0020] (1) Preparation of monoester
[0021] 246g (1.5mol) 5-norbornene-2,3-dicarboxylic anhydride was heated to reflux at 69°C to 90°C in 259g ethanol for 2 hours to prepare 5-norbornene-2,3-dicarboxylic acid monoethyl ester (NE ).
[0022] 286g (1mol) 2,3,3',4'-diphenyl ether tetracarboxylic dianhydride reacted in 256g ethanol with reflux at 69~90°C for 5 hours to prepare 2,3,3',4'-diphenyl ether tetra Monoethyl formate.
[0023] 3,3',4,4'- Bisphenol A diphenyl ether tetracarboxylate monoethyl ester.
[0024] (2) Preparation of polyimide matrix resin
[0025] Dissolve 400g (2mol) of 4,4'-diaminodiphenyl ether in 358g of ethanol and stir for half an hour, then add the above-prepared 2,3,3',4'-diphenyl ether tetracarboxylate monoethyl ester and 3, 3',4,4'-bisphenol A diphenyl ether tetracarboxylate monoethyl ester mixture, after stirring for 1 to 2 hours, and 5-norbornene-2,3-dicarboxylic acid monoethyl ester (NE) at 70 ℃ ~ 83 ℃ stirring reaction for 5 hours to obtain a ...
Embodiment 2
[0033] Except that the dosage of 2,3,3',4'-diphenyl ether tetracarboxylic dianhydride is 1mol, and the dosage of 3,3',4,4'-bisphenol A diphenyl ether tetracarboxylic dianhydride is 0.6mol, polyamide The imine matrix resin solution is prepared by mixing 5-norbornene-2,3-dioic acid monoethyl ester, 2,3,3',4'-diphenyl ether tetracarboxylic acid monoethyl ester and 3,3',4, The ethanol solution of 4'-bisphenol A tetracarboxylic acid monoethyl ester is mixed with the ethanol solution of 4,4'-diaminodiphenyl ether; the organosilicon coupling agent γ-aminopropyltriethoxysilane treated The glass fibers were impregnated in the prepared polyimide matrix resin solution, and the other formulations and operating steps were the same as in Example 1. As a result, the thread bearing capacity was 10KN and the bolt tensile failure force was 2.5KN.
Embodiment 3
[0035] Except that carbon fiber is used instead of glass fiber, other formulations and operating procedures are the same as in Example 1. As a result, the bearing capacity of thread is 13KN, and the tensile breaking force of bolt is 3.1KN.
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