05-03-2015 дата публикации
Номер: US20150064393A1
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A laminate for joining parts of composite material includes a first layer of adhesive material, a second layer of preimpregnated composite material, adjacent to the first layer, and a third layer of adhesive material, adjacent to the second layer. A method for joining at least two parts of composite material with a laminate includes the steps of providing already cured composite material parts, positioning the laminate for joining between two cured parts, and applying pressure and temperature to the whole structure including the at least two parts and the laminate, in such a way that the laminate is cured and the at least two parts are joined together in a resulting structure. 1312. Laminate () for joining parts ( , ) of composite material that comprises:{'b': 3', '1, 'a first layer (.) of adhesive material,'}{'b': 3', '2', '3', '1, 'a second layer (.) of at least a preimpregnated composite material, adjacent to the first layer (.), and'}{'b': 3', '3', '3', '2, 'a third layer (.) of adhesive material, adjacent to the second layer (.).'}231232. Laminate () for joining parts ( claim 1 , ) according to characterized in that the second layer (.) comprises at least two layers of fresh fiber which are laid at 0°.3312. Laminate () for joining parts ( claim 1 , ) according to characterized in that the second layer comprises at least two layers of fresh fiber which are laid at 45°.4123. Method for joining at least two parts ( claim 1 , ) of composite material with a laminate () according to claim 1 , comprising the steps of:{'b': 1', '2, 'providing already cured composite material parts (, ),'}{'b': 3', '1', '2, 'positioning the laminate () for joining between the two cured parts (, ),'}{'b': 1', '2', '3', '3', '1', '2, 'applying pressure and temperature to the whole structure comprising the at least two parts (, ) and the laminate (), in such a way that the laminate () is cured and the at least two parts (, ) are joined together in a resulting structure.'}54. Method ...
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