Single vacuum debulk composite panel repair

Details Single vacuum debulk composite panel repair Single vacuum debulk composite panel repair

B - Operations, Transporting

29

C

B29C 73/10 (2006.01)

Patent

CA 2600006

A method of attaching a composite member to a structure. The method including forming a laminate of fabric impregnated with resin; applying heat at a first temperature to the impregnated laminate; applying vacuum at a first pressure to the impregnated laminate to degas the resin and form a degassed, impregnated laminate; positioning the degassed, impregnated laminate on a structure; and curing the degassed, impregnated laminate on the substrate by applying heat at a second temperature and by applying vacuum at a second pressure.

L'invention concerne un procédé de fixation d'un élément composite à une structure. Le procédé consiste à: former un stratifié de tissu imprégné de résine; appliquer de la chaleur, à une première température, sur le stratifié imprégné; appliquer un vide, à une première pression, sur le stratifié imprégné afin de dégazer la résine et de former un stratifié imprégné dégazé; placer le stratifié imprégné dégazé sur une structure; et polymériser le stratifié imprégné dégazé sur le substrat par application de chaleur à une seconde température, et application de vide à une seconde pression.

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