Method of repairing composite material and composite material
AssigneeMitsubishi Aircraft Corporation
InventorsToshikazu Shigetomi, Masayoshi Suhara, Morimasa Ishida, Shuhei Muto
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AssigneeMitsubishi Aircraft Corporation
InventorsToshikazu Shigetomi, Masayoshi Suhara, Morimasa Ishida, Shuhei Muto
Estimating the term…
A method of repairing a composite material is provided in which a frustum-shaped portion of a composite material is removed, and the composite material and a repair material are bonded with each other while evacuating. The repair method includes step S2 of removing a damaged part 11 from the front side so as to pass through in the thickness direction while leaving a support wall protruding inward in the radial direction from the periphery of the top face of the frustum-shaped portion; step S3 of sealing the back side by placing a sealing plate, which is inserted from the front side into a through hole formed by the removing step, on the support wall; step S5 of placing the repair material through an adhesive on the composite material where the frustum-shaped portion has been removed; and step S6 of evacuating in a state in which the front side is sealed.
A method of repairing a composite material that is formed of fibers and resin in a plate shape and has a to-be-removed frustum-shaped portion having a diameter enlarging from a back side toward a front side, the composite material being bonded with a repair material replacing the removed portion, comprising the steps of:
Dependencies are inferred from the claim text.