JSME Materials and Processing Conference (M&P)
Online ISSN : 2424-2861
10.2
会議情報
614 Aircraft design tensile strength of carbon fiber irradiated by EB
Akihiro MizutaniAtushi KimuraTakashi ToriyamaKazuya OguriAkira TonegawaYoshitake Nishi
著者情報
会議録・要旨集 フリー

p. 498-501

詳細
抄録
Using sheet electron beam (EB) irradiation, reinforcement for carbon fiber was achieved. In order to annihilate twisting strain in carbon fiber, fracture stress was precisely obtained by means of a twisting free tensile test developed. The EB treatment enhanced the fracture stress at different integrated fracture rates (R_f) and increased Weibull modulus. It also enhanced design stress, when the integrated fracture probability (P_f) is (10)^<-5> for aircraft materials. The aircraft design stress was approximately 4 GPa larger than that before EB treatment.
著者関連情報
© 2002 The Japan Society of Mechanical Engineers
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