DESIGN SUBSTANTIATION AND APPLICATION OF BORON-EPOXY PATCH REPAIR ON AN F-16 UPPER FUSELAGE SKIN

机译：F-16上壳体蒙皮的硼酸修补修复设计实例及应用

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The known potential of composite repairs led the Israeli Air Force (IAF) to the decision of implementing a bonded repair for a fatigue problem in the F-16 aircraft Fuselage upper skin (STA. 341.8). A 4mm thick Boron Epoxy co-cured patch was designed and manufactured. The repair concept was successfully tested both on the aircraft and by means of component tests.

机译：复合维修的已知潜力使以色列空军（IAF）决定对F-16飞机机身上部蒙皮的疲劳问题进行保税维修（STA。341.8）。设计并制造了一个4毫米厚的硼环氧树脂共固化贴剂。维修概念已在飞机上和通过组件测试成功进行了测试。

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来源
《ICAF-Doc. 2311; International Committee on Aeronautical Fatigue Symposium(ICAF 2003) vol.1; 20030507-09; Lucerne(CH)》|2003年|P.591-599|共9页
会议地点 Lucerne(CH)
作者
I. Kressel; G.Ghilai; S.Gali; N.Hackman; H.Leibovich; D.Peled; A.Brot; U.So; E.Grosu; I.Cohen; M.ben-noon; S. Jiny; Y.Meir; R.Halevi; L.Alon; A.Atzmoni;
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IAI Engineering Division, Ben Gurion International Airport 70100 Israel;

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原文格式 PDF
正文语种 eng
中图分类飞机的疲劳;
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DESIGN SUBSTANTIATION AND APPLICATION OF BORON-EPOXY PATCH REPAIR ON AN F-16 UPPER FUSELAGE SKIN

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