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座舱玻璃划伤故障容限研究
引用本文:张志林,叶彬.座舱玻璃划伤故障容限研究[J].洪都科技,2002(1):8-13.
作者姓名:张志林  叶彬
作者单位:洪都航空工业集团650所
摘    要:确定了座舱玻璃划伤故障模型,得出了MDYB-3玻璃表面裂纹断裂韧度和表面划伤扩展门坎值,建立了座舱玻璃划伤故障剩余强度准则和划伤故障容限计算方法,并给出了9mm厚MDYB-3玻璃划伤故障容限值。为外场划伤故障分析处理提供了简便易行的方法。

关 键 词:剩余强度  军用飞机  座舱玻璃  使用寿命  故障模型

Research of Scratch Tolerance for Cabin Glass
Zhang Zhilin Ye Bin.Research of Scratch Tolerance for Cabin Glass[J].Hongdu Science and Technology,2002(1):8-13.
Authors:Zhang Zhilin Ye Bin
Abstract:This paper established the scratch model of the cabin glass and obtained fracture toughness of face crack and threshold level of scratch propagation of MDYB -3glass,and established residual str ength specification and the method o f calculation for the scratch tolerance value,and gave th e scratch tolerance value of MDYB -3g lass that thickness is 9mm and provided some simple methods for disposing outfield scratch prob-lems.
Keywords:Plexiglas Scratch Tolerance Residual Strength
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