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文中介绍了舱盖后部骨架与玻璃间有XM-18胶的飞机舱盖玻璃后部槽口应力裂纹和有关的试验、观测情况,并在这些试验、观测的基础上,对舱盖玻璃上的应力产生作了分析,提出了应力裂纹产生原因的看法。
This paper introduces the stress cracks in the rear notch of the glass hatchback with the XM-18 adhesive between the rear hatch and the glass, and the related tests and observations. Based on these tests and observations, The stress generation was analyzed and the view of the cause of stress cracks was put forward.