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Shear Load Transfer for Corrosion Coated Clamped Joints

机译:腐蚀涂层夹紧接头的剪切载荷传递

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Rotorcraft transmission housings contain multiple joints that are typically held together by threaded fasteners. For many of these installations, the material surfaces are now coated with corrosion inhibitors that can change the strength of the joint. To identify these changes, Bell Helicopter has conducted coupon testing of coated materials in shear. Historically, the faying surfaces have been left bare with the perception that coatings would degrade the ability to transfer shear loads. Fastener and joint design has been based on assumed joint slip coefficients. A test effort to identify the shear load transfer characteristics of a clamped joint was undertaken. A double shear coupon test was used to measure the shear load capability of the clamped joint with bare material surfaces as well as with corrosion protection coated surfaces. Tests were run with calibrated bolt preloads to reduce variability. To simulate the gearbox temperature environment, the test coupons and mechanical grips were placed in an oven to maintain a temperature of 180°F. Testing showed that the addition of coating reduced the joint slip coefficient when compared to baseline bare materials.
机译:旋翼航空器变速箱壳体包含多个接头,这些接头通常通过螺纹紧固件固定在一起。对于许多这样的安装,现在材料表面都涂有腐蚀抑制剂,这些腐蚀抑制剂可以改变接头的强度。为了识别这些变化,贝尔直升机公司已对剪切的涂层材料进行了试样测试。从历史上看,接合面一直裸露在外,因为涂层会降低传递剪切载荷的能力。紧固件和接头设计均基于假定的接头滑移系数。进行了测试工作,以确定夹紧接头的剪切载荷传递特性。使用双重剪切试样试验来测量具有裸露材料表面以及具有防腐涂层的表面的夹紧接头的剪切载荷能力。使用校准的螺栓预紧力进行测试,以减少变化。为了模拟齿轮箱的温度环境,将测试样板和机械夹具放在烤箱中以保持180°F的温度。测试表明,与基线裸露材料相比,添加涂层降低了接头滑移系数。

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