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Bending Fatigue Tests of Helicopter Case Carburized Gears: Influence of Material, Design and Manufacturing Parameters

机译:直升机外壳渗碳齿轮弯曲疲劳试验:材料,设计和制造参数的影响

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A single tooth bending (STB) test procedure has been developed to optimally map the AgustaWestland gear design parameters and a test program on case carburized, aerospace standard gears, has been conceived and performed in order to appreciate the influence of various technological parameters on fatigue resistance, and to draw the curve shape up to the gigacycle region. In a first phase, tests up to 10 million cycles have been performed on four test groups differing by material (VAR and VIM-VAR 9310, and VIM-VAR EX-53) and by manufacturing process (ground fillet versus unground fillet); in the second phase, VIM-VAR 9310 ground fillet specimen have been tested up to 100 million cycles. All the gear types were shotpeened. FEM analysis, strain gauge measurements and rating formula of AGMA standard are used to express test loads in terms of tooth root stresses. The program has been completed by failure analysis, based on SEM, on failed specimens and by ultimate load tests.
机译:已经开发出单齿弯曲(STB)测试程序,以最佳地图渗碳,航空航天标准齿轮的AgustaWestland齿轮设计参数和测试程序,以便欣赏各种技术参数对疲劳性抗性的影响,并将曲线形状绘制到缩放区域。在第一阶段,已经对由材料(VAR和VIM-VAR 9310和VIM-VAR EX-53)不同的四个测试组进行了高达1000万个周期的测试,并通过制造工艺(接地圆角与未处理圆角);在第二阶段,Vim-var 9310接地圆角样本已被测试高达1亿周期。所有的齿轮类型都被抛丸。 AGMA标准的FEM分析,应变计测量和额定值配方用于表达齿根应力方面的测试载荷。该程序已通过故障分析完成,基于SEM,失败的标本和最终负载测试。

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