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Strategies for Improving the Damage Tolerance of Rotorcraft Components

机译:改善旋翼机组件损坏容差的策略

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The purpose of this paper is to discuss several metal treatment approaches, based on deep residual stress (DRS) treatments, that can transform mechanical system members with little or no damage tolerance into members capable of satisfying the damage tolerance requirements of FAR 29.571. These approaches include: (1) Cold-working with an oversized mandrel, (2) ForceMate® cold-expanded bushings, and (3) Laser shock peening. The differences between the DRS approaches and the relative advantages of each are discussed, as are the challenges which must be overcome in successfully implementing each approach. The need for a holistic approach which combines simulations of the manufacturing treatment processes used to induce the residual stresses with the traditional DTA analyses is emphasized, due to the large plastic strains induced and the risk of premature failure during the application of the DRS treatment. Engineering models for predicting the strains during the cold-working or laser shock peening treatment process and the resulting residual stresses are discussed, along with a weight function-based approach for determining the stress intensity factors for a crack growth analysis. Examples are presented comparing the crack growth lives of typical mechanical system members with and without the DRS fatigue life enhancement treatment to illustrate the relative advantage of each method, and to illustrate the potential of these methods in imparting damage tolerance to mechanical and dynamic system components.
机译:本文的目的是讨论几种基于深度残余应力(DRS)处理的金属处理方法,可以将机械系统构件转换为能够满足远期29.571的损坏公差要求的构件几乎没有损伤或没有损坏的耐受性。这些方法包括:(1)冷加工用超大的心轴,(2)Forcemate®冷膨胀衬套,和(3)激光冲击喷丸。讨论了DRS方法之间的差异以及每个方法的相对优势,也是必须克服成功实施每种方法的挑战。需要一种全面的方法,其中制造处理过程的联合收割机模拟用于诱导与传统的DTA分析被强调,残余应力由于感应的大的塑性应变和过早失效的DRS治疗的应用期间的风险。用于预测冷加工或激光休克治疗过程中菌株的工程模型以及所得到的残余应力,以及基于重量的函数的方法,用于确定裂纹生长分析的应力强度因子。提出了将典型的机械系统构件的裂纹生长寿命与DRS疲劳寿命增强处理进行比较,以说明每种方法的相对优势,并说明这些方法在赋予机械和动态系统部件的损坏容差。

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