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FATIGUE DAMAGE OF SHAFT WITH THE COLLAR FORMED BY A NEW DEFORMATION PROCESSING METHOD FOR ENLARGING PARTIAL DIAMETER

机译:轴的疲劳损坏与套环形成的新变形处理方法,用于扩大部分直径

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We have proposed a new deformation processing method for enlarging partial diameter of shaft. The method is called a collar-forming method. To examine fatigue damage of the part processed (called a collar) during the forming process, rotary bending fatigue tests and tensile strength verification tests were carried out on smooth test specimen as well as two kinds of collared test specimen, namely the specimen with burrs and without burr. Moreover, stress concentration and strain hardening in the root of collar were quantitatively evaluated by the finite element method. The following were clarified from those results: Though there are burrs, the fatigue damage in the root of a collar during the forming process is not caused at all when an increase rate of shaft diameter is within 1.7. The processing stage in which the increase rate is within 1.7 is still a stage of the work hardening, and is not a stage in which the fatigue life is shortened by increasing of macro-damage. There are not any signs of fatigue deterioration in the root of collar formed by the processing method from a practical viewpoint, either but there is sound to the fatigue damage enough.
机译:我们提出了一种新的变形处理方法,用于扩大轴的部分直径。该方法称为环形形成方法。为了检查在成型过程中处理(称为衣领)的部件的疲劳损伤,在光滑的试样以及两种颈弧试样上进行旋转弯曲疲劳试验和拉伸强度验证试验,即带有毛刺和毛刺的样品没有毛刺。此外,通过有限元方法定量地评估套环根部的应力浓度和应变硬化。从那些结果中澄清了以下内容:虽然存在毛刺,但是当轴直径的提高速率在1.7内时,根本不会引起轴环的根部疲劳损伤。增加速率在1.7内的加工阶段仍然是工作硬化的阶段,并且不是通过增加宏损伤来缩短疲劳寿命的阶段。从实际观点来看,由加工方法形成的套环根部没有任何疲劳劣化迹象,但是疲劳损坏的声音足够。

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