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    • 2. 发明授权
    • Determining expected fatigue life of hard machined components
    • 确定硬加工零件的预期疲劳寿命
    • US07117574B2
    • 2006-10-10
    • US10389241
    • 2003-03-14
    • Chunghorng R. LiuSalah Ramadan Agha
    • Chunghorng R. LiuSalah Ramadan Agha
    • B23Q17/00
    • F16C33/64G05B19/4155G05B2219/36295Y10T29/49764Y10T82/10
    • A method of determining expected fatigue life of machined bearing races or other components wherein a hardened surface of each bearing race is machined to provide a machined surface including the steps of determining hardness distribution and residual stress distribution along a depth into the machined surface as a function of cutting parameters, determining a relationship of expected fatigue life of the machined bearing races as a function of the hardness distribution and the residual stress distribution using a fracture mechanics model, and determining expected fatigue life from the relationship using actual cutting parameters employed in machining the hardened surface of the bearing races. Cutting conditions to optimize fatigue life can be selected based on the expected fatigue life.
    • 确定加工轴承座圈或其他部件的预期疲劳寿命的方法,其中加工每个轴承座圈的硬化表面以提供加工表面,其包括以下步骤:确定沿加工表面的深度的硬度分布和残余应力分布作为一个功能 切削参数,使用断裂力学模型确定机加工轴承座圈的预期疲劳寿命的关系作为硬度分布和残余应力分布的函数,并且根据使用在加工中使用的实际切削参数的关系确定预期的疲劳寿命 轴承座的硬化表面。 可根据预期的疲劳寿命选择切割条件以优化疲劳寿命。
    • 3. 发明授权
    • Method of manufacturing a component
    • 制造零件的方法
    • US5878496A
    • 1999-03-09
    • US631686
    • 1996-04-09
    • Chunghorng R. LiuShridhar Mittal
    • Chunghorng R. LiuShridhar Mittal
    • B23Q15/00B21K1/04C21D7/04C21D9/40F16C33/64B23P15/00
    • F16C33/64B21K1/04C21D7/04C21D9/40C21D2261/00Y10S148/906Y10T29/49689Y10T29/49758Y10T29/49764Y10T29/49776
    • A process for manufacturing a component on which in-service stresses are imposed by in-service loading conditions. The process generally entails fabricating the component such that residual stresses are induced in the component that substantially offset one or more primary stresses which would otherwise limit the maximum service life of the component. The residual stresses are induced by creating compressive stresses in the component that extend sufficiently beneath the working surface of the component during fabrication. In order to appropriately attain the necessary residual stresses, the process of this invention includes developing a model of the component, and then applying the in-service loading conditions to the model to determine the in-service stresses on the component. Thereafter, at least one of the in-service stresses is identified as being critical, i.e., a stress that establishes the maximum service life of the component. Finally, the component is fabricated such that necessary residual stresses are induced in the component in order to offset the identified critical stress.
    • 用于制造通过在役加载条件施加在职应力的部件的过程。 该方法通常需要制造部件,使得在部件中引起基本上抵消一个或多个主应力的残余应力,否则将限制部件的最大使用寿命。 残余应力通过在组件中产生压缩应力而引起,该压缩应力在制造期间充分地延伸到部件的工作表面下方。 为了适当地获得必要的残余应力,本发明的方法包括开发组件的模型,然后将在用加载条件应用于模型以确定部件上的使用中应力。 此后,至少一个在役应力被识别为关键的,即,确定组件的最大使用寿命的应力。 最后,制造该部件,使得在部件中产生必要的残余应力以抵消所识别的临界应力。