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    • 22. 发明授权
    • Bend bar quality control method for laser shock peening
    • 激光冲击硬化弯曲棒质量控制方法
    • US07906745B2
    • 2011-03-15
    • US11009123
    • 2004-12-10
    • Richard D. TenagliaAllan H. ClauerJeff L. DulaneyDavid F. LahrmanSteve Toller
    • Richard D. TenagliaAllan H. ClauerJeff L. DulaneyDavid F. LahrmanSteve Toller
    • B23K26/00
    • C21D10/005G01N3/20G01N3/62G01N2203/0248G01N2203/0664
    • A bend bar is available for use in a quality control test for testing for a consistency of residual stress effects in a particular material using a given a laser peening process. The bar is composed of the particular material to be tested and has a bar length and a bar thickness. The particular material has a characteristic maximum stress penetration depth for compressive residual stresses that can be formed in using the given laser peening process. The bar thickness is chosen so as to be at least twice the characteristic maximum stress penetration depth. The bar has a test surface that extends parallel to the bar length and perpendicular to the bar thickness. After forming a spot pattern on the test surface using the given laser peening process, the deflection generated in the bar due to the compressive residual stresses induced by laser peening can then be measured and used as a quality control measurement.
    • 弯曲杆可用于质量控制测试,用于使用给定的激光喷丸处理来测试特定材料中的残余应力效应的一致性。 该棒由待测试的特定材料组成,具有棒长度和棒厚度。 特定材料具有特定的最大应力穿透深度,用于在使用给定的激光喷丸处理过程中形成的压缩残余应力。 选择棒厚度至少是特征最大应力穿透深度的两倍。 棒具有平行于棒长度并垂直于棒厚度的测试表面。 在使用给定的激光喷丸处理方法在测试表面上形成斑点图案之后,可以测量由于激光喷丸处理引起的压缩残余应力而在棒中产生的偏转并用作质量控制测量。
    • 23. 发明授权
    • Automated positioning of mobile laser peening head
    • 自动定位移动激光喷丸头
    • US06867390B2
    • 2005-03-15
    • US10372523
    • 2003-02-21
    • Allan H. ClauerJeff L. DulaneyDavid F. Lahrman
    • Allan H. ClauerJeff L. DulaneyDavid F. Lahrman
    • B64F5/00G01N21/95B23K26/00
    • G01N21/95B23K26/356B64F5/60C21D7/02
    • The present invention enables the processing head to locate itself precisely on the surface of the structure being processed, and to then reposition itself correctly for the next laser spot. Further, the present invention will complete processing a laser peened area, the area including a multiplicity of spots arranged in a specific pattern, and correctly laser peen each spot in the area under control of a controller including control linkages with the laser.The invention further provides an automated laser peening processing head encompassing spatial position sensing and locating means, as well as programmed spatial positioning, application of overlay materials, verification of proper overlay condition and positioning, and notification of the laser to pulse the surface of the structure.
    • 本发明使处理头能够精确地定位在正在处理的结构的表面上,并且随后重新定位它自己正确地为下一个激光点。 此外,本发明将完成处理激光喷丸区域,该区域包括以特定图案布置的多个斑点,以及在包括与激光器的控制连接的控制器的控制下的区域中的每个点的正确激光喷丸。本发明进一步 提供了包括空间位置感测和定位装置的自动化激光喷丸处理头,以及编程的空间定位,覆盖材料的应用,适当的覆盖条件和定位的验证以及激光器通知结构的表面。
    • 25. 发明授权
    • System for laser shock processing objects to produce enhanced stress distribution profiles
    • 用于激光冲击加工的系统产生增强的应力分布曲线
    • US06759626B2
    • 2004-07-06
    • US10207527
    • 2002-07-29
    • Allan H. ClauerDavid F. LahrmanJeff L. DulaneySteve M. Toller
    • Allan H. ClauerDavid F. LahrmanJeff L. DulaneySteve M. Toller
    • B23K2600
    • C21D10/005
    • Various laser shock processing systems are provided to establish selective compressive residual stress distribution profiles within a workpiece. An asymmetrical stress profile may be formed through the thickness of a thin section of a gas turbine engine airfoil. One system is configured to simultaneously irradiate a workpiece with a set of laser beams to form a corresponding set of adjacent non-overlapping laser shock peened surfaces, enabling the shockwaves to encounter one another. Another system irradiates opposite sides of the workpiece at different times to form opposing laser shock peened surfaces, enabling the shockwaves to meet at a location apart from the mid-plane. Another system simultaneously irradiates opposite sides of the workpiece using laser beams having different pulse lengths to form opposing laser shock peened surfaces. Another system simultaneously irradiates opposite sides of the workpiece to form a set of laterally offset laser shock peened surfaces.
    • 提供各种激光冲击处理系统,以在工件内建立选择性压缩残余应力分布轮廓。 可以通过燃气涡轮发动机翼型件的薄部分的厚度形成非对称应力分布。 一个系统被配置为同时用一组激光束照射工件以形成相应的一组相邻的不重叠的激光冲击喷丸表面,使得冲击波彼此相遇。 另一种系统在不同时间照射工件的相对侧,以形成相对的激光冲击喷丸表面,使得冲击波在远离中平面的位置处相遇。 另一个系统使用具有不同脉冲长度的激光束同时照射工件的相对侧,以形成相对的激光冲击喷丸表面。 另一个系统同时照射工件的相对侧,以形成一组侧向偏移的激光冲击喷丸表面。