Simultaneous offset dual sided laser shock peening with oblique angle laser beams
    13.
    发明公开
    Simultaneous offset dual sided laser shock peening with oblique angle laser beams 审中-公开
    激光激光打标机激光打火机

    公开(公告)号:EP1288317A1

    公开(公告)日:2003-03-05

    申请号:EP02255623.7

    申请日:2002-08-13

    IPC分类号: C21D10/00 B23K26/00 F01D5/28

    摘要: A method to laser shock peen articles such as a gas turbine engine rotor blade (108) with first and second oblique laser beams (102, 104) to form pairs of longitudinally spaced apart (LD) first and second laser shock peened elliptical spots (60) that are on opposite sides of the article or blade (108) and transversely offset (OS) from each other. The oblique laser beams (102, 104) are fired at a portion of the leading or trailing edges (LE, TE) of the blade (108) at first and second oblique angles (110, 111) with respect to opposite surfaces of the edge. Another method laser shock peens the leading and trailing edges (LE, TE) of gas turbine engine integrally bladed rotors and disks that are blocked by other rows of blades by firing the laser beams at compound angles such that the beams are aimed at the first and second oblique angles (110, 111) with respect to the surfaces of the edge and at a third oblique angle with respect to a rotor axis (9).

    摘要翻译: 一种激光冲击片材制品的方法,例如具有第一和第二倾斜激光束(102,104)的燃气涡轮发动机转子叶片(108),以形成一对纵向间隔开的(LD)第一和第二激光冲击喷丸椭圆形点 ),其在物品或叶片(108)的相对侧上并且彼此横向偏移(OS)。 倾斜的激光束(102,104)相对于边缘的相对表面在第一和第二倾斜角(110,111)处在叶片(108)的前缘或后缘(LE,TE)的一部分处被烧制 。 激光冲击的另一种方法是燃烧涡轮发动机的前缘和后缘(LE,TE)通过以复合角度激发激光束而被其他行的叶片阻挡的整个叶片的转子和盘,使得梁朝向第一和 相对于所述边缘的表面和相对于转子轴线(9)以第三倾斜角度的第二倾斜角(110,111)。