发明名称 Process and system for forming shaped air holes
摘要 A process is provided for forming shaped air holes, such as for use in turbine blades. Aspects of the disclosure relate to forming shaped portions of air holes using a short pulse laser, forming a metered hole corresponding to each shaped portion, and separately finishing the shaped portion using a short-pulse laser. In other embodiments, the order of these operations may be varied, such as to form the shaped portions and to finish the shaped portions using the short-pulse laser prior to forming the corresponding metered holes.
申请公布号 US8857055(B2) 申请公布日期 2014.10.14
申请号 US201012697005 申请日期 2010.01.29
申请人 General Electric Company 发明人 Wei Bin;Schaeffer Jon Conrad;Bunker Ronald Scott;Zhang Wenwu;Morey Kathleen Blanche;Lipkin Jane Marie;Lacy Benjamin Paul;Scheidt Wilbur Douglas
分类号 B21D53/78;B21K3/04;B23P15/02;F02C7/18;F01D25/12;B23K26/38;B23K26/06;B23K26/30;B23K26/08 主分类号 B21D53/78
代理机构 代理人 Agosti Ann M.
主权项 1. A method for forming shaped holes, comprising: forming a plurality of shaped portions of air holes in a turbine component using a first short-pulse laser; after forming the plurality of shaped portions, then forming a plurality of metered holes through the turbine component extending from the shaped portions of the air holes to an inner cavity of the turbine component, wherein each metered hole corresponds to one of the plurality of shaped portions of air holes; and after forming the plurality of metered holes, then finishing the air holes by smoothing, applying surface textures, and/or applying surface contours to the respective shaped portions.
地址 Niskayuna NY US