Methods and apparatus for modeling gas turbine engine combustor liners
    2.
    发明授权
    Methods and apparatus for modeling gas turbine engine combustor liners 失效
    燃气轮机发动机燃烧器衬套建模方法和装置

    公开(公告)号:US06629415B2

    公开(公告)日:2003-10-07

    申请号:US10029364

    申请日:2001-10-27

    IPC分类号: F02G300

    摘要: A method for fabricating a three-dimensional turbine engine combustor liner model includes coupling at least a first member to a second member to form an assembly that has an inner surface. The assembly inner surface simulates an inner surface of the aircraft engine combustor liner. The first member is at least one of a pre-formed conical member and a pre-formed cylindrical member, and the second portion is at least one of a pre-formed conical member and a pre-formed cylindrical member. The method also includes coupling the assembly to a baseplate, and coupling a plurality of templates to the assembly.

    摘要翻译: 一种用于制造三维涡轮发动机燃烧器衬套模型的方法包括将至少第一构件联接到第二构件以形成具有内表面的组件。 组件内表面模拟飞行器发动机燃烧器衬套的内表面。 第一构件是预成形的圆锥形构件和预成形的圆柱形构件中的至少一个,并且第二部分是预成形的圆锥构件和预成形的圆柱构件中的至少一个。 该方法还包括将组件联接到基板,以及将多个模板耦合到组件。