首页> 外国专利> Foundry method for fabricating jet engine blade, involves manufacturing shell whose additional part is arranged on another part, where additional part is plane and perpendicular to vertical axis of latter part

Foundry method for fabricating jet engine blade, involves manufacturing shell whose additional part is arranged on another part, where additional part is plane and perpendicular to vertical axis of latter part

机译:用于制造喷气发动机叶片的铸造方法,涉及制造壳体,该壳体的附加部件布置在另一部件上,其中附加部件是平面并且垂直于该部件的竖直轴线

摘要

The method involves manufacturing a wax spray having models of part to be fabricated, and manufacturing a shell (302) around the spray. The shell has an additional part (90) that is arranged on a part (32) of the shell while manufacturing the shell. The additional part is plane and perpendicular to a vertical axis (22) of the part (32). The part (32) is formed around a central shaft of the spray. Independent claims are also included for the following: (A) a spray for implementing the foundry method (B) a shell for implementing the foundry method (C) an aircraft engine equipped with a jet engine blade.
机译:该方法包括制造具有将要制造的零件模型的蜡喷雾,以及围绕该喷雾制造外壳(302)。壳体具有附加部分(90),该附加部分在制造壳体时布置在壳体的一部分(32)上。附加部分是平面并且垂直于部分(32)的垂直轴(22)。部件(32)围绕喷雾的中心轴形成。还包括以下方面的独立权利要求:(A)用于实施铸造方法的喷雾剂(B)用于实施铸造方法的壳体(C)配备有喷气发动机叶片的飞机发动机。

著录项

  • 公开/公告号FR2874340A1

    专利类型

  • 公开/公告日2006-02-24

    原文格式PDF

  • 申请/专利权人 SNECMA MOTEURS SOCIETE ANONYME;

    申请/专利号FR20040051878

  • 发明设计人 FARGEAS SERGE;

    申请日2004-08-20

  • 分类号B22C9/04;B22C9/20;B22D27/04;

  • 国家 FR

  • 入库时间 2022-08-21 21:17:24

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