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COMPONENT OF TURBINE (VERSIONS), TURBINE AND PROCEDURE FOR TURBINE COMPONENT COATING

机译:涡轮组件(版本),涡轮以及涡轮组件涂层的程序

摘要

FIELD: machine building.;SUBSTANCE: component of turbine consists of root, neck, platform and aerodynamic profile with external and internal surfaces defining cooling pass channels. According to one version the root of turbine component has one first coating, while the neck has the second coating. Also, composition of the first coating differs from the composition of the second coating. According to another version internal surface is covered with the first coating, while external surface is covered with the second coating; the first and second coating have different compositions. The third coating different from the first and the second one covers the platform and/or a lower side of the platform. The neck is covered with the fourth coating different from the third coating; the root is covered with the fifth coating different from the fourth coating. According to another one version the neck is covered with the first coating, a bottom of the platform is covered with the second coating; also, the first and the second coating are of different compositions. Internal surface is covered with the fourth coating, while the root is covered with the fifth coating corresponding in particular to a diffusion aluminide, aluminised layer, chromised layer or aluminised and chromised layer, also, the fifth coating differs from the fourth coating. Another invention of the group refers to a turbine containing the first step of working and guiding blades and the second step of working and guiding blades where the working blades of the first and second steps correspond to above said turbine components. Another invention of the group refers to procedure for coating the turbine component consisting in applying the first coating on all external and internal surfaces of the component, in applying the second coating on the first part of the coated component, and in applying the third coating on the second part of the coated component; also, the first, second and third coatings have different compositions.;EFFECT: increased reliability of turbine component.;90 cl, 15 dwg
机译:领域:机械制造;实质:涡轮的组成部分包括根部,颈部,平台和空气动力学轮廓,其内外表面定义了冷却通道。根据一种形式,涡轮机部件的根部具有一个第一涂层,而颈部具有第二涂层。同样,第一涂层的组成不同于第二涂层的组成。根据另一种形式,内表面覆盖有第一涂层,而外表面覆盖有第二涂层。第一和第二涂层具有不同的组成。与第一和第二涂层不同的第三涂层覆盖平台和/或平台的下侧。颈部覆盖有不同于第三涂层的第四涂层;根部被不同于第四涂层的第五涂层覆盖。根据另一种形式,颈部覆盖有第一涂层,平台的底部覆盖有第二涂层。同样,第一涂层和第二涂层具有不同的组成。内表面被第四涂层覆盖,而根部被第五涂层覆盖,特别是对应于扩散铝化物,渗铝层,铬化层或渗铝和铬化层,第五涂层也不同于第四涂层。该组的另一项发明涉及一种涡轮,其包括工作叶片和导向叶片的第一步骤以及工作叶片和导向叶片的第二步骤,其中第一步骤和第二步骤的工作叶片对应于所述涡轮机部件的上方。该组的另一项发明涉及涂覆涡轮机部件的步骤,该方法包括在部件的所有外表面和内表面上涂覆第一涂层,在涂覆部件的第一部分上涂覆第二涂层,以及在部件上涂覆第三层涂层。涂层成分的第二部分;同样,第一,第二和第三涂层的成分也不同。效果:提高了涡轮机组件的可靠性; 90 cl,15 dwg

著录项

  • 公开/公告号RU2414603C2

    专利类型

  • 公开/公告日2011-03-20

    原文格式PDF

  • 申请/专利权人 SIMENS AKTSIENGEZELLSHAFT;

    申请/专利号RU20080152090

  • 发明设计人 BOKS POL (GB);UAJTKHERST MIK (GB);

    申请日2006-06-08

  • 分类号F01D5/28;

  • 国家 RU

  • 入库时间 2022-08-21 17:48:31

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