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TURBO MACHINE SHOVEL CONTAINING PROTECTIVE INSERT OF SHOVEL TOP

机译:装有防护罩的TURBO机床防护罩

摘要

1. The blade (10) of the rotor of the turbomachine, comprising a housing (12), extending radially relative to the main axis of the rotor of the turbomachine and including: - a radially external end vertex (16), - the surface of the trough (22) located on the side upstream of the housing (12), in the direction of rotation of the rotor; - the leading edge (18) with the main radial orientation, located axially upstream with respect to the gas flow in the turbomachine; and - the rear edge (20) with the main radial orientation, located axially lower in relation to the gas flow in the turbomachine, while the blade (10) contains an insert (26) that covers the top (16) of the housing (12), and the insert ( 26) is formed by the first part (28) that covers the radially apex (16) of the blade (10), and the second part (30) that partially covers the surface of the trough (22) of the blade (10), while the first part (28) of the insert (26) contains an edge located on the side downstream of the blade (10) in the direction of rotation of the rotor and located at the same level with the surface of the back (24) of the housing (12), located on the downstream side of the housing (12) in the direction of rotation of the rotor, characterized in that the cross section of the insert (26) in a plane radial relative to the axis of the rotor has the shape of an angle, the first part ( 28) insert (26) which extends tangentially relative to the main axis of the rotor, and the second part (30) extends generally radially relative to the main axis of the rotor. 2. The rotor blade (10) according to claim 1, characterized in that the second part (30) of the insert (26) extends over the entire axial size of the blade (10) from the leading edge (18) to the trailing edge (20). 3. The rotor blade (10) according to claim 1, characterized in that the second part (30) of the insert (26) has a surface of the trough (32), which is located at the same level with the surface of the trough (22) of the housing (12) .4. Shovel
机译:1.一种涡轮机的转子的叶片(10),其包括壳体(12),所述壳体相对于所述涡轮机的转子的主轴线径向地延伸,并且包括:-径向外端顶点(16),-所述表面位于壳体(12)上游侧的槽(22)沿转子的旋转方向; -具有主要径向方向的前缘(18),位于相对于涡轮机中气流的轴向上游; -具有主要径向方向的后边缘(20),其位置相对于涡轮机中的气流轴向较低,而叶片(10)则包含一个插件(26),该插件(26)覆盖壳体的顶部(16)。插入件(26)由覆盖叶片(10)的径向顶点(16)的第一部分(28)和部分覆盖槽(22)的表面的第二部分(30)形成。插入件(26)的第一部分(28)包含一个沿转子旋转方向位于叶片(10)下游一侧的边缘,并且与壳体(12)的后部(24)的表面沿转子的旋转方向位于壳体(12)的下游侧,其特征在于,插入件(26)的横截面在一个平面中相对于转子的轴线径向具有角度的形状,第一部分(28)插入件(26)相对于转子的主轴线切向地延伸,并且第二部分(30)相对于转子的主轴线大致径向地延伸。 2.根据权利要求1所述的转子叶片(10),其特征在于,所述插入件(26)的第二部分(30)在所述叶片(10)的整个轴向尺寸上从所述前缘(18)延伸到所述后缘边缘(20)。 3.根据权利要求1所述的转子叶片(10),其特征在于,所述插入件(26)的第二部分(30)具有所述槽(32)的表面,所述表面位于与所述槽(32)的表面相同的高度处。外壳(12)的槽(22).4。铲

著录项

  • 公开/公告号RU2014139700A

    专利类型

  • 公开/公告日2016-04-27

    原文格式PDF

  • 申请/专利权人 СНЕКМА (FR);

    申请/专利号RU20140139700

  • 发明设计人 МАРЭН СЕБАСТЬЕН (FR);

    申请日2013-03-06

  • 分类号F01D5/14;

  • 国家 RU

  • 入库时间 2022-08-21 14:11:24

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