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Turbomachine hollow vane equipped with primary and secondary disturbers

机译:配备一级和二级干扰器的涡轮机空心叶片

摘要

Hollow blade (10) of a turbomachine (100), said blade comprising a cooling circuit (12), a wall (13) of the internal circuit (12) having at least one rib forming a primary disturbance (14) configured to disturb a flow cooling circulating within the cooling circuit (12), the primary disturbance having a cross section in the form of a first quadrilateral, the primary disturbance (14) being provided with at least one rib and / or at least one groove forming a secondary disturbance (16) configured to disturb the cooling flow within the cooling circuit (12), the secondary disturbance (16) having a cross section in the form of a second quadrilateral. Figure for the abstract: Fig. 2.
机译:涡轮机(100)的中空叶片(10),所述叶片包括冷却回路(12),内部回路(12)的壁(13)具有至少一个肋,该肋形成主扰动(14),该主扰动被配置为扰动发动机在冷却回路(12)内循环的流动冷却,主要扰动具有第一四边形形式的横截面,主要扰动(14)设有至少一个肋和/或至少一个形成次扰动的凹槽(16)构造成扰动冷却回路(12)内的冷却流,次级扰动(16)具有第二四边形形式的横截面。图为摘要:图2。

著录项

  • 公开/公告号FR3089549A1

    专利类型

  • 公开/公告日2020-06-12

    原文格式PDF

  • 申请/专利权人 SAFRAN AIRCRAFT ENGINES;

    申请/专利号FR1872505

  • 发明设计人 PAUL OLIVIER DANRE;JEAN-LUC BACHA;

    申请日2018-12-07

  • 分类号F01D5/08;F01D5/18;

  • 国家 FR

  • 入库时间 2022-08-21 11:00:24

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