首页> 外国专利> Structures and methods for forcing coupling of flow fields of adjacent bladed elements of turbomachines, and turbomachines incorporating the same

Structures and methods for forcing coupling of flow fields of adjacent bladed elements of turbomachines, and turbomachines incorporating the same

机译:用于迫使涡轮机的相邻叶片元件的流场耦合的结构和方法,以及包括该结构和方法的涡轮机

摘要

Turbomachines having close-coupling flow guides (CCFGs) that are designed and configured to closely-couple flow fields of adjacent bladed elements. In some embodiments, the CCFGs may be located in regions extending between the adjacent bladed elements, described herein as coupling avoidance zones, where conventional turbomachine design would suggest no structure should be added. In yet other embodiments, CCFGs are located upstream and/or downstream of rows of blades coupled to the bladed elements, including overlapping one of more of the rows of blades, to improve flow coupling and machine performance. Methods of designing turbomachines to incorporate CCFGs are also provided.
机译:具有紧密耦合导流器(CCFG)的涡轮机,其设计和配置为紧密耦合相邻叶片元件的流场。在一些实施例中,CCFG可位于在相邻叶片元件之间延伸的区域中,在本文中被描述为联接避免区域,在该区域中常规涡轮机械设计将建议不添加任何结构。在其他实施例中,CCFG位于联接至带叶片元件的叶片排的上游和/或下游,包括与叶片排中的一个或多个重叠,以改善流动联接和机器性能。还提供了设计涡轮机以结合CCFG的方法。

著录项

  • 公开/公告号US10590951B2

    专利类型

  • 公开/公告日2020-03-17

    原文格式PDF

  • 申请/专利权人 CONCEPTS NREC LLC;

    申请/专利号US201615379912

  • 发明设计人 DAVID JAPIKSE;

    申请日2016-12-15

  • 分类号F04D29/44;F01D5/22;F01D9/04;F04D29/24;F04D29/54;F04D29/16;F04D29/68;B23P15;F01D5/14;F01D25/06;F04D29/28;F04D29/32;F04D29/38;F04D29/66;F04D1;F04D17/10;

  • 国家 US

  • 入库时间 2022-08-21 11:30:41

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