首页> 外国专利> CENTRIFUGAL IMPELLER, SINGLE-SHAFT MULTIPLE-STAGE CENTRIFUGAL COMPRESSOR USING CENTRIFUGAL IMPELLER, AND CENTRIFUGAL IMPELLER MANUFACTURING METHOD

CENTRIFUGAL IMPELLER, SINGLE-SHAFT MULTIPLE-STAGE CENTRIFUGAL COMPRESSOR USING CENTRIFUGAL IMPELLER, AND CENTRIFUGAL IMPELLER MANUFACTURING METHOD

机译:离心式叶轮,使用离心式叶轮的单轴多级离心式压缩机以及离心式叶轮的制造方法

摘要

PROBLEM TO BE SOLVED: To provide a centrifugal impeller and a single-shaft multistage centrifugal compressor having a wider operating range at low cost while ensuring high performance.SOLUTION: Blades of a centrifugal impeller according to the present invention are constituted by main blades each having a blade shape such that a blade load from a front edge thereof to a throat position is lighter than a blade load from the throat position to a rear edge thereof, and intermediate blades each having a front edge provided downstream of the throat position and shorter than the main blade. The main blades and the intermediate blades are alternately disposed circumferentially between an impeller hub and a shroud facing the impeller hub, the main blades are integrally joined to the impeller hub and the shroud, and the intermediate blades are integrally joined to at least either the impeller hub or the shroud. Furthermore, a single-shaft multistage compressor according to the present invention is configured so that the centrifugal impeller is disposed in at least a most downstream stage.SELECTED DRAWING: Figure 2
机译:解决的问题:提供一种离心式叶轮和单轴多级离心压缩机,其在确保高性能的同时以低成本在较宽的工作范围内。解决方案:根据本发明的离心式叶轮的叶片由主叶片构成,每个主叶片具有叶片形状,使得从其前边缘到喉部位置的叶片载荷比从喉部位置到其后边缘的叶片载荷更轻,中间叶片的前缘设置在喉部位置的下游并且短于主刀片。主叶片和中间叶片在周向交替地布置在叶轮毂和面对叶轮毂的护罩之间,主叶片一体地结合到叶轮毂和护罩,并且中间叶片一体地结合到至少一个叶轮。集线器或导流罩。此外,根据本发明的单轴多级压缩机被构造成使得离心式叶轮至少布置在最下游的级中。

著录项

  • 公开/公告号JP2016033350A

    专利类型

  • 公开/公告日2016-03-10

    原文格式PDF

  • 申请/专利权人 HITACHI LTD;

    申请/专利号JP20140156374

  • 申请日2014-07-31

  • 分类号F04D29/28;F04D17/12;F04D29/30;F04D29/66;

  • 国家 JP

  • 入库时间 2022-08-21 14:44:21

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