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Journal ArticleDOI

Numerical Investigation of the Effect of Different Back Sweep Angle and Exducer Width on the Impeller Outlet Flow Pattern of a Centrifugal Compressor With Vaneless Diffuser

Andre Hildebrandt, +1 more
- 01 Jan 2006 - 
- Vol. 129, Iss: 2, pp 1077-1086
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TLDR
In this article, the effect of different back sweep angles and exducer widths on the steady-state impeller outlet flow pattern of a centrifugal compressor with a vaneless diffuser was investigated.
Abstract
This paper presents a numerical investigation of the effect of different back sweep angles and exducer widths on the steady-state impeller outlet flow pattern of a centrifugal compressor with a vaneless diffuser. The investigations have been performed with commercial computational fluid dynamics (CFD) and in-house programmed one-dimensional (ID) codes. CFD calculations aim to investigate how flow pattern from the impeller is quantitatively influenced by compressor geometry parameters; thereby, the location of wake and its magnitude (flow angle and relative velocity magnitude) are analyzed. Results show that the increased back sweep impeller provides a more uniform flow pattern in terms of velocity and flow deviation angle distribution, and offers better potential for the diffusion process inside a vaneless (or vaned) diffuser Secondary flux fraction and flow deviation angle from CFD simulation are implemented into the ID two-zone program to improve ID prediction results. (Less)

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Citations
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Journal ArticleDOI

Impeller Design of a Centrifugal Fan with Blade Optimization

TL;DR: In this article, a method is presented for redesigning a centrifugal impeller and its inlet duct, which is geared towards meeting the design volute exit pressure while reducing the power required to operate the fan.
Journal ArticleDOI

Small-scale turbocompressors for wide-range operation with large tip-clearances for a two-stage heat pump concept

TL;DR: This paper will guide the readers through different stages of the design process of small-scale turbocompressors subjected to different operational and design constraints and help the designers make suitable parameter selections for achieving high efficiency and wide compressor operating range.
Patent

Flow control structures for turbomachines and methods of designing the same

David Japikse
TL;DR: Flow control devices and structures designed and configured to improve the performance of a turbomachine are discussed in this paper, where they include various flow guiding channels, ribs, diffuser passage width reductions, and other treatments and may be located on one or both of a shroud and hub side of a machine.
Journal ArticleDOI

A numerical study of the effects of blade angle distribution on the performance and loss generation of centrifugal compressor impellers

TL;DR: The blade angle distribution from the inlet to outlet of an impeller in a centrifugal compressor is known to have significant influence on its flow characteristics as mentioned in this paper, and it is known that the angle distribution can affect the flow characteristics of the compressor.
References
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Journal ArticleDOI

A Theoretical Model for Rotating Stall in the Vaneless Diffuser of a Centrifugal Compressor

TL;DR: In this article, a theoretical model for rotating stall in the vaneless diffuser of a centrifugal compressor is presented, which consists of a time-evolutive calculation of the strong interaction between the inviscid flow core and the unsteady boundary layers along the walls.
Journal ArticleDOI

Analysis of Secondary Flows in Centrifugal Impellers

TL;DR: In this paper, a model based on the vorticity equation for a rotating system was developed to determine the streamwise vortivities from the normal and binormal vortic components, which are known from the meridional flow profile.
Journal ArticleDOI

Investigation of an Inversely Designed Centrifugal Compressor Stage: Part 1 — Design and Numerical Verification

TL;DR: In this article, the three-dimensional inverse design code TURBOdesign-1 is applied to the design of the blade geometry of a centrifugal compressor impeller with splitter blades.
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