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    Experimental Study on the Effect of Diffuser Vane Setting Angle on Centrifugal Compressor Performance 

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 006:;page 61001
    Author(s): Tamaki, Hideaki
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effect of the diffuser vane setting angle on the performance of a centrifugal compressor was experimentally investigated. Seven different vaned diffusers were tested with the same impeller. In order to evaluate the ...
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    A Study on Matching Between Centrifugal Compressor Impeller and Low Solidity Diffuser and Its Extension to Vaneless Diffuser 

    Source: Journal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 004:;page 41026
    Author(s): Tamaki, Hideaki
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A centrifugal compressor requires a wide operating range as well as a high efficiency. At high pressure ratios, the impeller discharge velocity becomes transonic and effective pressure recovery in a vaned or vaneless ...
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    A Method for Preliminary Design of Variable Geometry Vaned Diffuser for Centrifugal Compressor 

    Source: Journal of Turbomachinery:;2023:;volume( 146 ):;issue: 003:;page 31014-1
    Author(s): Tamaki, Hideaki; Yamaguchi, Satoshi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Centrifugal compressors require a wide operating range as well as high efficiency. Typical active control forms to enhance the operating range are suction throttling with a valve in a suction line, discharge throttling ...
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    Experimental Investigation of High Pressure Ratio Centrifugal Compressor With Axisymmetric and Nonaxisymmetric Recirculation Device 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 003:;page 31023
    Author(s): Tamaki, Hideaki; Zheng, Xinqian; Zhang, Yangjun
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Centrifugal compressors used for turbochargers are required to have a wide operating range. A recirculation device, which consists of a bleed slot, an upstream slot, and an annular cavity connecting both slots, is often ...
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    Stability Improvement of High Pressure Ratio Turbocharger Centrifugal Compressor by Asymmetrical Flow Control—Part II: Nonaxisymmetrical Self Recirculation Casing Treatment 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 002:;page 21007
    Author(s): Zheng, Xinqian; Zhang, Yangjun; Yang, Mingyang; Bamba, Takahiro; Tamaki, Hideaki
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This is part II of a twopart paper involving the development of an asymmetrical flow control method to widen the operating range of a turbocharger centrifugal compressor with highpressure ratio. A nonaxisymmetrical ...
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    A Transonic Mixed Flow Compressor for an Extreme Duty 

    Source: Journal of Turbomachinery:;2015:;volume( 137 ):;issue: 005:;page 51010
    Author(s): Hazby, Hamid; Casey, Michael; Numakura, Ryusuke; Tamaki, Hideaki
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes the design of a transonic mixed flow compressor stage for an extreme duty, with an extremely high flow coefficient (د†) of 0.25 and a high isentropic pressure rise coefficient (دˆ) of 0.56. The impeller ...
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    Effects of Blade Deformation on the Performance of a High Flow Coefficient Mixed Flow Impeller 

    Source: Journal of Turbomachinery:;2015:;volume( 137 ):;issue: 012:;page 121005
    Author(s): Hazby, Hamid; Woods, Ian; Casey, Michael; Numakura, Ryusuke; Tamaki, Hideaki
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effects of blade deformation under running conditions on the performance of a highly loaded transonic mixed flow impeller were investigated. Two impellers were manufactured, one using the “runningâ€‌ blade profiles ...
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    Enhancement of Centrifugal Compressor Operating Range by Control of Inlet Recirculation With Inlet Fins 

    Source: Journal of Turbomachinery:;2016:;volume( 138 ):;issue: 010:;page 101010
    Author(s): Tamaki, Hideaki; Unno, Masaru; Tanaka, Ryuuta; Yamaguchi, Satoshi; Ishizu, Yohei
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The operating points of a turbocharger compressor tend to approach or cross its surge line while an engine is accelerating, particularly under lowengine speed conditions, hence the need for an acceptable surge margin under ...
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    Stability Improvement of a Turbocharger Centrifugal Compressor by a Nonaxisymmetric Vaned Diffuser 

    Source: Journal of Turbomachinery:;2018:;volume 140:;issue 004:;page 41007
    Author(s): Zheng, Xinqian; Sun, Zhenzhong; Kawakubo, Tomoki; Tamaki, Hideaki
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The nonuniformity of the flow field induced by a nonaxisymmetric volute significantly degrades the stability of a turbocharger centrifugal compressor. In this paper, a nonaxisymmetric vaned diffuser is investigated as a ...
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    Stability Improvement of High Pressure Ratio Turbocharger Centrifugal Compressor by Asymmetric Flow Control—Part I: Non Axisymmetrical Flow in Centrifugal Compressor 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 002:;page 21006
    Author(s): Yang, Mingyang; Zheng, Xinqian; Zhang, Yangjun; Bamba, Takahiro; Tamaki, Hideaki; Huenteler, Joern; Li, Zhigang
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This is Part I of a twopart paper documenting the development of a novel asymmetric flow control method to improve the stability of a highpressureratio turbocharger centrifugal compressor. Part I focuses on the nonaxisymmetrical ...
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