Design of a Small-Scale, High-Rotational-Speed Centrifugal Compressor Operating with R-290

The current work highlights key challenges in the design of small-scale, high-rotational-speed centrifugal compressors for R-290 at domestic application scale on the basis of a single-stage demonstrator unit that is currently developed by ebm-papst. The demonstrator is operated in a vapor-compression cycle at a total pressure ratio up to 3, a maximum rotational speed of 240 krpm, and with maximum power supply of 3.2 kWe. Emphasis is placed on challenges related to aerodynamic stage design, impeller back wall sealing, and impeller thrust force balancing. Appropriate measures are proposed to overcome these challenges and compressor performance is quantified to evaluate the prospects of small-scale, centrifugal compressors for R-290 application in a wider context. Considerations related to mechanical design and manufacturing are briefly illustrated. Main design and performance assessments are conducted through 3D CFD RANS calculations.

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Publication Details

Journal
International Journal of Turbomachinery Propulsion and Power
Published
2025-12-17
DOI
https://doi.org/10.3390/ijtpp10040052
Primary Topic
Turbomachinery Performance and Optimization
Type
article
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article

Design of a Small-Scale, High-Rotational-Speed Centrifugal Compressor Operating with R-290

Sönke Teichel, Ahmet Çokşen, Renan Emre Karaefe
International Journal of Turbomachinery Propulsion and Power
Turbomachinery Performance and Optimization
article

Design of a Small-Scale, High-Rotational-Speed Centrifugal Compressor Operating with R-290

Sönke Teichel, Ahmet Çokşen, Renan Emre Karaefe
article en

Abstract

The current work highlights key challenges in the design of small-scale, high-rotational-speed centrifugal compressors for R-290 at domestic application scale on the basis of a single-stage demonstrator unit that is currently developed by ebm-papst. The demonstrator is operated in a vapor-compression cycle at a total pressure ratio up to 3, a maximum rotational speed of 240 krpm, and with maximum power supply of 3.2 kWe. Emphasis is placed on challenges related to aerodynamic stage design, impeller back wall sealing, and impeller thrust force balancing. Appropriate measures are proposed to overcome these challenges and compressor performance is quantified to evaluate the prospects of small-scale, centrifugal compressors for R-290 application in a wider context. Considerations related to mechanical design and manufacturing are briefly illustrated. Main design and performance assessments are conducted through 3D CFD RANS calculations.

International Journal of Turbomachinery Propulsion and PowerVol. 10(4)
ebm-papst (DE)
Openalex Percentile: Top 48%
Turbomachinery Performance and Optimization
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