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Journal articles on the topic 'Centrifugal Compressor'

Author: Grafiati

Published: 4 June 2021

Last updated: 26 July 2025

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1

Harasymiv, V. M., O. V. Moiseenko, and T. G. Harasymiv. "Application and algorithmic software of the control system of the technical state parameters of the two-stage centrifugal compressor." METHODS AND DEVICES OF QUALITY CONTROL, no. 1(44) (June 28, 2020): 110–18. http://dx.doi.org/10.31471/1993-9981-2020-1(44)-110-118.

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Efficiency of the technical state of the compressor station basic components depends on the timely prediction of the appearance of damages. It is defined by the estimation of the technical state of the basic components during the compression process. It is known that the two-stage centrifugal compressors are commonly used in the Ukrainian compressor stations. So, application software and algorithm for the two-stage centrifugal compressor have been developed, what allows to define its technical state parameters, taking into account the construction features of the compressor volute. The algorit

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2

Smolarik, Lukas, Dusan Mudroncik, and Milan Strbo. "Compressor and Throttle Characteristics for Models." Applied Mechanics and Materials 404 (September 2013): 200–206. http://dx.doi.org/10.4028/www.scientific.net/amm.404.200.

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Turbocharger is a device used for compression of gases of different features. I tis a conversion of kinetic energy or mechanical energy into pressure. Compressed media can be vary from pure gases such as hydrogen, oxygen, noble gases to the gas mixtures such as air, a mixture, of hydrogen and others. Gas composition is very important because of its physical and chemical properties depends on many parameters of compressor design [. The basis of modelling surge dynamics of centrifugal compressors is Greitzerov nonlinear model. This article is getting the gear characteristics of the mass flow and

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3

Danilishin, A. M., and Y. V. Kozhukhov. "Centrifugal Compressors Gas-Dynamic Characteristics Influence on the Refrigerating Machines Efficiency." Problems of the Regional Energetics, no. 2(58) (May 2023): 72–80. http://dx.doi.org/10.52254/1857-0070.2023.2-58-07.

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The article is devoted to the study R134a refrigerating machine efficiency and consisting of a centrifugal compressor, a condenser, a temperature-regulating valve and an evaporator. The main purpose of the work is to analyze the centrifugal compressor gas dynamic characteristics effect on the refrigeration machine vapor-compression cycle efficiency. This goal is achieved through the study by actual working process numerical experiment in the refrigeration machine centrifugal compressor with an idealized process for other elements. The object of the study are the refrigeration machine character

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4

Xu, Cheng, and Ryoichi S. Amano. "Empirical Design Considerations for Industrial Centrifugal Compressors." International Journal of Rotating Machinery 2012 (2012): 1–15. http://dx.doi.org/10.1155/2012/184061.

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Computational Fluid Dynamics (CFD) has been extensively used in centrifugal compressor design. CFD provides further optimisation opportunities for the compressor design rather than designing the centrifugal compressor. The experience-based design process still plays an important role for new compressor developments. The wide variety of design subjects represents a very complex design world for centrifugal compressor designers. Therefore, some basic information for centrifugal design is still very important. The impeller is the key part of the centrifugal stage. Designing a highly efficiency im

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5

Motriuk, R. W., and D. P. Harvey. "Centrifugal Compressor Modifications and Their Effect on High-Frequency Pipe Wall Vibration." Journal of Pressure Vessel Technology 120, no. 3 (1998): 276–82. http://dx.doi.org/10.1115/1.2842058.

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High-frequency pulsation generated by centrifugal compressors, with pressure wavelengths much smaller than the attached pipe diameter, can cause fatigue failures of the compressor internals, impair compressor performance, and damage the attached compressor piping. There are numerous sources producing pulsation in centrifugal compressors. Some of them are discussed in literature at large (Japikse, 1995; Niese, 1976). NGTL has experienced extreme high-frequency discharge pulsation and pipe wall vibration on many of its radial inlet high-flow centrifugal gas compressor facilities. These pulsation

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6

Raman, Senthil, and Heuy Kim. "Computational Analysis of the Performance Characteristics of a Supercritical CO2 Centrifugal Compressor." Computation 6, no. 4 (2018): 54. http://dx.doi.org/10.3390/computation6040054.

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A centrifugal compressor working with supercritical CO 2 (S-CO 2 ) has several advantages over other supercritical and conventional compressors. S-CO 2 is as dense as the liquid CO 2 and becomes difficult to compress. Thus, during the operation, the S-CO 2 centrifugal compressor requires lesser compression work than the gaseous CO 2 . The performance of S-CO 2 compressors is highly varying with tip clearance and vanes in the diffuser. To improve the performance of the S-CO 2 centrifugal compressor, knowledge about the influence of individual components on the performance characteristics is nec

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7

ASLANOV, Jamaladdin, and Tarlan FARAJOV. "FAILURES IN CENTRIFUGAL COMPRESSORS." Machine Science Journal 4, no. 2 (2024): 50–58. https://doi.org/10.61413/fcbe3989.

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Centrifugal flash gas compressors are mechanisms that convert the kinetic energy of gas into pressure energy, playing a crucial role in compressing and transporting associated gases in the oil and gas industry. These compressors operate on the principle of centrifugal force and are widely used in key industrial sectors. They are considered essential equipment for compressing and transporting gases in fields such as the oil and gas industry, chemical production, power generation, and cooling systems. Capable of handling high flow rates and large volumes, centrifugal compressors use impellers to

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8

Yu Dong, Xu, Li Cong, Lv Qiong Ying, Zhang Xin Ming, and Mu Guo Zhen. "The influence of the trailing edge angle of the micro centrifugal impeller on the performance of the centrifugal compressor." International Journal of Applied Electromagnetics and Mechanics 66, no. 4 (2021): 619–33. http://dx.doi.org/10.3233/jae-201590.

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In order to study the effect of the trailing edge sweep angle of the centrifugal impeller on the aerodynamic performance of the centrifugal compressor, 6 groups of centrifugal impellers with different bending angles and 5 groups of different inclination angles were designed to achieve different impeller blade trailing edge angle. The computational fluid dynamics (CFD) method was used to simulate and analyze the flow field of centrifugal compressors with different blade shapes under design conditions. The research results show that for transonic micro centrifugal compressors, changing the blade

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9

Lebedev, A. A., A. A. Aksenov, S. M. Lebedeva, A. Yu Petrov, and Minh Hai Nguyen. "Improving the reliability of the compressor unit using the wavelet transform method." E3S Web of Conferences 140 (2019): 05013. http://dx.doi.org/10.1051/e3sconf/201914005013.

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Centrifugal compressors are an integral part of modern production in such industries as gas transmission, oil refining, metallurgical, machine-building, mining, as well as in electric and heat power engineering. Interruptions in the operation or failures of compressors lead to decrease in profit or large material loss. Conditions should be created for the safe (stable) operation of centrifugal compressors. Surge is global (complete) loss of stability, an unacceptable phenomenon for a centrifugal compressor. Compressor surge protection must function during operation. The algorithms used to prot

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10

Shikar Mammadov, Gunel Karimova, Shikar Mammadov, Gunel Karimova. "EFFECT OF VIBRATION ON CENTRIFUGAL COMPRESSOR." PAHTEI-Procedings of Azerbaijan High Technical Educational Institutions 39, no. 04 (2024): 442–49. http://dx.doi.org/10.36962/pahtei39042024-442.

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Centrifugal compressors play a critical role in various industrial applications, including oil and gas, petrochemical, and aerospace industries. These machines are subjected to various operating conditions, including mechanical vibrations, which can significantly affect their performance, reliability, and longevity. Centrifugal compressors often face challenges related to mechanical vibrations, which can compromise performance and reliability. This article provides a comprehensive review of the effects of vibration on centrifugal compressors, covering the mechanisms of vibration generation, it

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11

Zou, Wangzhi, Xiao He, Wenchao Zhang, Zitian Niu, and Xinqian Zheng. "Roles of vanes in diffuser on stability of centrifugal compressor." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233, no. 14 (2019): 5380–92. http://dx.doi.org/10.1177/0954410019844433.

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The stability considerations of centrifugal compressors become increasingly severe with the high pressure ratios, especially in aero-engines. Diffuser is the major subcomponent of centrifugal compressor, and its performance greatly influences the stability of compressor. This paper experimentally investigates the roles of vanes in diffuser on component instability and compression system instability. High pressure ratio centrifugal compressors with and without vanes in diffuser are tested and analyzed. Rig tests are carried out to obtain the compressor performance map. Dynamic pressure measurem

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12

Al Ghafri, Yazeed Sulaiman, and Aydin Azizi. "Centrifugal Compressor Behavior in Upstream Business." Applied Mechanics and Materials 823 (January 2016): 459–64. http://dx.doi.org/10.4028/www.scientific.net/amm.823.459.

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Centrifugal compressors are critical rotating equipments in industrial processes, especially for natural gas applications. Compressible gas exhibit complex flow behavior that requires a thorough understanding to ensure extended, safe and stabilized compressor performance. Without, Centrifugal compressors can undergo surge which restricts compressor operational range and jeopardize the safety of its components. Dynamic simulation then becomes necessary to evaluate performance and to implement integrated control schemes. This paper will investigate how centrifugal compressor responds to changes

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13

Spakovszky, Z. S. "Backward Traveling Rotating Stall Waves in Centrifugal Compressors." Journal of Turbomachinery 126, no. 1 (2004): 1–12. http://dx.doi.org/10.1115/1.1643382.

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Rotating stall waves that travel against the direction of rotor rotation are reported for the first time and a new, low-order analytical approach to model centrifugal compressor stability is introduced. The model is capable of dealing with unsteady radially swirling flows and the dynamic effects of impeller-diffuser component interaction as it occurs in centrifugal compression systems. A simple coupling criterion is developed from first principles to explain the interaction mechanism important for system stability. The model findings together with experimental data explain the mechanism for fi

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14

Kang, Hyun-Su, Sung-Yeon Kim, and Youn-Jea Kim. "Wet Compression Study for an Aero-Thermodynamic Performance Analysis of a Centrifugal Compressor at Design and Off-Design Points." Processes 10, no. 5 (2022): 936. http://dx.doi.org/10.3390/pr10050936.

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In this study, to analyze the effect of wet compression technology on the aero-thermodynamic performance of a centrifugal compressor, a numerical analysis study was conducted on the design point and off-design point. Wet compression technology sprays water droplets at the inlet of the compressor. During the compression process, water droplets evaporate, reducing the heat of compression and reducing the compression work, which improves the efficiency of the compressor. In wet compression technology, detailed research is needed for the application to compressors because the droplet behavior affe

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15

Fan, Tengbo, Baotong Wang, Chuanxiang Yan, Wenchao Zhang, Zhaoyun Song, and Xinqian Zheng. "Effect of Self-Recirculating Casing Treatment on the Aerodynamic Performance of Ultra-High-Pressure-Ratio Centrifugal Compressors." Processes 11, no. 8 (2023): 2439. http://dx.doi.org/10.3390/pr11082439.

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The motivation to design a more efficient and compact aircraft engine leads to a continuous increase in overall pressure ratio and decrease in the stage number in compressors. Compared to the traditional multi-stage compressor, a single-stage ultra-high-pressure-ratio centrifugal compressor with a pressure ratio higher than 10.0 can significantly improve the engine’s power-to-weight ratio and fuel economy with a reduced structure complexity. Thus, it has great potential to be adopted in the compression system of advanced aero engines, such as turboshaft engines, in the future. However, the hig

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16

Zhu, Jin Fang. "Fault Tree Analysis of Centrifugal Compressor." Key Engineering Materials 474-476 (April 2011): 1587–90. http://dx.doi.org/10.4028/www.scientific.net/kem.474-476.1587.

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Centrifugal compressor is one of the most typical equipment of all rotary machinery equipment, which is used widely and largely in petrochemical settings. Thus it is necessary to study the reliability of centrifugal compressor. The fault tree has been introduced and applied to the practical facilities. The reliability of centrifugal compressor also has been analyzed. Qualitative analysis aims to find the minimum cut and calculate the failure probability of compressors.

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17

Yang, Zimu, Hongsheng Jiang, Weilin Zhuge, Yuping Qian, and Yangjun Zhang. "Investigation on unsteady characteristics of flow separation in a supercritical carbon dioxide centrifugal compressor." Journal of Physics: Conference Series 2707, no. 1 (2024): 012004. http://dx.doi.org/10.1088/1742-6596/2707/1/012004.

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Abstract As one of the core components of supercritical carbon dioxide (S-CO2) closed Brayton cycle, the efficiency of S-CO2 centrifugal compressor plays a crucial role. Affected by the special thermophysical properties of S-CO2 fluid, the flow mechanism of S-CO2 centrifugal compressor is different from the centrifugal compressor of conventional fluid, such as air. Previous studies have found that the flow separation within the flow domain of this kind of compressor is easily to occur downstream the pressure surface. Many steady computational fluid dynamics (CFD) studies have been conducted on

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18

A P, Yashwant, Tanushree Kale, Nikita Mane, Purva Rupavate, and Gaurav Bankar. "Working Model of Turbojet Engine." International Scientific Journal of Engineering and Management 03, no. 12 (2024): 1–7. https://doi.org/10.55041/isjem02148.

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The project made to show the working model of Turbojet Engine. The turbojet engine operates on the Brayton cycle and features four primary stages: air intake, compression, combustion, and exhaust. The turbo-jet engine is for high speeds. The working model shows how atmospheric air is taken in and compressed using a multi-stage axial or centrifugal compressor. The compressed air then enters the combustion chamber, where it mixes with fuel and undergoes ignition, producing high-energy exhaust gases. These gases rapidly expand through a turbine, extracting mechanical energy to drive the compresso

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19

Zhao, Yuanyang, Qichao Yang, Liansheng Li, Jun Xiao, Yue Shu, and Qian Zhang. "Experimental research on stability enhancement for centrifugal compressors using active control casing treatment system." Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy 231, no. 5 (2017): 333–43. http://dx.doi.org/10.1177/0957650917708494.

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Centrifugal compressors are widely used in many fields, where they become unstable when operated at the edge of the surge line. This paper presents a method, which is based on the active control casing treatment to enhance the operating stability of the centrifugal compressor. To investigate the effect of the active control casing treatment system on the performance of a centrifugal compressor, a test rig with rotating speed of 15,000 r/min was built up. The experimental results show that the active control casing treatment system can significantly decrease the surge flow rate and extend the e

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20

Awasthi, Garima. "Flow Analysis of Centrifugal Compressor using ANSYS." International Journal for Research in Applied Science and Engineering Technology 12, no. 7 (2024): 1447–55. http://dx.doi.org/10.22214/ijraset.2024.63784.

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Abstract: The aerodynamic and structural designs of the impeller are vital to the functioning of the entire compressor stage in centrifugal compressors. In contrast to previous years, there has been a greater demand for industrial centrifugal compressors to operate with greater efficiency and operational range. Although the efficiency of low-pressure-ratio centrifugal compressors has nearly achieved its maximum, intermediate and high-pressure ratio machines still lag behind the state-of-the-art in terms of efficiency. Maintaining maximum efficiency while extending the working range is a challe

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21

Yang, Chuanlei, Zhaoling Liu, Yang Liu, et al. "Influence of Diffuser Vane Thickness on Centrifugal Compressor Performance." Journal of Physics: Conference Series 2437, no. 1 (2023): 012007. http://dx.doi.org/10.1088/1742-6596/2437/1/012007.

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Abstract The structure of diffuser vanes has a significant influence on the performance of centrifugal compressors. To research the influence of diffuser vane thickness on the overall performance and internal flow condition of the centrifugal compressor. This paper takes a centrifugal compressor as the research object. By changing the diffuser vane thickness, and using three-dimensional fluid simulation technology to carry out simulation research. The results show that the thinner diffuser vanes can greatly improve the efficiency, flow rate and outlet temperature of the centrifugal compressor.

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22

Came, P. M., and C. J. Robinson. "Centrifugal compressor design." Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science 213, no. 2 (1998): 139–55. http://dx.doi.org/10.1243/0954406991522239.

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Centrifugal compressors are used in a wide range of applications in which performance and mechanical integrity are invariably among the paramount design objectives. There is therefore continuing interest in the development of a sound understanding of the relevant physical phenomena and in the systematic application of the knowledge base that is the forerunner of the established design procedures. The paper reviews centrifugal compressor design methods that are commonly used in industry and reviews the underlying engineering science supporting the design practices. The design process, starting

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23

Aribi, Yacine, and Razika Zammoum Boushaki. "A Novel Approach for Active Surge Control in Multistage Centrifugal Compressor." WSEAS TRANSACTIONS ON POWER SYSTEMS 18 (January 26, 2023): 1–10. http://dx.doi.org/10.37394/232016.2023.18.1.

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Compressors are used in the hydrocarbon industry from upstream to downstream to boost the pressure required to transport gas into processing and transportation pipelines inside and toward processing facilities. Turbo-centrifugal compressors are subject to repetitive damages resulting from the manifestation phenomenon known as surge, observed as fluid flow reversal at low mass flows. Active surge control aims to increase the compressor operating region by allowing the compressor to operate at low mass flow in the naturally-unstable region of the compressor. Surge is avoided in the industry by f

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24

Sukhomlinov, Igor, and Mihail Golovin. "Expedited method of testing and refinement of refrigeration centrifugal compressors." E3S Web of Conferences 140 (2019): 06004. http://dx.doi.org/10.1051/e3sconf/201914006004.

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Currently existing regulatory documents assume that refrigeration compressors are tested as part of test rigs with heat-exchange equipment. Given the high energy intensity of centrifugal compressors, the drive power of which in cooling mode with a cold capacity of up to 8.0 MW can be 2.0 or more MW, the creation of test rigs for preliminary and acceptance tests at the manufacturer’s factory requires a large investment. An alternative to the considered refrigeration centrifugal compressors test method is a test on a test rig in which the agent is partially condensed. In this case, an evaporator

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25

Wang, Zhongjun, and Ke Zhang. "Aerodynamic design of two-stage centrifugal compressor for vehicle hydrogen fuel cell." Journal of Physics: Conference Series 2865, no. 1 (2024): 012033. http://dx.doi.org/10.1088/1742-6596/2865/1/012033.

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Abstract The on-board hydrogen fuel cell is a power generation device that converts the chemical energy of hydrogen and oxygen directly into electrical energy. The centrifugal compressor mainly provides oxygen for the cathode of the fuel cell system. With the rapid development of the hydrogen fuel cell industry, the key components of the air compressor field are also developing rapidly. In the technical route, most companies launched two-stage compression centrifugal air compressors in response to the increasing power of the product development trend. The newly developed hydrogen fuel cell sys

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26

Xu, C., and R. S. Amano. "Meridional Considerations of the Centrifugal Compressor Development." International Journal of Rotating Machinery 2012 (2012): 1–11. http://dx.doi.org/10.1155/2012/518381.

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Centrifugal compressor developments are interested in using optimization procedures that enable compressor high efficiency and wide operating ranges. Recently, high pressure ratio and efficiency of the centrifugal compressors require impeller design to pay attention to both the blade angle distribution and the meridional profile. The geometry of the blades and the meridional profile are very important contributions of compressor performance and structure reliability. This paper presents some recent studies of meridional impacts of the compressor. Studies indicated that the meridional profiles

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27

Hacıbaba Huseynov, Mehdi Jafarov, Hacıbaba Huseynov, Mehdi Jafarov. "PROSPECTS FOR THE USE OF GAS TURBINE CENTRIFUGAL COMPRESSOR UNITS AT OIL AND GAS FACILITIES." PAHTEI-Procedings of Azerbaijan High Technical Educational Institutions 41, no. 06 (2024): 27–34. http://dx.doi.org/10.36962/pahtei41062024-03.

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The article is devoted to the study of gas turbine compressor units and, on the basis of this, the determination of technological, parametric and specific criteria and features of the use of gas turbine centrifugal compressor units in gas transmission systems and underground gas reservoirs. For this purpose, the advantages and disadvantages of gas turbine compressor units are analyzed. Comparative information is provided on the use of centrifugal, piston and screw compressors, which are often used in the oil and gas industry. The influence of the supply limit and supply volume, production time

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28

Novecosky, T. "Axial Inlet Conversion to a Centrifugal Compressor With Magnetic Bearings." Journal of Engineering for Gas Turbines and Power 116, no. 1 (1994): 152–55. http://dx.doi.org/10.1115/1.2906784.

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NOVA’s Alberta Gas Transmission Division transports natural gas via pipeline throughout the province of Alberta, Canada, exporting it to eastern Canada, United States, and British Columbia. There is a continuing effort to operate the facilities and pipeline at the highest possible efficiency. One area being addressed to improve efficiency is compression of the gas. By improving compressor efficiency, fuel consumption and hence operating costs can be reduced. One method of improving compressor efficiency is by converting the compressor to an axial inlet configuration, a conversion that has been

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29

Biočanin, Stojko, and Milica Timotijević. "Analysis of centrifugal compressor testing capabilities." IMK-14 - Istrazivanje i razvoj 27, no. 4 (2021): 99–104. http://dx.doi.org/10.5937/imk2103099b.

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The work shows examining of the centrifugal compressor for which there are no technical conditions by which the compressor manufacturer defines the form and important characteristics of the measuring installation. In the absence of the necessary data, a table for testing of centrifugal compressors was designed, where the pipeline measures and other details are freely defined in accordance with the available possibilities.

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30

Pu, Hong Bin, Yun Ping Zheng, Yu Chun Wang, Bai Song Cai, and Qi Liu. "Research on Modeling of Compressor Characteristics for Sichuan-East Gas Transmission Pipeline Project." Advanced Materials Research 468-471 (February 2012): 2393–98. http://dx.doi.org/10.4028/www.scientific.net/amr.468-471.2393.

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Optimized operation of compressor stations is of great importance for energy saving of Sichuan-East transmission pipeline at high flow rate. However, it is difficult to build an accurate mathematical model to describe the performance curves of centrifugal compressor due to the wide range of rotary speed. The achievements of this thesis are shown as follows. Firstly, the mathematic models for performance curves of the Euramerican centrifugal compressors were established. The optimized regression coefficients were solved rapidly and accurately by Zhan Chong-xi method. Secondly, the compressor ra

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31

S, Shivani, Amar Murthy A, and Srinivas G. "Aerodynamic performance enhancement of centrifugal compressor using numerical techniques." F1000Research 13 (May 17, 2024): 480. http://dx.doi.org/10.12688/f1000research.145060.1.

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Background Centrifugal compressors are dynamic machines utilizing a rotating impeller, efficiently accelerate incoming gases, transforming kinetic energy into pressure energy for compression. They serve a wide range of industries, including air conditioning, refrigeration, gas turbines, industrial processes, and applications such as air compression, gas transportation, and petrochemicals, demonstrating their versatility. Designing a centrifugal compressor poses challenges related to achieving high aerodynamic efficiency, surge and choke control, material selection, rotor dynamics, cavitation,

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Sun, Jianting, Hucan Hou, Zhitao Zuo, Hongtao Tang, and Haisheng Chen. "Numerical study on wet compression in a supercritical air centrifugal compressor." Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy 234, no. 3 (2019): 384–97. http://dx.doi.org/10.1177/0957650919861490.

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Wet compression is widely used to reduce compression work and improve efficiency in gas turbines. However, wet compression has not been industrially applied in the compressed air energy storage system (only few studies on isothermal compressed air energy storage system exist), which has an urgent demand to reduce the compression work. The high-pressure section of the compressed air energy storage system usually contains supercritical air, and the influence of supercritical wet compression is not yet clear. Thus, in this study, supercritical wet compression was numerically investigated in a cen

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33

Arnulfi, G. L., P. Giannattasio, C. Giusto, A. F. Massardo, D. Micheli, and P. Pinamonti. "Multistage Centrifugal Compressor Surge Analysis: Part I—Experimental Investigation." Journal of Turbomachinery 121, no. 2 (1999): 305–11. http://dx.doi.org/10.1115/1.2841315.

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This paper reports an experimental investigation on centrifugal compressor surge. The compression system consists of a four-stage blower with vaned diffusers and a large plenum discharging into the atmosphere through a throttle valve. Measurements of unsteady pressure and flow rate in the plant, and of instantaneous velocity in the diffusers of the first and fourth compressor stage, are performed during deep surge, at several valve settings and three different rotation speeds. Additional tests have been carried out on a different system configuration, i.e., without plenum, in order to obtain t

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34

Wang, Yongsheng, Feng Lin, Chaoqun Nie, and Abraham Engeda. "Design and Performance Evaluation of a Very Low Flow Coefficient Centrifugal Compressor." International Journal of Rotating Machinery 2013 (2013): 1–12. http://dx.doi.org/10.1155/2013/293486.

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Very low flow coefficient centrifugal compressors are often applied as the last stages of multistage compressors. Due to the lower volume flow rate, the flow channels in the impeller and diffuser are so narrow that friction loss becomes the main factor, which leads to lower efficiency than that of other stages in the same compressors. In addition, most of design methods are generally based on medium flow coefficient centrifugal compressors. Taking on researches on the low flow coefficient centrifugal compressors is significant and necessary. One-dimensional (1D) code, consisting of design and

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35

Liu, H. I., X. P. Li, and Y. N. Rui. "Monitor On-Line and Fault Diagnosis to High Speed Centrifugal Hydrogen Compressors Based on the Theories of EMD and Correlation Dimension." Applied Mechanics and Materials 33 (October 2010): 523–27. http://dx.doi.org/10.4028/www.scientific.net/amm.33.523.

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High Speed Centrifugal Hydrogen Compressors are big and critical equipments which are widely used in chemical enterprises. It is very important to monitor their condition on-line and diagnose their failure. Based on the research of EMD (empirical mode decomposition) and correlation dimension and experimental simulation, the vibration signals of a High Speed Centrifugal Hydrogen Compressor’s main spindle are collected when working. Then the signals are decomposed by EMD, their correlation dimensions are calculated and taken as fault feature. Finally, using BP algorithm of a neural network in wh

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36

Hung, Kuo-Shu, Kung-Yun Ho, Wei-Chung Hsiao, and Yean-Der Kuan. "The Characteristic of High-Speed Centrifugal Refrigeration Compressor with Different Refrigerants via CFD Simulation." Processes 10, no. 5 (2022): 928. http://dx.doi.org/10.3390/pr10050928.

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This study used Computational Fluid Dynamics (CFD) to simulate and analyze the working fluid in magnetic centrifugal refrigerant compressors using R-134a to mixed refrigerant: R-513A and HFO (Hydrofluoroolefins) Hydrofluoroolefin refrigerant: R-1234yf, and the impact on integrated part-load performance, Integrated Part Load Value (IPLV) and internal flow field. This study used a single-stage 280 USRT maglev centrifugal refrigerant compressor as a simulation model. Three different refrigerants were used: R-134a, R-513A, and R-1234yf, as presented in the National Institute of Standards and Techn

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Hong, Shuli, Zetao Wang, and Junyu Zhang. "Flow characteristics and phase transition analysis of a supercritical carbon dioxide centrifugal compressor." Journal of Physics: Conference Series 2939, no. 1 (2025): 012018. https://doi.org/10.1088/1742-6596/2939/1/012018.

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Abstract Micro centrifugal compressors are a key component of the Brayton cycle system with supercritical carbon dioxide (S-CO2) as the working medium in which the system can achieve a higher efficiency cycle. A typical micro centrifugal compressor is investigated. Then, the numerical simulations are performed for two working media; the S-CO2 and air. The results of the 3D flow simulation show that the fluid in the S-CO2 compressor can be divided into three zones: the supercritical zone, the liquid region, and the gas-liquid mixing zone. Research shows that the mechanism of phase transition oc

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Dubinin, E. V., B. F. Idiyatullin, and N. G. Khasanov. "Optimization of centrifugal compressor stages." Omsk Scientific Bulletin. Series Aviation-Rocket and Power Engineering 7, no. 4 (2023): 33–39. http://dx.doi.org/10.25206/2588-0373-2023-7-4-33-39.

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The article describes а hydraulic efficiency increase in the centrifugal compressor stage using automatic optimization algorithms. The optimization criterion is the polytropic efficiency of the intermediate compressor stage. The sequence of stages of the optimization process in the Fine/Design3D software module of the Numeca software package is presented. The creating process a solid model of the compression stage is shown. The performance curves of the developed stage after optimization of the shape of the rotor and stator elements are also presented.

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Wang, Yu, and Zhen Luo. "CFD Modeling of Flow Performance inside Subsonic Centrifugal Compressor." Advanced Materials Research 291-294 (July 2011): 251–54. http://dx.doi.org/10.4028/www.scientific.net/amr.291-294.251.

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Centrifugal Compressors, which offer good flow stability, compact size and high stage pressure ratio, have been widely used in helicopter engines and sometime served as high pressure stage in small turbojet engines. In this paper, a method of developing a CFD model is presented for investigating the flow performance of a subsonic centrifugal compressor. The configuration used for the study is a subsonic centrifugal compressor which has a 60mm diameter impeller. A CFD modeling is carried out to obtain the performance and operational range of the compressor stage. The mesh independence studies w

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40

Dasari, Ravi Kiran. "CENTRIFUGAL COMPRESSORS CONTROL CRITICALITY." International Journal of Engineering Applied Sciences and Technology 7, no. 11 (2023): 40–45. http://dx.doi.org/10.33564/ijeast.2023.v07i11.007.

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This article focused mainly on the importance of anti-surge control of compressor and how to design the recirculation line for turndown of compressors that’s referred as surge. Also some recommendations will be made for better design and safety

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Koyyalamudi, V. V. N. K. Satish, and Quamber H. Nagpurwala. "Stall Margin Improvement in a Centrifugal Compressor through Inducer Casing Treatment." International Journal of Rotating Machinery 2016 (2016): 1–19. http://dx.doi.org/10.1155/2016/2371524.

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The increasing trend of high stage pressure ratio with increased aerodynamic loading has led to reduction in stable operating range of centrifugal compressors with stall and surge initiating at relatively higher mass flow rates. The casing treatment technique of stall control is found to be effective in axial compressors, but very limited research work is published on the application of this technique in centrifugal compressors. Present research was aimed to investigate the effect of casing treatment on the performance and stall margin of a high speed, 4 : 1 pressure ratio centrifugal compress

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42

Eremenko, V. V., A. E. Mikhailov, A. B. Mikhailova, M. O. Goryukhin, and D. G. Krasnoperov. "Comparative analysis of turbulence model influence in numerical simulation of an experimental radial compressor stage." VESTNIK of Samara University. Aerospace and Mechanical Engineering 22, no. 4 (2023): 99–111. http://dx.doi.org/10.18287/2541-7533-2023-22-4-99-111.

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The accuracy of a CFD model of a turbo-machine might depend on a number of factors: turbulence model, quality of the mesh model, boundary conditions, solver settings, consideration of secondary geometric factors, etc. The purpose of this work is to develop practical recommendations for CFD calculations of centrifugal compressors based on the validation of a model of NASA High Efficiency Centrifugal Compressor experimental radial compressor stage. Results of a grid independence test are presented, and the optimal grid size for the High Efficiency Centrifugal Compressor stage is identified as co

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Kozhukhov, Yuri, Aleksey Danilishin, Sergey Kartashov, et al. "Application of Super-Computer Technologies in the Research and Improvement of Steps and Elements of the Flow Path of the Turbocompressors." E3S Web of Conferences 220 (2020): 01078. http://dx.doi.org/10.1051/e3sconf/202022001078.

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This paper presents the results of the study of the spatial flow in the turbocompressors elements of computational fluid dynamics methods using the Ansys CFX software package on a multiprocessor computer system. Five objects of research are considered: 1) flow path of an intermediate stage of an average-flow centrifugal compressor; 2) flow path of the low-flow centrifugal compressor stage; 3) a natural gas centrifugal compressor stage; 4) vaned diffuser of the first stage of an industrial multistage centrifugal compressor; 5) adjustable inlet stator of the first stage of an industrial turbocom

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Rohit, Kumar. "Design and Analysis of a High Speed Centrifugal Compressor for Aircraft Engine Application." Design and Analysis of a High Speed Centrifugal Compressor for Aircraft Engine Application 9, no. 1 (2024): 5. https://doi.org/10.5281/zenodo.10565920.

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This paper presents the design and analysis of a high-speed centrifugal compressor for aircraft engine applications. The compressor was designed to operate at a pressure ratio of 6.5 and a design speed of 70,000 RPM. The design process involved the selection of suitable impeller and diffuser geometries, as well as the determination of the optimal blade angles and chord lengths. The aerodynamic performance of the compressor was analyzed using computational fluid dynamics (CFD) simulations, and the structural integrity was evaluated using finite element analysis (FEA) simulations. The results of

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Hamrick, Joseph T. "A Review of the History of the National Advisory Committee for Aeronautics Centrifugal Compressor Program and Arrival at Current Computational Design Procedures." Journal of Fluids Engineering 127, no. 1 (2005): 94–97. http://dx.doi.org/10.1115/1.1855326.

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Before and during World War II, the design and development of single stage high pressure ratio centrifugal compressors was essentially a cut-and-try exercise. To reach a high pressure without substantial experimentation required multiple stages of impellers and diffusers with pressure ratios in the 2:1 range. While such arrangements were satisfactory for commercial use where weight was not a major consideration, they were not suitable for jet engines. The centrifugal compressor for the Whittle engine, the first British jet engine, was developed by trial and error with numerous modifications of

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Dong, Jingya, Bin Song, Xiaoyun Yuan, Wanchun Jin, and Jin Wang. "Research on aerodynamic performance of centrifugal compressors for hydrogen-mixed natural gas." PLOS ONE 19, no. 10 (2024): e0312829. http://dx.doi.org/10.1371/journal.pone.0312829.

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Natural gas-doped hydrogen transportation has been widely used in industrial engineering. The change of the physical parameters of the conveying medium affects the working performance of the centrifugal compressor. This study aims to explore the aerodynamic performance of centrifugal compressors for hydrogen mixed natural gas, including the effects of hydrogen blending ratio (HBR) and inlet temperature on the pressure ratio and isentropic efficiency of compressors. The numerical simulation method is used and the results are compared with the experimental results to determine the reliability of

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Zhao, Huanxin, Lei Tan, Dangguo Yang, Bing Liu, Honggang Fan, and Hongshuai Li. "Optimization Design and Pressure Fluctuation Suppression Based on Orthogonal Method for a Centrifugal Compressor." Machines 11, no. 5 (2023): 559. http://dx.doi.org/10.3390/machines11050559.

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An air compressor is the core component of the air supply system of a hydrogen fuel cell, which demands high efficiency and reliable stability in a wide operation region. In this work, a centrifugal air compressor for a hydrogen fuel cell is first designed and then measured experimentally. Furthermore, a test rig for assessing the aerodynamic performance of the centrifugal air compressor is established, which includes a pipeline, gas flowmeter, flow regulating valve, pressure transmitter, centrifugal compressor, controller, DC power supply and computer. Then, the orthogonal method is employed

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Qi, Bin, Su Jun Dong, and Jun Wang. "Optimization of Loss Models for Centrifugal Compressor Performance Prediction Based on Numerical Analysis Results." Applied Mechanics and Materials 300-301 (February 2013): 225–31. http://dx.doi.org/10.4028/www.scientific.net/amm.300-301.225.

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An optimization of loss models for performance prediction of centrifugal compressors has been conducted in this paper. A centrifugal compressor with vaneless diffuser (VLD) and vaned diffuser (VD) is selected for the present study. The study begins with a numerical analysis, using commercial software ANSYS CFX. The numerical result is used to modify mean streamline analysis loss models. Matlab optimization toolbox is used for this purpose. Also, a matlab program is compiled to calculate the off-design performance of the centrifugal compressor. The results show that after optimizating the loss

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Wang, Yuan, and Shaolin Hu. "State monitoring and fault prediction of centrifugal compressors based on long short–term memory and principal component analysis (LSTM-PCA)." PeerJ Computer Science 10 (October 21, 2024): e2433. http://dx.doi.org/10.7717/peerj-cs.2433.

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Centrifugal compressors are widely used in the petroleum and natural gas industry for gas compression, reinjection, and transportation. Early fault identification and fault evolution prediction for centrifugal compressors can improve equipment safety and reduce maintenance and operating costs. This article proposes a dynamic process monitoring method for centrifugal compressors based on long short-term memory (LSTM) and principal component analysis (PCA). This method constructs a sliding window for monitoring at each sampling point, which contains 100 data from the past and current time points

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Chen, Jiaxi, Zhitao Zuo, Jixiang Chen, Jianting Sun, and Haisheng Chen. "A Numerical Study on Leakage Flow in the Shroud Cavity of a Centrifugal Impeller." Energies 18, no. 8 (2025): 2042. https://doi.org/10.3390/en18082042.

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A high-pressure centrifugal compressor with a shroud cavity is a key piece of energy equipment found in a compressed air energy storage (CAES) system. The leakage flow of the shroud cavity is an important factor affecting the efficiency of the system. Using systematic numerical studies, the influence of leakage flow on high-pressure centrifugal compressors under different leakage rates has been comprehensively elucidated. The study reveals that the leakage flow significantly increases the circumferential swirl angle of the flow at the impeller inlet, thereby exerting a significant influence on

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