Relevant bibliographies by topics / Centrifugal Compressor

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Centrifugal Compressor'

Author: Grafiati
Published: 4 June 2021
Last updated: 26 July 2025

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Journal articles on the topic "Centrifugal Compressor"

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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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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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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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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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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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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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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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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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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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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Dissertations / Theses on the topic "Centrifugal Compressor"

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Hazby, Hamid Richard. "Centrifugal compressor aerodynamics." Thesis, University of Cambridge, 2011. https://www.repository.cam.ac.uk/handle/1810/252228.

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Moenne-Loccoz, Victor. "Analyse expérimentale des instabilités aérodynamiques dans un compresseur centrifuge de nouvelle génération." Thesis, Lyon, 2019. http://www.theses.fr/2019LYSEC005.

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L’étude effectuée au cours de cette thèse a permis la caractérisation expérimentale des instabilités aérodynamiques se développant dans un compresseur centrifuge et une première évaluation de l’efficacité d’une stratégie de contrôle par aspiration de couche limite. Le compresseur, développé par Safran Helicopter Engines et dénommé Turbocel, est composé d’une roue directrice d’entrée, d’un rouet centrifuge splitté, d’un diffuseur radial aubé et splitté et d’un redresseur axial. Des travaux numériques antérieurs réalisés au Laboratoire de Mécanique des Fluides et d’Acoustique ont montré, aux bas
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Harris, P. K. "Erosion in centrifugal compressor impellers." Thesis, Cranfield University, 1996. http://dspace.lib.cranfield.ac.uk/handle/1826/10622.

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An experimental and theoretical study of erosion in centrifugal compressor impellers is presented. An experimental rig using laser anemometry techniques was employed to create a database of particle restitution ratios for a range of materials. This data was unique in that the particle rebound was measured in a quiescent condition where the aerodynamic effects had been minimised, and also parametric factors not previously available were included. These values were incorporated into the existing Particle Trajectory Code developed by Cranfield University and Rolls Royce PLC. The code is used to c
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Pinsley, Judith Ellen. "Active control of centrifugal-compressor surge." Thesis, Massachusetts Institute of Technology, 1988. http://hdl.handle.net/1721.1/39016.

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Guidotti, Emanuele <1977&gt. "Towards Centrifugal Compressor Stages Virtual Testing." Doctoral thesis, Alma Mater Studiorum - Università di Bologna, 2014. http://amsdottorato.unibo.it/6550/1/Guidotti_Emanuele_tesi.pdf.

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Flow features inside centrifugal compressor stages are very complicated to simulate with numerical tools due to the highly complex geometry and varying gas conditions all across the machine. For this reason, a big effort is currently being made to increase the fidelity of the numerical models during the design and validation phases. Computational Fluid Dynamics (CFD) plays an increasing role in the assessment of the performance prediction of centrifugal compressor stages. Historically, CFD was considered reliable for performance prediction on a qualitatively level, whereas tests were necessary
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Guidotti, Emanuele <1977&gt. "Towards Centrifugal Compressor Stages Virtual Testing." Doctoral thesis, Alma Mater Studiorum - Università di Bologna, 2014. http://amsdottorato.unibo.it/6550/.

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Flow features inside centrifugal compressor stages are very complicated to simulate with numerical tools due to the highly complex geometry and varying gas conditions all across the machine. For this reason, a big effort is currently being made to increase the fidelity of the numerical models during the design and validation phases. Computational Fluid Dynamics (CFD) plays an increasing role in the assessment of the performance prediction of centrifugal compressor stages. Historically, CFD was considered reliable for performance prediction on a qualitatively level, whereas tests were necessary
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Lancel, Jerome. "Analysis and test of a centrifugal compressor." Thesis, University of Sussex, 2002. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.250183.

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Leung, Kam Man. "Investigation of surge improvement of centrifugal compressor." Thesis, University of Sussex, 2003. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.400033.

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Benneke, Björn. "A methodology for centrifugal compressor stability prediction." Thesis, Massachusetts Institute of Technology, 2009. http://hdl.handle.net/1721.1/54609.

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Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2009.<br>Cataloged from PDF version of thesis.<br>Includes bibliographical references (p. 133-135).<br>The stable operation of centrifugal compressors is limited by well-known phenomena, rotating stall and surge. Although the manifestation of the full scale instabilities is similar to the ones observed in axial machines, the stall inception in centrifugal compressors is less well understood. This thesis focuses on developing an integrated methodology to predict the stability limit and the stall incepti
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Al-Mawali, Salim. "Centrifugal compressor surge suppression using fuzzy logic control." Thesis, University of Newcastle Upon Tyne, 2008. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.493201.

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Turbo gas compressors are among the most used machines ever invented. In the process industry, they are used intensively to provide compressed air for all types of pneumatic instruments and tools. These compressors suffer from an instability known as surge which usually occurs at low flow rates. The flow becomes seriously unstable and sometimes reverses. Surge has been a major problem for designers and users since the invention of the turbo-compressor. Although many successful echniques have been proposed to tackle the surge problem, most of them seem to offer to control at a single operating
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Books on the topic "Centrifugal Compressor"

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Japikse, David. Centrifugal compressor design and performance. Concepts ETI, 1996.

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Gresh, M. Theodore. Compressor performance: Selection,operation, and testing of axial and centrifugal compressors. Butterworth-Heinemann, 1991.

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Center, Lewis Research, ed. Final report for scaled centrifugal compressor program. Garrett Turbine Engine Company, 1986.

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Center, Lewis Research, ed. Final report for scaled centrifugal compressor program. Garrett Turbine Engine Company, 1986.

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McKain, Ted F. Coordinates for a high performance 4:1 pressure ratio centrifugal compressor. National Aeronautics and Space Administration, 1997.

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J, Holbrook Greg, and United States. National Aeronautics and Space Administration., eds. Coordinates for a high performance 4:1 pressure ratio centrifugal compressor. National Aeronautics and Space Administration, 1997.

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Reunanen, Arttu. Experimental and numerical analysis of different volutes in a centrifugal compressor. Lappeenrannan teknillinen korkeakoulu, 2001.

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J, Skoch Gary, United States. Army Aviation Systems Command., and United States. National Aeronautics and Space Administration., eds. A 4-spot time-of-flight anemometer for small centrifugal compressor velocity measurements. National Aeronautics and Space Administration, 1992.

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J, Skoch Gary, United States. Army Aviation Systems Command., and United States. National Aeronautics and Space Administration., eds. A 4-spot time-of-flight anemometer for small centrifugal compressor velocity measurements. National Aeronautics and Space Administration, 1992.

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J, Skoch Gary, United States. Army Aviation Systems Command., and United States. National Aeronautics and Space Administration., eds. A 4-spot time-of-flight anemometer for small centrifugal compressor velocity measurements. National Aeronautics and Space Administration, 1992.

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Book chapters on the topic "Centrifugal Compressor"

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Bose, Tarit. "Centrifugal Compressor." In Airbreathing Propulsion. Springer New York, 2012. http://dx.doi.org/10.1007/978-1-4614-3532-7_8.

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Lüdtke, Klaus H. "Compressor Design Constraints." In Process Centrifugal Compressors. Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-662-09449-5_4.

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Lüdtke, Klaus H. "Basic Compressor Aero-Thermodynamics." In Process Centrifugal Compressors. Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-662-09449-5_1.

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Lüdtke, Klaus H. "Standardization of Compressor Components." In Process Centrifugal Compressors. Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-662-09449-5_10.

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Lüdtke, Klaus H. "Compressor Off-Design Operation." In Process Centrifugal Compressors. Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-662-09449-5_5.

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Lüdtke, Klaus H. "Aerodynamic Compressor Design: Case Study." In Process Centrifugal Compressors. Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-662-09449-5_6.

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Giampaolo, Tony. "Surge Control Centrifugal/Axial Compressors." In Compressor Handbook: Principles and Practice, 2nd ed. River Publishers, 2023. http://dx.doi.org/10.1201/9781003449874-7.

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Giampaolo, Tony. "Centrifugal/Axial Compressors Description of Surge." In Compressor Handbook: Principles and Practice, 2nd ed. River Publishers, 2023. http://dx.doi.org/10.1201/9781003449874-6.

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Yoon, Se Young, Zongli Lin, and Paul E. Allaire. "Design of AMB Supported Centrifugal Compressor." In Advances in Industrial Control. Springer London, 2013. http://dx.doi.org/10.1007/978-1-4471-4240-9_4.

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Unnikrishnan, G. "Bayesian Network for Centrifugal Compressor Damage." In Oil and Gas Processing Equipment. CRC Press, 2020. http://dx.doi.org/10.1201/9780429287800-7.

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Conference papers on the topic "Centrifugal Compressor"

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Xu, C. "Centrifugal Compressor Design Considerations." In ASME 2006 2nd Joint U.S.-European Fluids Engineering Summer Meeting Collocated With the 14th International Conference on Nuclear Engineering. ASMEDC, 2006. http://dx.doi.org/10.1115/fedsm2006-98061.

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Initial design considerations of centrifugal compressor are commonly performed with experience base, although computer technology and numerical methods had made significantly progress. Three-dimensional Computational Fluid Dynamics (CFD) codes are still not major design tools for centrifugal compressors. Major design systems for industrial centrifugal compressor design are largely based on one-dimensional meanline and two-dimensional through flow tools. The experience of designers is one of the key factors to drive design success. The impeller is one of the key components of a centrifugal comp
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Jaiswal, Sujeet Kumar, Sadashiv Bubanale, and M. C. Keerthi. "Inlet Distortion Studies on a Centrifugal Compressor." In ASME 2023 Gas Turbine India Conference. American Society of Mechanical Engineers, 2023. http://dx.doi.org/10.1115/gtindia2023-118322.

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Abstract Centrifugal compressors can be subjected to non-uniformity in inlet flows due to complicated inlet pipe geometries arising from space constraints and the wakes of protruding instrumentation, impacting the compressor’s performance. Inlet distortion can cause premature stall initiation and surge, effectively reducing the operating range of the device. This motivates a detailed characterization of the performance for different types of inlet distortion. While the impact of distortion in axial compressors is studied extensively, there are relatively fewer studies for centrifugal compresso
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Brun, Klaus, and Rainer Kurz. "Analysis of the Effects of Pulsations on the Operational Stability of Centrifugal Compressors in Mixed Reciprocating and Centrifugal Compressor Stations." In ASME Turbo Expo 2008: Power for Land, Sea, and Air. ASMEDC, 2008. http://dx.doi.org/10.1115/gt2008-50540.

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Mixed operation with both centrifugal and reciprocating compressors in a compression plant poses significant operational challenges as pressure pulsations and machine mismatches lead to centrifugal compressors’ instabilities or poor performance. Arrangements with reciprocating compressors placed in series with centrifugal compressors generally lead to higher suction/discharge pulsations on the centrifugal compressor than conventional parallel operation. This paper demonstrates that by properly analyzing and designing the interconnecting piping between the compressors, utilizing pulsation atten
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Ameli, Alireza, Teemu Turunen-Saaresti, and Jari Backman. "Numerical Investigation of the Flow Behavior Inside a Supercritical CO2 Centrifugal Compressor." In ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2016. http://dx.doi.org/10.1115/gt2016-57481.

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Centrifugal compressors are one of the best choices among compressors in supercritical Brayton cycles. A supercritical CO2 centrifugal compressor increases the pressure of the fluid which state is initially very close to the critical point. When the supercritical fluid is compressed near the critical point, wide variations of fluid properties occur. The density of carbon dioxide at its critical point is close to the liquid density which leads to reduction in compressor work. The investigated compressor is a centrifugal compressor tested in the Sandia supercritical CO2 compression loop. In orde
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Xu, C., and R. S. Amano. "The Development of Centrifugal Compressor Impeller." In ASME Turbo Expo 2008: Power for Land, Sea, and Air. ASMEDC, 2008. http://dx.doi.org/10.1115/gt2008-50200.

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Impeller is one of the key components of industrial centrifugal compressors and turbochargers. Aerodynamic and structure designs of the impeller are critical to the success of the whole compressor stages. The requirements for efficiency and operating range of industrial centrifugal compressors and turbochargers have been increased dramatically compared with the situation in the past. The efficiency of newly developed low-pressure ratio centrifugal compressor has reached the possible level of the machine. However, the efficiency level of intermediate and high-pressure ratio machine still have g
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Kurz, Rainer, Robert McKee, and Klaus Brun. "Pulsations in Centrifugal Compressor Installations." In ASME Turbo Expo 2006: Power for Land, Sea, and Air. ASMEDC, 2006. http://dx.doi.org/10.1115/gt2006-90070.

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Compressor stations where both centrifugal and reciprocating compressors operate can exhibit operational problems due to low frequency pulsations. Avoiding these problems requires an understanding of the mechanisms that generate the pulsations, the transmission and attenuation of the pulsation, as well as their effect on the operation of the centrifugal compressor and the accuracy and reliability of flow measurements. The pulsation frequencies in question are typically lower than vortex shedding frequencies and blade passing frequencies. This paper will provide insight into the mechanisms and
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Rodgers, C. "The Centrifugal Compressor Inducer." In ASME 1998 International Gas Turbine and Aeroengine Congress and Exhibition. American Society of Mechanical Engineers, 1998. http://dx.doi.org/10.1115/98-gt-032.

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The function of the centrifugal compressor inducer is to provide wide flow margins from the design flow to the stall and choke flow limits, together with high static pressure recovery. At transonic conditions the inducer becomes the critical to impeller performance in that shock losses and blockage growth diminish stable flow range and may trigger near vertical stage characteristics. The paper covers the various types of inlet configurations upstream of the inducer, followed by a review of the state-of-art inducer design for centrifugal compressors, culminating with some research developments
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Muthanandan, Sundralingam. "Centrifugal Pump and Centrifugal Compressor Process Containment." In SPE/IATMI Asia Pacific Oil & Gas Conference and Exhibition. Society of Petroleum Engineers, 2017. http://dx.doi.org/10.2118/186410-ms.

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Methel, Jeanne, William J. Gooding, John C. Fabian, Nicole L. Key, and Mark Whitlock. "The Development of a Low Specific Speed Centrifugal Compressor Research Facility." In ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2016. http://dx.doi.org/10.1115/gt2016-56683.

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To achieve aggressive specific fuel consumption goals, aircraft engines are tending toward higher overall pressure ratios and higher bypass ratios for turbofans. As sizes decrease to meet these requirements, centrifugal compressors become a viable option as the last stage of the high pressure compressor. The last stages of an axial compressor in a small core engine face reduced efficiency due to the relatively large tip clearances with respect to blade height, and therefore, it may be more appropriate to finish the final compression stage with a low specific speed centrifugal compressor. A new
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Burandt, Bodo, and Matthias H. Buschmann. "New Centrifugal Compressor for Water Steam." In ASME Turbo Expo 2006: Power for Land, Sea, and Air. ASMEDC, 2006. http://dx.doi.org/10.1115/gt2006-90493.

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Environmental protection has been gaining more and more importance. Following this trend, the Institut fu¨r Luft- und Ka¨ltetechnik Dresden gGmbH (ILK) has designed a new chiller using water as natural refrigerant. Because of the special thermodynamic properties of water steam, the heart of the chiller, the centrifugal compressor, must be designed differently than the usual compressors used for refrigerating machines. This paper describes the compressor, its characteristic field and the test facilities used to investigate and optimize the compressor.
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Reports on the topic "Centrifugal Compressor"

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Katcher, Kelsi, Abhay Patil, Reese Roddy, and Subhra Shankha Koley. PR015-23206-R01 Centrifugal Compressor Station Efficiency Optimization. Pipeline Research Council International, Inc. (PRCI), 2024. http://dx.doi.org/10.55274/r0000102.

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The Compressor and Pump Station Technical Committee of Pipeline Research Council International (PRCI) has identified a need to reduce fuel and energy consumption at centrifugal compressor stations by improving the operating efficiency of centrifugal compressors at off-design conditions. It is commonplace for centrifugal compressors to operate well away from their original design point (and best efficiency point); this is generally due to (1) compressor stations needing to operate over an increasingly wide range of conditions and (2) economics favoring the installation of 1 or 2 large compresso
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Gottschlich, Joseph M., Robert P. Scaringe, and Fulin Gui. Lubrication Free Centrifugal Compressor. Defense Technical Information Center, 1994. http://dx.doi.org/10.21236/ada351103.

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Skone, Timothy J. Compressor, Single-Stage Centrifugal, Operation. Office of Scientific and Technical Information (OSTI), 2012. http://dx.doi.org/10.2172/1509358.

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Skone, Timothy J. Wellhead Compressor, Electrically-Powered Centrifugal, 500 HP. Office of Scientific and Technical Information (OSTI), 2011. http://dx.doi.org/10.2172/1509236.

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Skone, Timothy J. Wellhead Compressor, Gas-Powered Centrifugal, 200 HP. Office of Scientific and Technical Information (OSTI), 2011. http://dx.doi.org/10.2172/1509237.

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Lagus, P. L., and B. S. Flanagan. PR-197-723-R01 Compressor Flow Measurements. Pipeline Research Council International, Inc. (PRCI), 1988. http://dx.doi.org/10.55274/r0011964.

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The objective of the proposed research was to demonstrate the viability and utility of a constant flow tracer dilution technique for inferring the flowrate through a high-pressure natural gas centrifugal compressor. Testing was performed by injecting a known flowrate of tracer gas, sulfur hexafluoride(SF6), into a natural gas stream immediately upstream of an operating centrifugal compressor. Measurements of the diluted tracer gas concentration downstream of the compressor were made by means of electron capture gas chromatography. Knowledge of the injection concentration and injection flowrate
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7

Di Bella, Francis A. Development Of A Centrifugal Hydrogen Pipeline Gas Compressor. Office of Scientific and Technical Information (OSTI), 2015. http://dx.doi.org/10.2172/1227195.

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8

Lee. L51588 Improved Internal Seals for Pipeline Centrifugal Compressors. Pipeline Research Council International, Inc. (PRCI), 1988. http://dx.doi.org/10.55274/r0010524.

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Reviews current technology of internal labyrinth seals and concludes that internal leakage can reduce compressor efficiencies as much as 3 to 6 percent. Discusses limitations on abradable seals with tighter clearances and the effect of compressor surge on both types of seals. Proposes resiliently mounted seals as subject for future investigation to accommodate rotor movement without excessive seal wear.
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9

Ruckes, John. High Technology Centrifugal Compressor for Commercial Air Conditioning Systems. Office of Scientific and Technical Information (OSTI), 2006. http://dx.doi.org/10.2172/902086.

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10

Sabatino, Francesco Di. PR015-242001-R01 Gas Turbine Driven Centrifugal Compressor Roadmap. Pipeline Research Council International, Inc. (PRCI), 2025. https://doi.org/10.55274/r0000106.

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This report outlines the proposed roadmap projects across a variety of research topics from emissions to reliability to system monitoring of gas turbine-driven gas compressions stations. The background and the scope of work of each proposed project are presented.
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