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Статті в журналах з теми "Centrifugal Gas Compressors"
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 (May 17, 2017): 333–43. http://dx.doi.org/10.1177/0957650917708494.
Повний текст джерелаAl 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.
Повний текст джерелаLebedev, 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.
Повний текст джерелаKalinkevych, M., V. Ihnatenko, O. Bolotnikova, and O. Obukhov. "Design of high efficiency centrifugal compressors stages." Refrigeration Engineering and Technology 54, no. 5 (October 31, 2018): 4–9. http://dx.doi.org/10.15673/ret.v54i5.1239.
Повний текст джерелаPu, 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.
Повний текст джерелаRekstin, A., V. Semenovskiy, K. Soldatova, Y. Galerkin, and K. Sokolov. "The simulation of gas-dynamic characteristics of centrifugal compressors in turbo-expander units." E3S Web of Conferences 124 (2019): 01008. http://dx.doi.org/10.1051/e3sconf/201912401008.
Повний текст джерелаKalinkevych, Mykola, and Andriy Skoryk. "Design Method for Channel Diffusers of Centrifugal Compressors." International Journal of Rotating Machinery 2013 (2013): 1–7. http://dx.doi.org/10.1155/2013/589357.
Повний текст джерелаAfandy, Muhammad Arif, Ifani P. Ramadhani, and Totok R. Biyanto. "Gas Turbine Compressor Configuration Analysis for Production and Efficiency Optimization at PT Saka Indonesia Pangkah Ltd." IOP Conference Series: Earth and Environmental Science 927, no. 1 (December 1, 2021): 012031. http://dx.doi.org/10.1088/1755-1315/927/1/012031.
Повний текст джерелаBaba, Toshiaki, Koumei Fujioka, Hirotoshi Arihara, Yoshitaka Baba, and Takuya Iwata. "EXPERIMENTAL EVALUATION OF PERFORMANCE AND MECHANICAL RELIABILITY FOR HIGH PRESSURE CO2 INTEGRALLY GEARED COMPRESSOR." Journal of the Global Power and Propulsion Society 4 (August 20, 2020): 128–44. http://dx.doi.org/10.33737/jgpps/124724.
Повний текст джерелаKurz, Rainer. "Natural Gas." Mechanical Engineering 133, no. 04 (April 1, 2011): 52. http://dx.doi.org/10.1115/1.2011-apr-7.
Повний текст джерелаДисертації з теми "Centrifugal Gas Compressors"
Jonson, Lance Gordon. "Surge testing of natural gas pipeline centrifugal compressors." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1998. http://www.collectionscanada.ca/obj/s4/f2/dsk2/tape17/PQDD_0010/MQ31322.pdf.
Повний текст джерелаBudinis, Sara. "Control and operation of centrifugal gas compressors, with an emphasis on CO2 compression." Thesis, Imperial College London, 2015. http://hdl.handle.net/10044/1/55458.
Повний текст джерелаDe, Villiers Lodewyk Christoffel Barend. "Design of a centrifugal compressor for application in micro gas turbines." Thesis, Stellenbosch : Stellenbosch University, 2014. http://hdl.handle.net/10019.1/96052.
Повний текст джерелаENGLISH ABSTRACT: This thesis details the methodology for developing a centrifugal compressor for application in a Micro Gas Turbine (MGT). This research forms part of a larger project, namely project Ballast, initiated by the South African Air Force (SAAF) in conjunction with Armscor. The methodology encompasses the development of a mean-line code that makes use of 1-dimensional theory in order to create an initial centrifugal compressor geometry which includes a rotor as well as radial vaned diffuser. This is followed by a Computational Fluid Dynamics (CFD) simulation process during which the compressor is optimised in order to maximise its performance. Before manufacturing a Finite Element Analysis (FEA) is done in order to ensure that the rotor does not fail during testing. The testing of the compressor is done to compare the numerical results with the experimental results and in so doing confirms the design process. A previous student had designed a rotor by making use of a mean-line code as well as a CFD optimisation process. The rotor had a measured total-static pressure ratio of roughly 2.8 at 121 kRPM and a total-total isentropic efficiency of 79.1 % at said rotational speed. The inclusion of a vaned diffuser resulted in a higher total-static pressure ratio and accordingly the compressor designed in this report has a CFD determined total-static pressure ratio of 3.0. The efficiency would however drop and as such a total-total isentropic efficiency of 76.5 % was determined theoretically. The theoretical results correlated well with the experimental results and as such it was concluded that the design methodology developed was sound.
AFRIKAANSE OPSOMMING: Hierdie tesis bespreek die metodologie vir die ontwikkeling van ‘n sentrifugale kompressor vir toepassing in ‘n Mikro-Gasturbine (MGT). Die tesis vorm deel van ‘n groter projek, genaamd die Ballast projek, wat deur die Suid-Afrikaanse Lugmag (SALM) daargestel is in samewerking met Krygkor. Die metodologie behels die ontwikkeling van ‘n middel-lyn kode wat gebruik maak van 1-dimensionele teorie om die aanvanklike geometrie van die kompressor te skep. Die geometrie bevat beide die rotor asook die gelemde radiale diffusor. Hierdie proses word gevolg deur ‘n Berekeningsvloeidinamika (BVD) simulasie waartydens die kompressor geoptimeer word om sodoende die verrigting ten volle te verbeter. Voordat vervaardiging plaasvind word ‘n Eindige Element Analise (EEA) toegepas om te verseker dat die rotor nie sal faal tydens toetse nie. Die toetse word gedoen sodat die eksperimentele resultate met die numeriese resultate vergelyk kan word. Sodoende word die proses waardeur die kompressor ontwikkel word bevestig. ‘n Vorige student het ‘n rotor ontwerp deur gebruik te maak van ‘n middel-lyn kode asook ‘n BVD optimerings proses. Die rotor het ‘n gemete totaal-statiese drukverhouding van ongeveer 2.8 teen 121 kRPM gelewer en ‘n totaal-totale isentropiese benutingsgraad van 79.1 % teen dieselfde omwentelingspoed. Met die insluiting van ‘n gelemde radiale diffuser word ‘n hoër totaal-statiese druk verhouding verwag en as sulks lewer die nuut-ontwerpte kompressor soos in die tesis bespreek ‘n teoretiese totaal-statiese drukverhouding van 3.0. Die benutingsgraad sal egter daal en daarvolgens het die nuwe kompressor ‘n totaal-totale isentropiese benutingsgraad van 76.5 % gelewer. Die eksperimentele resultate het goed ooreengestem met die teoretiese resultate en as sulks was dit besluit dat die ontwerps-metodologie goed is.
Калінкевич, Микола Васильович, Николай Васильевич Калинкевич, Mykola Vasylovych Kalinkevych та Н. А. Андрущенко. "Многовальные центробежные компрессоры для сжатия природного газа низкого давления". Thesis, Сумский государственный университет, 2016. http://essuir.sumdu.edu.ua/handle/123456789/45652.
Повний текст джерелаОбухова, Анастасія Олександрівна, Анастасия Александровна Обухова та Anastasiia Oleksandrivna Obukhova. "Анализ эффективности элементов проточной части ступени центробежного компрессора при немодельных изменениях её геометрии". Thesis, Сумский государственный университет, 2016. http://essuir.sumdu.edu.ua/handle/123456789/45731.
Повний текст джерелаKrige, David Schabort. "Performance evaluation of a micro gas turbine centrifugal compressor diffuser." Thesis, Stellenbosch : Stellenbosch University, 2013. http://hdl.handle.net/10019.1/80119.
Повний текст джерелаENGLISH ABSTRACT: Micro gas turbines used in the aerospace industry require high performance with a compact frontal area. These micro gas turbines are often considered unattractive and at times impractical due to their poor fuel consumption and low cycle efficiency. This led to a joint effort to investigate and analyze the components of a particular micro gas turbine to determine potential geometry and performance improvements. The focus of this investigation is the radial vaned diffuser which forms part of a centrifugal compressor. The size of the diffuser is highly constrained by the compact gas turbine diameter. The micro gas turbine under consideration is the BMT 120 KS. The radial vaned diffuser is analyzed by means of 1-D and 3-D (CFD) analyses using CompAero and FINETM/Turbo respectively. The aim is to design a diffuser that maximizes the total-to-static pressure recovery and mass flow rate through the compressor with minimal flow losses. An experimental test facility was constructed and the numerical computations were validated against the experimental data. Three new diffusers were designed, each with a different vane geometry. The static-to-static pressure ratio over the radial diffuser was improved from 1.39 to 1.44 at a rotational speed of 120 krpm. The static pressure recovery coefficient was improved from 0.48 to 0.73 with a reduction in absolute Mach number from 0.47 to 0.22 at the radial diffuser discharge.
AFRIKAANSE OPSOMMING: Mikro-gasturbines wat in die lugvaart industrie gebruik word, vereis ‘n hoë werkverrigting met ‘n kompakte frontale area. Hierdie gasturbines word menigmaal onaantreklik geag weens swak brandstofverbruik en n lae siklus effektiewiteit. Dit het gelei tot ‘n gesamentlike projek om elke komponent van ‘n spesifieke mikro-gasturbine te analiseer en te verbeter. Die fokus van dié ondersoek is die radiale lem diffusor wat deel vorm van ‘n sentrifugaalkompressor. Die deursnee van die diffusor word deur die kompakte gasturbine diameter beperk. Die mikro gasturbine wat ondersoek word is die BMT 120 KS. Die radiale lem diffusor word geanaliseer deur middel van 1-D en 3-D (BVD) berekeninge met behulp van CompAero en FINETM/Turbo onderskeidelik. Die doelwit is om ‘n diffusor te ontwerp met ‘n verhoogde massavloei en drukverhouding oor die kompressor. ‘n Eksperimentele toetsfasiliteit is ingerig om toetse uit te voer en word gebruik om numeriese berekeninge te bevestig. Die staties-tot-stasiese drukstyging oor die radiale diffusor is verbeter van 1.39 tot 1.44 by ‘n omwentelingspoed van 120 kopm. Die statiese drukherwinningskoeffisiënt is verbeter van 0.48 tot 0.73 met ‘n vermindering in die absolute Machgetal vanaf 0.47 tot 0.22 by die radiale diffusor uitlaat.
Mele, Erik. "Wet Gas Compressor Performance : A Numerical Investigation of Thermal-Equilibrium in a Centrifugal Compressor Exposed to Wet Gas." Thesis, Norges teknisk-naturvitenskapelige universitet, Institutt for energi- og prosessteknikk, 2012. http://urn.kb.se/resolve?urn=urn:nbn:no:ntnu:diva-18533.
Повний текст джерелаVan, der Merwe Bosman Botha. "Design of a centrifugal compressor impeller for micro gas turbine application." Thesis, Stellenbosch : Stellenbosch University, 2012. http://hdl.handle.net/10019.1/71610.
Повний текст джерелаENGLISH ABSTRACT: The use of micro gas turbines (MGTs) for the propulsion of unmanned aerial vehicles (UAVs) has become an industry standard. MGTs offer better performance vs. weight than similar sized, internal combustion engines. The front component of an MGT serves the purpose of compressing air, which is subsequently mixed with a fuel and ignited to both power the turbine which drives the compressor, and to produce thrust. Centrifugal compressors are typically used because of the high pressure ratios they deliver per stage. The purpose of this project was to design a centrifugal compressor impeller, and to devise a methodology and the tools with which to perform the aforementioned. A compressor impeller adhering to specific performance and dimensional requirements was designed. The new compressor was designed using a mean-line performance calculation code. The use of the code was vindicated through comparison with the results from a benchmark study. This comparison included mean-line, Computational Fluid Dynamic (CFD), and experimental results: the new design mean-line results were compared to the results of CFD simulations performed on the same design. The new design was optimised using an Artificial Neural Network (ANN) and Genetic Algorithm. Prior to and during optimisation, the ANN was trained using a database of sample CFD calculations. A Finite Element Analysis (FEA) was done on the optimised impeller geometry to ensure that failure would not occur during operation. According to CFD results, the final design delivered good performance at the design speed with regards to pressure ratio, efficiency, and stall margin. The mechanical stresses experienced during operation were also within limits. Experimental results showed good agreement with CFD results of the optimised impeller. Keywords: micro gas turbine, centrifugal compressor, impeller, CFD, experimental, optimisation, FEA.
AFRIKAANSE OPSOMMING: Die gebruik van mikrogasturbines vir die aandrywing van onbemande vliegtuie het ‟n standaard geword in die industrie. Mikrogasturbines bied beter werkverrigting teen gewig as binnebrandenjins van soortgelyke grote. Hierdie eienskap verseker dat mikrogasturbines as aandryfmotors vir onbemande vliegtuie uiters voordelig is. Die voorste komponent van ‟n mikrogasturbine dien om lug saam te pers, wat dan met brandstof gemeng en daarna aan die brand gesteek word om krag aan die kompressor en stukrag te voorsien. Sentrifugaalkompressors word tipies gebruik as gevolg van die hoë drukverhoudings wat hierdie komponente per stadium kan lewer. Die doel van hierdie projek was om ‟n sentrifugaalkompressor te ontwerp, en ‟n metode en die hulpmiddels te ontwikkel om laasgenoemde uit te voer. ‟n Kompressor rotor wat voldoen het aan sekere werkverrigtings en dimensionele vereistes is ontwerp. Die nuwe kompressor rotor is met behulp van 1-dimensionele werkverrigting-berekeningskode ontwerp. Die berekeningsakkuraatheid van die kode en díé van ‟n kommersiële Berekenings Vloeidinamika pakket is bevestig deur die berekende resultate te vergelyk met die van eksperimente. Die nuwe rotor is gevolglik deur middel van ‟n Kunsmatige Neurale Netwerk en Genetiese Algoritme geoptimeer. Die Kunsmatige Neurale Netwerk is voor en gedurende optimering deur Berekenings Vloeidinamika simulasies opgelei. Die meganiese sterkte van die geoptimeerde rotor is nagegaan met behulp van ‟n Eindige Element Analise. Dit is gedoen om te verseker dat die rotor nie sal faal by die bedryfspunt nie. Berekenings Vloeidinamika resultate het getoon dat die finale rotor ontwerp ‟n goeie werkverrigting lewer by die ontwerpspoed, met betrekking tot drukverhouding, bennutingsgraad, en stakingsmarge. Eksperimentele resultate het goeie ooreenstemming met die Berekenings Vloeidinamika resultate van die geoptimeerde rotor getoon. Sleutelwoorde: mikrogasturbine, sentrifigaalkompressor, rotor, Berekenings Vloeidinamika, eksperimenteel, optimering, Eindige Element Analise.
Kurauchi, Sandro Kojiro. "Design and off-design analysis of a centrifugal compressor for natural gas." Instituto Tecnológico de Aeronáutica, 2012. http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2102.
Повний текст джерелаLuiten, Ruben Vincent. "Performance improvement of the Rover 1S/60 Gas Turbine Compressor." Thesis, Stellenbosch : Stellenbosch University, 2015. http://hdl.handle.net/10019.1/97049.
Повний текст джерелаENGLISH ABSTRACT: The use of gas turbines in central receiver solar power plant cycles has become an increasingly popular research topic. This has led to the need to investigate and analyse the effect of the solar receiver on the gas turbine cycle. The aim of this thesis is to construct an experimental gas turbine setup to accommodate further research on utilizing solar energy to power gas turbines. The gas turbine under consideration is the Rover Gas Turbines 1S/60. The focus of this investigation is the centrifugal compressor of the gas turbine. An increase in static pressure is required for the gas turbine to cope with anticipated pressure drops in the central receiver that will be part of the gas turbine cycle. The standard compressor design is analysed by means of 3-D (CFD) analysis using CFX® and experimental data. The new centrifugal compressor is designed by means of 1-D and 3-D (CFD) analysis using CompAero and CFX®. The aim is to design a compressor that maximizes the total-to-static pressure ratio. The size of the compressor is highly constrained by the geometry parameters of the gas turbine. Since the turbine rotor will remain unchanged, the power input, mass flow rate and rotational speed must stay the same. The experimental setup was build and the numerical results of the standard compressor were validated against the experimental results. A new centrifugal compressor was designed. The total-to-static pressure ratio was increased from 2.50 to 3.30 at an operating speed of 46 krpm. The efficiency of the compressor was improved from 63.8% to 85.6%. The input power of the new compressor design deviated 1.6% from the set benchmark, and 1.3% from the numerical data of the standard compressor.
AFRIKAANSE OPSOMMING: Die gebruik van gasturbines in sonkragstasiesiklusse met ’n sentrale ontvanger het gegroei tot ’n gewilde navorsingsonderwerp. Dit het gelei tot die behoefte om die effek van die sonontvanger op die gasturbinesiklus te ondersoek en te analiseer. Die doel van hierdie tesis is om ’n eksperimentele gasturbine opstelling te bou vir verdere navorsing oor die benutting van sonenergie om ’n gasturbine aan te dryf. Die gasturbine in oorweging is die Rover Gas Turbines 1S/60. Die fokus van hierdie ondersoek is die sentrifugale kompressor van die gasturbine. ’n Toename in statiese druk word benodig vir die gasturbine om die verwagte drukverlies in die sentrale ontvanger, wat deel uit maak van die gasturbinesiklus, te hanteer. Die standaard kompressor ontwerp is geanaliseer deur middel van 3-D Berekenings Vloeimeganika (BVM) analises met behulp van CFX® en eksperimentele data. Die nuwe sentrifugale kompressor is ontwerp deur middel van 1-D en 3-D BVM analises met behulp van CompAero en CFX®. Die doel is om ’n kompressor te ontwerp wat die totale-tot-statiese drukverhouding maksimeer. Die grootte van die kompressor is beperk deur die geometrie van die gasturbine omhulsel. Aangesien die turbinerotor onveranderd sal bly, moet die insetdrywing, massa-vloeitempo en rotasiespoed dieselfde bly. Die eksperimentele opstelling is gebou en die numeriese resultate van die standaard kompressor is teenoor die eksperimentele resultate gevalideer. ’n Nuwe sentrifugale kompressor is ontwerp. Die totale-tot-statiese drukverhouding is verhoog van 2.50 tot 3.30 teen ’n rotasiespoed van 46 000 omwentelings per minuut. Die doeltreffendheid van die kompressor is verbeter van 63.8% tot 85.6%. Die insetdrywing van die nuwe kompressor ontwerp het met 1.6% afgewyk van die vasgestelde maatstaf, en met 1.3% van die numeriese data van die standaard kompressor.
Книги з теми "Centrifugal Gas Compressors"
Sapiro, Leon. Aerodynamic performance of centrifugal compressors for gas and oil applications. New York: ASME, 2007.
Знайти повний текст джерелаParker, Philip M. The 2007-2012 World Outlook for New Stationary Centrifugal and Axial Gas Compressors Excluding Natural Gas Compressors. ICON Group International, Inc., 2006.
Знайти повний текст джерелаThe 2006-2011 World Outlook for New Stationary Centrifugal and Axial Gas Compressors Excluding Natural Gas Compressors. Icon Group International, Inc., 2005.
Знайти повний текст джерелаStandard 617 Centrifugal Compressors for Petroleum:: Chemical & Gas Service Industry. 6th ed. Amer Petroleum Inst, 1995.
Знайти повний текст джерелаA, Clark David, Wood Jerry R, United States. Army Aviation Research and Technology Activity. Propulsion Directorate., and Lewis Research Center, eds. Effect of area ratio on the performance of a 5.5:1 pressure ratio centrifugal impeller. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.
Знайти повний текст джерелаThe 2006-2011 World Outlook for New Stationary Centrifugal and Axial Natural Gas Compressors. Icon Group International, Inc., 2005.
Знайти повний текст джерелаParker, Philip M. The 2007-2012 World Outlook for New Stationary Centrifugal and Axial Natural Gas Compressors. ICON Group International, Inc., 2006.
Знайти повний текст джерелаCzechowski, Edward S. Critical factors in the application of a diesel engine drive on a centrifugal gas compressor: A Master's project in Industrial Technology. 1996.
Знайти повний текст джерелаKollmann, Karl, Calum E. Douglas, and S. Can Gülen. Turbo/Supercharger Compressors and Turbines for Aircraft Propulsion in WWII: Theory, History and Practice—Guidance from the Past for Modern Engineers and Students. ASME, 2021. http://dx.doi.org/10.1115/1.884676.
Повний текст джерелаL, Mattern Duane, Le Dzu K, and United States. National Aeronautics and Space Administration., eds. Comparisons of rig and engine dynamic events in the compressor of an axi-centrifugal turboshaft engine. [Washington, D.C: National Aeronautics and Space Administration, 1996.
Знайти повний текст джерелаЧастини книг з теми "Centrifugal Gas Compressors"
Johansen, Oddgeir. "Performance Monitoring System for Centrifugal Compressors On Heimdal Gas Field." In Profitable Condition Monitoring, 55–67. Dordrecht: Springer Netherlands, 1993. http://dx.doi.org/10.1007/978-94-011-1616-9_7.
Повний текст джерелаRozova, Lyudmyla, and Gennadii Martynenko. "Mathematical Modeling and Program Implementation of Gasdynamic Solution of Dry Gas Seals for Centrifugal Compressors." In Advances in Intelligent Systems and Computing, 591–602. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-63270-0_40.
Повний текст джерелаUnnikrishnan, G. "Bayesian Network for Centrifugal Compressor Damage." In Oil and Gas Processing Equipment, 103–12. First edition. | Boca Raton : CRC Press, 2021.: CRC Press, 2020. http://dx.doi.org/10.1201/9780429287800-7.
Повний текст джерелаBonneton, M., L. Tavian, G. M. Gistau-Baguer, F. Turcat, and P. Viennot. "A High Reliability Gas-Driven Helium Cryogenic Centrifugal Compressor." In Advances in Cryogenic Engineering, 643–49. Boston, MA: Springer US, 1998. http://dx.doi.org/10.1007/978-1-4757-9047-4_78.
Повний текст джерелаHafaifa, Ahmed, Guemana Mouloud, and Belhadef Rachid. "Fuzzy Modeling and Control of Centrifugal Compressor Used in Gas Pipelines Systems." In Applied Condition Monitoring, 379–89. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-14532-7_39.
Повний текст джерелаCherepanov, Ivan E., Vladimir Ya Modorskii, Stanislav L. Kalyulin, Anton O. Mikryukov, Danila S. Maksimov, and Anna V. Babushkina. "Applying Parallel Calculations to Model the Centrifugal Compressor Stage of a Gas Transmittal Unit in 2FSI Statement." In Communications in Computer and Information Science, 321–35. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-55326-5_23.
Повний текст джерелаNail, Bachir, Nadji Hadroug, Ahmed Hafaifa, and Abdellah Kouzou. "Fault Detection and Localization of Centrifugal Gas Compressor System Using Fuzzy Logic and Hybrid Kernel-SVM Methods." In Studies in Systems, Decision and Control, 137–53. Singapore: Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-1746-4_7.
Повний текст джерелаBoyce, Meherwan P. "Centrifugal Compressors." In Gas Turbine Engineering Handbook, 219–73. Elsevier, 2006. http://dx.doi.org/10.1016/b978-075067846-9/50009-2.
Повний текст джерелаBoyce, Meherwan P. "Centrifugal Compressors." In Gas Turbine Engineering Handbook, 253–301. Elsevier, 2012. http://dx.doi.org/10.1016/b978-0-12-383842-1.00006-8.
Повний текст джерелаWilkes, Jason, Brian Pettinato, Rainer Kurz, Justin Hollingsworth, Donghui Zhang, Matt Taher, Chris Kulhanek, Ferdinand Werdecker, Dirk Büche, and George Talabisco. "Centrifugal Compressors." In Compression Machinery for Oil and Gas, 31–133. Elsevier, 2019. http://dx.doi.org/10.1016/b978-0-12-814683-5.00003-1.
Повний текст джерелаТези доповідей конференцій з теми "Centrifugal Gas Compressors"
Noushad, Jisha, Anand Babu Dhamarla, and Pavan Kumar. "Casing Treatment of Centrifugal Compressors." In ASME 2015 Gas Turbine India Conference. American Society of Mechanical Engineers, 2015. http://dx.doi.org/10.1115/gtindia2015-1337.
Повний текст джерелаHoppock, William G. "Revamp Experiences With Centrifugal Pipeline Compressors." In ASME 1989 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1989. http://dx.doi.org/10.1115/89-gt-109.
Повний текст джерелаPereira dos Santos, Sidney. "Gas Compressor Service With Turbo Compressors." In 2004 International Pipeline Conference. ASMEDC, 2004. http://dx.doi.org/10.1115/ipc2004-0183.
Повний текст джерелаBerot, François, and Hervé Dourlens. "On Instability of Overhung Centrifugal Compressors." In ASME 1999 International Gas Turbine and Aeroengine Congress and Exhibition. American Society of Mechanical Engineers, 1999. http://dx.doi.org/10.1115/99-gt-202.
Повний текст джерелаGalerkin, Y., A. Rekstin, K. Soldatova, and A. Drozdov. "Gas Dynamic Designs of Centrifugal Compressors for Gas Industry." In ASME 2015 Gas Turbine India Conference. American Society of Mechanical Engineers, 2015. http://dx.doi.org/10.1115/gtindia2015-1215.
Повний текст джерелаTaher, Matt, and Cyrus Meher-Homji. "Matching of Gas Turbines and Centrifugal Compressors: Oil and Gas Industry Practice." In ASME Turbo Expo 2012: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/gt2012-68283.
Повний текст джерелаHughes, G. A. "Applications for Hydrocarbon Testing in Centrifugal Compressors." In ASME 1987 International Gas Turbine Conference and Exhibition. American Society of Mechanical Engineers, 1987. http://dx.doi.org/10.1115/87-gt-134.
Повний текст джерелаMizuki, Shimpei, and Hikaru Imai. "A Study Concerning Performance Characteristics of Centrifugal Compressors." In ASME 1985 International Gas Turbine Conference and Exhibit. American Society of Mechanical Engineers, 1985. http://dx.doi.org/10.1115/85-gt-97.
Повний текст джерелаAshour, Osama, Arul Saravanapriyan, Abdurrahman Khalidi, Ever Fadlun, Nicola Giannini, Alberto Ceccherini, Marco Pierir, and David Bianucci. "Diagnostic Rules for Gas Turbines Driving Centrifugal Compressors." In Abu Dhabi International Petroleum Exhibition and Conference. Society of Petroleum Engineers, 2015. http://dx.doi.org/10.2118/177743-ms.
Повний текст джерелаStaroselsky, Naum, and Lawrence Ladin. "More Effective Control for Centrifugal Gas Compressors Operating in Parallel." In ASME 1986 International Gas Turbine Conference and Exhibit. American Society of Mechanical Engineers, 1986. http://dx.doi.org/10.1115/86-gt-204.
Повний текст джерелаЗвіти організацій з теми "Centrifugal Gas Compressors"
Skone, Timothy J. Wellhead Compressor, Gas-Powered Centrifugal, 200 HP. Office of Scientific and Technical Information (OSTI), April 2011. http://dx.doi.org/10.2172/1509237.
Повний текст джерелаDi Bella, Francis A. Development Of A Centrifugal Hydrogen Pipeline Gas Compressor. Office of Scientific and Technical Information (OSTI), April 2015. http://dx.doi.org/10.2172/1227195.
Повний текст джерелаDevelopment of turbine driven centrifugal compressors for non-condensible gas removal at geothermal power plants. Final report. Office of Scientific and Technical Information (OSTI), December 1997. http://dx.doi.org/10.2172/570103.
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