Relevant bibliographies by topics / Turbine compressor

Contents

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

Academic literature on the topic 'Turbine compressor'

Author: Grafiati
Published: 3 June 2025
Last updated: 31 July 2025

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Journal articles on the topic "Turbine compressor"

1

Batayev, Nurlan. "Axial compressor fouling detection for gas turbine driven gas compression unit." Indonesian Journal of Electrical Engineering and Computer Science 15, no. 3 (2019): 1257. http://dx.doi.org/10.11591/ijeecs.v15.i3.pp1257-1263.

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<span>One of the main reasons of the performance degradation of gas turbines is the axial compressor fouling due to air pollutants. Considering the fact that the fouling leads to high consumption of fuel, reducing of the axial compressor’s discharge air pressure and increasing of the exhaust temperature, thus designing a compressor degradation detection system will allow prevent such issues. Many gas turbine plants lose power due to dirty axial compressor blades, which can add up to 4% loss of power. In case of power plants, the power loosing could be observed by less megawatts produced
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Gulbala Alasgarov, Gulbala Alasgarov, Alovsat Baghirov Alovsat Baghirov, and Shahriyar Baghirov Shahriyar Baghirov. "DIAGNOSTICS OF THE OPTIMAL OPERATING MODES OF GAS TURBINE COMPRESSOR STATIONS BASED ON THE ANALYSIS OF TECHNOLOGICAL PROCESSES." PAHTEI-Procedings of Azerbaijan High Technical Educational Institutions 12, no. 01 (2022): 14–28. http://dx.doi.org/10.36962/pahtei1201202214.

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The article is dedicated to the analysis of the influence of the seasonally changing ambient temperature on the technological parameters of the compression process at a gas turbine compressor station for the transportation of natural and associated gas collected from oil and gas fields by an offshore subsea gas pipeline. As a result of the analysis, indicators of suction and discharge pressure, compressor capacity, ambient temperature during the summer and winter months were collected at each stage of a multi-unit two-stage compressor station. The indicators were divided into intervals, the nu
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E. H. Betelmal, A. M. Naas, and A. Mjani. "Energy and exergy analysis of a simple gas turbine combined with linde cycle and N2 injected into the compressor of the gas turbine." GSC Advanced Engineering and Technology 1, no. 1 (2021): 006–15. http://dx.doi.org/10.30574/gscaet.2021.1.1.0001.

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In this paper, we investigated a thermodynamic model of the regeneration gas turbine cycle with nitrogen supplied during the compression process. A suitable quantity of nitrogen that comes from the air separation cycle (Linde cycle) is injected between the stages of the compressor where it is evaporated, then the nitrogen and air mixture enters into the combustion chamber where it is burned and expanded in the turbine. We used this method to reduce greenhouse gases and improve gas turbine efficiency. In this work, we evaluated the operational data of the regeneration gas turbine cycle and the
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Tretyakova, P. A., T. V. Germanova, and T. V. Tretyakova. "Improving energy efficiency at compressor stations using waste heat boilers at gas turbine plants." IOP Conference Series: Earth and Environmental Science 990, no. 1 (2022): 012052. http://dx.doi.org/10.1088/1755-1315/990/1/012052.

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Abstract Improving the energy efficiency of compressor stations is currently an urgent problem in the gas industry. Increasing the pressure of the transported gas by compression with the use of gas turbine units as a compressor drive is the most energy-intensive heat-and-power process. The article discusses modern methods of increasing the energy efficiency of compressor s tations with gas pumping units operating based on gas turbine plants by utilizing the heat of exhaust gases from gas turbine plants. A complex system is considered, which includes a gas pumping unit, a gas turbine unit, a wa
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Betelmal, E. H., and S. A. Farhat. "Energy and Exergy Analysis of a Simple Gas Turbine Cycle with Wet Compression." Mechanical Engineering Research 8, no. 1 (2018): 30. http://dx.doi.org/10.5539/mer.v8n1p30.

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A thermodynamic model of the wet compressor in a simple gas turbine cycle was investigated in this paper. A suitable quantity of water was injected into the compressor-stages where it evaporated. Subsequently, the steam and air were heated in the combustion chamber and expanded in the turbine. The wet compressor (WC) has become a reliable way to reduce gas emissions and increase gas turbine efficiency. In this study, the operational data of the simple gas turbine and the maximum amount of water that can be injected into the compressor were assessed, as well as a comparison between the dry comp
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Chen, L., W. Zhang, and F. Sun. "Power and efficiency optimization for combined Brayton and two parallel inverse Brayton cycles. Part 1: Description and modelling." Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science 222, no. 3 (2008): 393–403. http://dx.doi.org/10.1243/09544062jmes640a.

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A thermodynamic model for open combined Brayton and two parallel inverse Brayton cycles is established using finite-time thermodynamics in part A of the current paper. The flow processes of the working fluid with the pressure drops of the working fluid and the size constraints of the real power plant are modelled. There are 17 flow resistances encountered by the gas stream for the combined Brayton and two parallel inverse Brayton cycles. Six of these, the friction through the blades and vanes of the compressors and the turbines, are related to the isentropic efficiencies. The remaining flow re
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Feng, Yee Chang. "A Clean Energy Generation System of In-Tandem Combinations Each of Heat Pump, Compressor and Turbine in Wind Tunnel." Applied Mechanics and Materials 705 (December 2014): 289–94. http://dx.doi.org/10.4028/www.scientific.net/amm.705.289.

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This is a series of in-tandem combinations each of heat pump, air compressor, and air turbine disposed in a wind tunnel, working together to generate clean/renewable electricity. The air compressor, located at downstream of the preceding air turbine, extracts air from this turbine thus reduces its backpressure and causes pressure drop at the turbine exit. Turbine output work Wtb is proportional to temperature difference (T3-T4) of turbine inlet/outlet air, which varies exponentially with turbine outlet/inlet air pressure ratio P4/P3 in adiabatic process as below: Wtb = MCp (T3-T4) = MCpT3{1-P4
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Caguiat, Daniel E. "Rolls Royce/Allison 501-K Gas Turbine Antifouling Compressor Coatings Evaluation." Journal of Turbomachinery 125, no. 3 (2003): 482–88. http://dx.doi.org/10.1115/1.1573665.

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The Naval Surface Warfare Center, Carderock Division (NSWCCD) Gas Turbine Emerging Technologies Code 9334 was tasked by NSWCCD Shipboard Energy Office Code 859 to research and evaluate fouling resistant compressor coatings for Rolls Royce Allison 501-K Series gas turbines. The objective of these tests was to investigate the feasibility of reducing the rate of compressor fouling degradation and associated rate of specific fuel consumption (SFC) increase through the application of anti-fouling coatings. Code 9334 conducted a market investigation and selected coatings that best fit the test objec
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Sanaye, Sepehr, and Salahadin Hosseini. "Off-design performance improvement of twin-shaft gas turbine by variable geometry turbine and compressor besides fuel control." Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy 234, no. 7 (2019): 957–80. http://dx.doi.org/10.1177/0957650919887888.

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A novel procedure for finding the optimum values of design parameters of industrial twin-shaft gas turbines at various ambient temperatures is presented here. This paper focuses on being off design due to various ambient temperatures. The gas turbine modeling is performed by applying compressor and turbine characteristic maps and using thermodynamic matching method. The gas turbine power output is selected as an objective function in optimization procedure with genetic algorithm. Design parameters are compressor inlet guide vane angle, turbine exit temperature, and power turbine inlet nozzle g
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Gao, Han, Hao Wang, Ming-Rui Zhang, Xiao-Lu Ma, and Yang-Yang Yu. "Optimization Simulation Analysis of Noise Reduction Based on the Mechanism of Noise Generation and Transmission in Turbine Compressors." Journal of Computers 36, no. 1 (2025): 255–70. https://doi.org/10.63367/199115992025023601017.

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Turbine compressors are highly efficient power compressors widely used in fields such as chemical engineering and refrigeration. However, there is vibration during compressor operation, and the vibration noise is amplified through the transmission path of the compressor structure itself, which has adverse effects on the production environment and the health of operators. Therefore, this article analyzes the mechanism of vibration noise generation and vibration propagation in turbine compressors, and constructs a vibration and vibration transmission path model. Based on the above two models, by
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Dissertations / Theses on the topic "Turbine compressor"

1

Khan, Jobaidur Rahman. "Fog Cooling, Wet Compression and Droplet Dynamics In Gas Turbine Compressors." ScholarWorks@UNO, 2009. http://scholarworks.uno.edu/td/908.

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During hot days, gas turbine power output deteriorates significantly. Among various means to augment gas turbine output, inlet air fog cooling is considered as the simplest and most costeffective method. During fog cooling, water is atomized to micro-scaled droplets and introduced into the inlet airflow. In addition to cooling the inlet air, overspray can further enhance output power by intercooling the compressor. However, there are concerns that the water droplets might damage the compressor blades and increased mass might cause potential compressor operation instability due to reduced
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Dong, Yuan. "Boundary layers on compressor blades." Thesis, University of Cambridge, 1988. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.278266.

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Farmakalides, C. D. "The effects of reaction on axial compressor performance." Thesis, Cranfield University, 1992. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.305299.

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Tain, Ludovic. "Compressor leading edges in incompressible and compressible flows." Thesis, University of Cambridge, 1998. https://www.repository.cam.ac.uk/handle/1810/272432.

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Afanasiev, Gennadiy. "DAMAGE MODELING METHOD FOR TURBINE COMPRESSOR BLADE TUNING." Master's thesis, University of Central Florida, 2004. http://digital.library.ucf.edu/cdm/ref/collection/ETD/id/4395.

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The thesis presents a method of evaluation for blade damage in Combustion Turbine Compressor Section. This method involves use of multiple domains within a single Finite Element Model to predict the effect of damage on the blade properties. This approach offers significant time and effort savings when compared to traditional evaluation methods of similar problems. It is demonstrated via examples that the multi-domain modeling approach yields acceptable accuracy results. The economical implications of described method are readily applicable to both the industrial and the aerospace Combustion Tu
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Krige, David Schabort. "Performance evaluation of a micro gas turbine centrifugal compressor diffuser." Thesis, Stellenbosch : Stellenbosch University, 2013. http://hdl.handle.net/10019.1/80119.

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Thesis (MScEng)--Stellenbosch University, 2013.<br>ENGLISH 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
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Doukelis, Angelos F. "Study of the flowfield in the tip clearance region of compressor bladings." Thesis, Cranfield University, 1998. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.267342.

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Vigueras, Zuniga Marco Osvaldo. "Analysis of gas turbine compressor fouling and washing on line." Thesis, Cranfield University, 2007. http://hdl.handle.net/1826/2448.

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This work presents a model of the fouling mechanism and the evaluation of compressor washing on line. The results of this research were obtained from experimental and computational models. The experimental model analyzed the localization of the particle deposition on the blade surface and the change of the surface roughness condition. The design of the test rig was based on the cascade blade arrangement and blade aerodynamics. The results of the experiment demonstrated that fouling occurred on both surfaces of the blade. This mechanism mainly affected the leading edge region of the blade. The
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Luiten, Ruben Vincent. "Performance improvement of the Rover 1S/60 Gas Turbine Compressor." Thesis, Stellenbosch : Stellenbosch University, 2015. http://hdl.handle.net/10019.1/97049.

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Thesis (MEng)--Stellenbosch University, 2015.<br>ENGLISH 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
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Branehög, Johan. "An investigation of the feasibility of composite turbine compressor blades." Master's thesis, University of Cape Town, 2000. http://hdl.handle.net/11427/4966.

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Includes bibliographical references.<br>A study has been conducted as to the feasibility of using a carbon fibre reinforced polymer (CFRP) composite to replace the titanium alloy (Ti-6Al-4V) for the manufacture of turbine compressor blades. These blades are used in the first compression stage of a gas turbine and suffer from high stresses at the roots and rotor discs induced by the high centrifugal forces during operation and are sensitive to vibrations. The blades are of a transonic type with typical rotational speeds of up to 10 000 rpm. The lighter composite blade will reduce stresses on th
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Books on the topic "Turbine compressor"

1

Center, Lewis Research, ed. T55-L-712 turbine engine compressor housing refurbishment. National Aeronautics and Space Administration, 1987.

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S, Yuhas John, United States. National Aeronautics and Space Administration., and United States. Army Aviation Research and Technology Activity., eds. T55-L-712 turbine engine compressor housing refurbishment: Plasma spray project. National Aeronautics and Space Administration, 1988.

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S, Yuhas John, United States. National Aeronautics and Space Administration., and United States. Army Aviation Research and Technology Activity., eds. T55-L-712 turbine engine compressor housing refurbishment: Plasma spray project. National Aeronautics and Space Administration, 1988.

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Davitt, James A. A baseline expert control system for marine gas turbine compressor surge. Naval Postgraduate School, 1989.

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B, Murthy S. N., United States. National Aeronautics and Space Administration., and United States. Federal Aviation Administration., eds. Jet engine simulation with water ingestion through compressor. National Aeronautics and Space Administration, 1987.

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United States. Army Aviation Research and Technology Activity. and United States. National Aeronautics and Space Administration., eds. Effects of inlet distortion on the development of secondary flows in a subsonic axial inlet compressor rotor. National Aeronautics and Space Administration, 1991.

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Chmielniak, Tadeusz. SYMKOM'99: International conference compressor & turbine stage flow path theory, experiment & user verification. Politechnika Łʹodzka, Instytut Maszn Przeoływowych, 1999.

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Melvin, Freling, Friedrich L. A, and Lewis Research Center, eds. Materials for Advanced Turbine Engines (MATE): Project 4--erosion resistant compressor airfoil coating. National Aeronautics and Space Administration, 1987.

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P, Shreeve Raymond, and Lewis Research Center, eds. Comparison of calculated and experimental cascade performance for controlled-diffusion compressor stator blading. National Aeronautics and Space Administration, Lewis Research Center, 1986.

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C, Smith Steven. Airflow calibration of a bellmouth inlet for measurement of compressor airflow in turbine-powered propulsion simulators. National Aeronautics and Space Administration, Ames Research Center, 1985.

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Book chapters on the topic "Turbine compressor"

1

Decher, Reiner. "The Compressor: Gas Turbine Engine Keystone." In The Vortex and The Jet. Springer Singapore, 2022. http://dx.doi.org/10.1007/978-981-16-8028-1_10.

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AbstractAll engines involve the raising of pressure in the engine’s medium, be it liquid compression of water, piston-cylinder compression of air or compression by aerodynamic forces. The last is the hardest because it is required to be efficient and stable. An aerodynamic air compressor works by slowing velocities to raise pressure. The airfoil has a difficult time doing this reliably and well and so does the compressor. When it does, it allows for amazing performance of the engine in terms of power and efficiency.
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Li, Zhihui. "Research of Helium Thermal Power System Based on Lead-Cooled Fast Reactor." In Springer Proceedings in Physics. Springer Nature Singapore, 2023. http://dx.doi.org/10.1007/978-981-99-1023-6_78.

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AbstractThe Helium Brayton cycle with re-compression has the advantages of compact layout, simple structure, thermal high efficiency, good heat transfer characteristics and small friction characteristics, its application in the power conversion system of the lead-cooled fast reactor and the high temperature gas-cooled reactor helps the miniaturization of the whole system. In this paper, the mathematical model was established for Helium Brayton cycle with re-compression and the 100 MWt lead-cooled fast reactor power system was calculated. The effects of several key factors such as the turbine i
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Schobeiri, Meinhard T. "Turbine and Compressor Cascade Flow Forces." In Turbomachinery Flow Physics and Dynamic Performance. Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-24675-3_6.

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Schobeiri, Meinhard T. "Losses in Turbine and Compressor Cascades." In Turbomachinery Flow Physics and Dynamic Performance. Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-24675-3_7.

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Schobeiri, Meinhard T. "Turbine and Compressor Cascade Flow Forces." In Gas Turbine Design, Components and System Design Integration. Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-58378-5_5.

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Schobeiri, Meinhard T. "Losses in Turbine and Compressor Cascades." In Gas Turbine Design, Components and System Design Integration. Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-58378-5_6.

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Schobeiri, Meinhard T. "Turbine and Compressor Cascade Flow Forces." In Gas Turbine Design, Components and System Design Integration. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-23973-2_5.

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Schobeiri, Meinhard T. "Losses In Turbine and Compressor Cascades." In Gas Turbine Design, Components and System Design Integration. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-23973-2_6.

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Schobeiri, Meinhard. "Turbine and Compressor Cascade Flow Forces." In Turbomachinery Flow Physics and Dynamic Performance. Springer Berlin Heidelberg, 2005. http://dx.doi.org/10.1007/978-3-540-26591-7_6.

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Schobeiri, Meinhard. "Losses in Turbine and Compressor Cascades." In Turbomachinery Flow Physics and Dynamic Performance. Springer Berlin Heidelberg, 2005. http://dx.doi.org/10.1007/978-3-540-26591-7_7.

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Conference papers on the topic "Turbine compressor"

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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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Wang, Yunhui, Qun Zheng, Yufeng Sun, and Guoxue Wang. "Theoretical and Experimental Study of Compressor and Gas Turbine Performances With Wet Compression." In 2002 4th International Pipeline Conference. ASMEDC, 2002. http://dx.doi.org/10.1115/ipc2002-27077.

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Theoretical and experimental study of compressor and gas turbine performance with wet compression has been carried out on S1A-02 industrial gas turbine to reveal its effects on gas turbines, compressors. Experiment results show that wet compression has significantly effects on performances of gas turbines and compressors; under situations of high ambient temperature, wet compression can be used to restore engine power output.
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Zampieri, Giuliano, and Vanni Damiani. "Italian Compressor Stations for Gas Storage." In ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1993. http://dx.doi.org/10.1115/93-gt-364.

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In Italy the gas transmission network, more than 23.000 km long, has 21 compressor stations with a total power of 500 MW. Some of the stations are used only for transmission purposes while others can also be used alternately or at the same time to compress gas into storage fields (Fig.1). Italy has one of Western Europe’s biggest gas reserves in storage fields: in fact the working gas used at the moment is about 12 Gm3 and the gas in place is about 24 Gm3. The total compression capacity is about 90 Mm3/d with discharge pressures of up to 150 bar. All the stations are remote controlled with no
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Bhirud, Mehul, Bharatkumar Valand, and Ankit Rathod. "Structural Validation of Portable Compressor Trailer Under Dynamic Conditions." In ASME 2023 Gas Turbine India Conference. American Society of Mechanical Engineers, 2023. http://dx.doi.org/10.1115/gtindia2023-118377.

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Abstract Portable air screw compressors are the most reliable, effective, and well-suited for the unique needs of building roads, performing restoration work, conducting civil engineering, mining, sandblasting, oil and gas exploration etc. This compressors must be designed to withstand tough site circumstances and difficult-to-reach site locations that may have challenging topography. Compressed air at remote locations is also used to power tools on the site, such as power hammers, drills, saws, wrenches, nail guns etc. These portable compressors are exposed to higher load such as dynamic load
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Bakken, Martin, and Tor Bjørge. "An Experimental Investigation on Hysteresis in a Wet Gas Compressor." In ASME 2017 Gas Turbine India Conference. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/gtindia2017-4518.

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Performance monitoring of wet gas compressors is challenging due to the liquid phase impact on performance. Introduction of a liquid phase alters both the thermodynamics as well as the fluid dynamics of the compression process. Hence, understanding the flow interaction between the impeller, diffuser and volute is pivotal. Previous investigations have detected occurrence of compressor hysteresis at certain wet gas operating conditions, resulting in temporary deviations from the steady state compressor characteristics. This kind of behavior influences both the compressor stability and performanc
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McKee, Robert J. "Mapping and Predicting Air Flows in Gas Turbine Axial Compressors." In ASME Turbo Expo 2003, collocated with the 2003 International Joint Power Generation Conference. ASMEDC, 2003. http://dx.doi.org/10.1115/gt2003-38745.

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Determining the airflow through a gas turbine’s axial compressor is not a simple or one step process as many factors affect flow and there is seldom a flow meter or a means to directly measure airflow rate. Speed of the compressor, inlet pressure and temperature, and resistance or backpressure at the compressor’s outlet all affect the amount of airflow. The type of gas turbine, single or twin spool, the magnitude of power produced, the use of bleed or bypass valves, the power turbine speed, and operating conditions all have influences on the amount of airflow. Despite this, there are several r
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Ebisawa, Naoto, Yasuo Fukushima, and Hideaki Orikasa. "Dynamic Simulation of Centrifugal Compressor Startup With Inlet Guide Vane." In ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition. ASMEDC, 2011. http://dx.doi.org/10.1115/gt2011-45810.

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To achieve safe and efficient operation of centrifugal compressors, understanding the transient behavior of the compression system and reflecting such characteristics into the design of compressors and peripheral equipment early in the plant engineering stage are important. Since such transient states cannot be completely studied by static analysis alone, additional analyses using plant’s dynamic model are desired. To utilize for compressor design and process verification in the engineering phase, a dynamic simulator specialized for compressor systems has been developed. The presented work dem
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Taylor, Joe S. "Gas Turbine Compressor Unit Repowering." In 1996 1st International Pipeline Conference. American Society of Mechanical Engineers, 1996. http://dx.doi.org/10.1115/ipc1996-1893.

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This paper presents how a major U.S. gas transmission and storage company restored gas storage peaking capacity by repowering obsolete gas turbine compressor units. Consumers Power Company’s Ray Field located in Macomb County, Michigan, USA, was developed as a 44 BCF working capacity gas storage field in 1966. Due to the high deliverability, the field is operated as a peaking reservoir, handling rates as high as 500 MMCFD on injection and 1,200 MMCFD on withdrawal. Ten (10) 2,750 horsepower gas turbine driven 4-stage centrifugal compressor units were installed in the mid to late 1960’s at the
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Bakken, Martin, and Tor Bjørge. "Volute Flow Influence on Wet Gas Compressor Performance." In ASME 2017 Gas Turbine India Conference. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/gtindia2017-4529.

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The world’s energy demand is increasing, asking for new and cost-efficient ways to extract oil and gas. With traditional technologies, oil and gas production relies on a sufficiently high well head pressure for transportation to nearby process facilities. Utilization of subsea wet gas compression systems enables production at significantly lower pressures and is a favourable solution concerning production in remote regions. Wet gas compressors are particularly useful when handling multiphase mixtures consisting of 95%–100% gas, on a volumetric basis. The remaining content is water and liquid c
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Farahani, A. Shahrabi, H. Beheshti Amiri, H. Khazaei, A. Madadi, and A. Fathi. "The Effect of Reynolds Number on Transonic Compressor Blade Rotor Section." In ASME 2012 Gas Turbine India Conference. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/gtindia2012-9639.

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To achieve at a more precise designing procedure in axial-compressors as well as a higher pressure ratio value, a comprehensive understanding on the flow aerodynamics and the governing phenomena is required. Existence of these complicated phenomena e.g., simultaneous production of supersonic and subsonic flows, shock-boundary layer interaction, unique incidence phenomenon, etc, makes it difficult to analyze the flow in the transonic compressors. One of the methods which is useful in the modeling of the phenomena occur in the compressors is investigating the flow in the blade to blade passage.
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Reports on the topic "Turbine compressor"

1

Lawson. L51597 Feasibility Study of New Technology for Intake Air Filtration. Pipeline Research Council International, Inc. (PRCI), 1989. http://dx.doi.org/10.55274/r0010105.

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Inlet air filters are widely used to remove solids and liquid droplets from the ambient air before it enters the compressor of a gas turbine. Clean inlet air provides many advantages: Less corrosion of the compressor and of gas-path hot parts, such as the turbine, decreased compressor fouling, less erosion of the compressor bladeThese in turn prevent deterioration of output and heat rate, and reduce maintenance costs. Compressor fouling is caused by the ingestion of substances that deposit and adhere to blade surfaces, resulting in reduced aerodynamic efficiency and decreased available output.
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2

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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3

Beshouri. PR-309-04200-R01 Modeling Methodology for Parametric Emissions Monitoring System for Combustion Turbines. Pipeline Research Council International, Inc. (PRCI), 2005. http://dx.doi.org/10.55274/r0010731.

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Prior attempts to develop a generic Parametric Emissions Monitoring methodology for combustion turbines, particularly low emissions units, have failed due either to the reduction of a complex problem to too few degrees of freedom or the brute force reliance on regression analysis. Field test data collected by the research team clearly illustrated that a successful PEMS model will need to incorporate multiple zones to account for pilot fuel versus pre-mixed combustion, and changes in air/fuel ratio at the flame front. The information reported herein shows that, ideally, the PEMS model should re
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4

Lawson. L51558 Gas Turbine Intake Air Quality. Pipeline Research Council International, Inc. (PRCI), 1988. http://dx.doi.org/10.55274/r0010941.

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Presents the results of preliminary research intended to evaluate the causes and effects of compressor fouling on pipeline gas turbines. The conclusions and recommendations presented are based on both a literature search and a field experience survey of principal pipeline operations.
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5

Henderson, A. PR-273-07202-R01 Gas Turbine Driven Compressor Station Efficiency Improvement Study. Pipeline Research Council International, Inc. (PRCI), 2008. http://dx.doi.org/10.55274/r0011005.

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6

Amos, Ian, and Rick Hackney. PO-743-22201-R01 Validation of Next Generation Predictive Emissions Monitoring System for Gas Turbines. Pipeline Research Council International, Inc. (PRCI), 2024. http://dx.doi.org/10.55274/r0000071.

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This report describes field trial demonstration and validation of a Gas Turbine Predictive Emissions Monitoring System (PEMS) using engine data from Siemens Energy SGT-300 gas turbine compressor drivers at SoCalGas Blythe Compressor Station, California, USA. The advanced PEMS model results are compared with CEMS data taken from process analyzers measuring emissions in the gas turbine exhaust. After the necessary corrections on emissions for water content and oxygen content in the exhaust, the values for PEMS and CEMS show good agreement across a wide range of operating conditions. Areas where
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7

Grauer and Chapman. L52331 Exhaust Manifold Design Guidelines to Optimize Scavenging and Turbocharger Performance. Pipeline Research Council International, Inc. (PRCI), 2009. http://dx.doi.org/10.55274/r0010664.

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To develop the requisite air flow rate, the turbocharger must operate at a relatively high efficiency. But as important, the system pressure losses must be minimized to optimize turbocharger operating flexibility so that the turbine can produce sufficient power to operate the turbocharger compressor. The relationship between the various pressures and pressure losses throughout the turbocharged engine system, the turbocharger overall efficiency, ambient conditions, and the required turbine inlet temperature for sustainability is rooted in fundamental thermodynamic principles. The goal of the Ex
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8

Steward, W. Gene. Flow Integrating Section for a Gas Turbine Engine in Which Turbine Blades are Cooled by Full Compressor Flow. Office of Scientific and Technical Information (OSTI), 1999. http://dx.doi.org/10.2172/764563.

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9

Allison. PR-015-10200-R01 Alternatives to Gas Turbine Expansion Starters. Pipeline Research Council International, Inc. (PRCI), 2013. http://dx.doi.org/10.55274/r0010775.

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Existing expansion-type starters at pipeline compressor stations require a significant quantity of start gas for purge, startup, and slow roll operating conditions, but they are widely used due to their relatively low cost and black-start capability. This effort examines the potential for available, easily adaptable, and new starter concepts and ranked them for various applications.
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10

Jay. L51723 Guidelines for Sound Power Level Measurements Compressor Equipment. Pipeline Research Council International, Inc. (PRCI), 1994. http://dx.doi.org/10.55274/r0010419.

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Increasing legislation and public awareness of noise are intensifying the efforts of industries today to reduce the noise. The natural gas industry has proved that it is one of the industrial leaders in its awareness of noise problems and has maintained a vigorous research program in noise control for over 30 years. A noise survey can be done in several ways: point measurements, grid point methods, contour methods, scanning techniques, etc. The selection of the method depends on the accuracy required, available personnel, expertise etc. For the most accurate determination of sound power, the s
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