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Abstract

This paper analyses the influence of three different ring-type inlet duct geometries on the performance of a small 1 MW backpressure steam turbine. It examines the efficiency and pressure drop of seven turbine variants, including four spiral inlet geometries and three stages with a mass flow rate around 30 t/h. A one-pipe and two-pipe inlets are analysed from aerodynamical point of view, taking into account stator and rotor blades in three stages without the outlet. An outlet is added to the best variant. Also analysed is the occurrence of vortices in the inlets of the studied variants 1–7 as well as the efficiency, drop pressure, turbine power and mass flow. Finally, the best inlet for a 1 MW steam turbine is suggested.
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Bibliography

[1] Bellucci J., Rubechin F., Arnone A.: Modeling partial admission in control stages of small steam turbines with CFD. In: Proc. ASME Turbo Expo, June 11-15 2018 Oslo, GT2018-76528, 2018.
[2] Lampart P., Szymaniak M., Rzadkowski R.: Unsteady load of partial admission control stage rotor of a large power steam turbine. In: Proc. ASME Turbo EXPO 2004, Power for Land, Sea and Air, June 14–17, 2004, Vienna, ASME GT-2004- 53886, 2004.
[3] Van den Braembussche R.A.: Flow and loss mechanisms in volutes of centrifugal pumps. Educational Notes. In: Design and Analysis of High Speed Pumps (12-1–12- 26). Educational Notes RTO-EN-AVT-143, Neuilly-sur-Seine, RTO, 2006 (available from: http://www.rto.nato.int/abstracts.asp).
[4] Drexler C.: Strömungsvorg ange und Verlustanteile in ungleichformig beaufschlagten Turbinenstufen. PhD thesis, RWTH Aachen University, Aachen 1996. Computational fluid dynamics analysis of 1 MW steam turbine inlet geometries 55
[5] Traupel W.: Thermische Turbomaschinen (4th Edn.). Springer, 2001.
[6] Kovats A.: Effect of non-rotating passages on performance of centrifugal pumps and subsonic compressors. In: Proc. Winter Annual Meeting, New York 1979.
[7] Lüdtke K.: Centrifugal process compressors – radial vs. tangential suction nozzles. In: ASME Paper 85-GT-80, 1985.
[8] Sievert R.: Analyse der Einflussparameter auf die Strömung im Eintritt von Niederdruck-Dampfturbinen. PhD thesis, Ruhr-Universität Bochum, Bochum 2006 (in German).
[9] Maier W.: Inlet casing for a turbine. US Patent US5927943A, 1999.
[10] Škach R., Uher J.: Spiral Inlets for Steam Turbines. AIP Conf. Proc. 1889, 020038, 2017.
[11] Hecker S., Rohe A., Stoff H.: Steam turbine inlet geometry from a structural and fluid dynamics point of view. In: Proc. ASME Turbo Expo 2012, GT2012-68678, 2012, 487–495.
[12] Gao K., Wang C., Xie Y., Zhang D.: Effects of inlet chamber structure of the control stage on the unsteady aerodynamic force. In: Proc. ASME Turbo Expo, Oslo, June 11–15 2018, GT2018-76632, 2018.
[13] Engelmann D., Schram A., Polklas T., Mailch P.: Losses of steam admission in industrial steam turbines depending on geometrical parameters. In: Proc. ASME Turbo Expo, Dusseldorf – Oslo, June 16-20 2014, GT2014-25172, 2014.
[14] Dejch M.,E., Filippov G.A., Lazarev L.Ja.: Collection of Profiles for Axial Turbine Cascades. Machinostroienie, Moscow 1965 (in Russian).
[15] Kietlinski K., Czerwinski P.: Retrofit of 18K370 steam turbine on the units 7–12 at Belchatow Power Plant. Arch. Energ. XLI(2011), 3-4, 77–96.
[16] Ansys CFX, Release 18.2.
[17] Ansys Meshing, Release 18.2
[18] Ansys TurboGrid, Release 18.2
[19] Ansys DesignModeller, Release 18.2
[20] Ansys CFX, Release 18.2, CFX documentation. Ansys, Inc.
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Authors and Affiliations

Arkadiusz Koprowski
1
Romuald Rzadkowski
1 2

  1. Institute of Fluid Flow Machinery Polish Academy of Sciences, Fiszera 14, 80-952 Gdansk, Poland
  2. Air Force Institute of Technology, Ksiecia Bolesława 6, 01-494 Warsaw, Poland
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Abstract

Problems related to power control of low power-output steam turbines are analyzed. These turbines are designed to operate in distributed power generation systems. Principles of automatic control involving a single control valve are presented on the basis of experience gathered with high power-output turbines. Results of simulations of power control for a low power-output turbine are discussed. It has been proven that closing of the control system and an application of a power controller (of optimally selected parameters) improves the object dynamics (shortening of the transition period). At the same time, a lack of such optimization can results in occurrence of undesirable phenomena such as: overshoot in the generator power characteristics, elongation of the response time to disturbance or overshoot of turbine control valves.
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Bibliography

[1] Karczewski J., Szuman P.: Electrohydraulic Ccontrol of Real Power of Turbosets in the Power and Electricity Generation System Control. Monografie 6. Wydawn. Inst. Energ., Warszawa 2020 (in Polish).
[2] Domachowski Z.: Automatic Control of Thermal Turbosets. Wydawn. PG, Gdansk 2014 (in Polish).
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[5] Chmielniak T.: Power Generation Technologies. PWN, Warszawa 2021 (in Polish).
[6] Kryłłowicz W., Szwaja S.: A lowpower-output steam turbine in a system with a heat recovery boiler. Project rep. POIG 01.03.01-26-021/12, Czestochowa 2015 (in Polish).
[7] Gundlach W.: Turbomachinery. PWN, Warszawa 1970 (in Polish). [8] Karczewski J., Szuman P.: Scilab. Modelling and Simulation of Control System Operation. Nakom, Poznan 2019 (in Polish).
[9] Karczewski J.: Coordination of loading of boiler and turbine systems in an electricpower unit. IEEE Catalog Number CFP19H21-ART.: ISBN: 978-1-7281-2053-9.
[10] Karczewski J., Pawlak M.: Power control problems of units co-burning biomass. Arch. Energ. XLI(2011), 3–4, 29–39.
[11] Karczewski J., Pawlak M., Szuman P., Wasik P.: Assessment of availability of the power unit participating in the regulation of the electrical power system. Arch. Energ. XL(2010), 1–2, 89–102.
[12] Karczewski J., Szuman P.: Testing of the power unit control systems using power unit and its parts simulation model. Elektronika (2018), 11 (in Polish).
[13] Karczewski J., Szuman P.: Testing of the power unit control systems using power unit simulator. Elektronika (2017), 11 (in Polish).
[14] Karczewski J., Szuman P.: Power unit work optimization based on simulation of various control system configurations. Prace Inst. Elektrotechn. 270(2015) (in Polish).
[15] Karczewski J., Szuman P.: Simulation of various control system configuration of power units. Elektronika (2015), 12 (in Polish).
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Authors and Affiliations

Władysław Kryłłowicz
1
Jacek Karczewski
2
Paweł Szuman
2

  1. Lodz University of Technology, Institute of Turbomachinery, Wolczanska 217/221, 93-003 Lodz, Poland
  2. Institute of Power Engineering, Mory 8, 01-330 Warsaw, Poland
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Abstract

The paper presents the results of the numerical analyses for the steam turbine rotor, dedicated for the newly-designed 900 MW steam unit with supercritical steam parameters (650 °C, 30.0 MPa). Basing on the design calculations, an optimal design solution was determined. Review of the available literature on materials for turbine rotors with supercritical steam parameters was done. Then the start-ups of the turbine were simulated. Thermal and strength states were analyzed. As a result, an optimal start-up characteristic was obtained.

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Authors and Affiliations

Henryk Łukowicz
Andrzej Rusin
Marian Lipka
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Abstract

In small steam turbines, sometimes the efficiency is not as important as the cost of manufacturing the turbine. The Curtis wheel is a solution allowing to develop a low output turbine of compact size and with a low number of stages. This paper presents three fully dimensional computational fluid dynamics cases of a Curtis stage with full and partial admission. A 1 MW steam turbine with a Curtis stage have been designed. The fully admitted stage reaches a power of over 3 MW. In order to limit its output power to about 1 MW, the partial admission was applied. Five variants of the Curtis stage partial admission were analyzed. Theoretical relations were used to predict the partial admission losses which were compared with a three-dimensional simulations. An analysis of the flow and forces acting on rotor blades was also performed.
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Bibliography

[1] Achille M., Cardarelli S., Pantano F., Zito M.: Design and CFD analysis of a Curtis turbine stage. In: Proc. 29th Int. Conf. on Efficiency, Cost, Optimisation, Simulation and Environmental Impact of Energy Systems, ECOS 2016, Portorož, June 19–23, 2016.
[2] Rashid S., Tremmel M., Waggott J., Moll R.: Curtis stage nozzle/rotor aerodynamic interaction and the effect on stage performance. J. Turbomach. 129(2007), 3, 551–562
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[4] Surwilo J., Lampart P., Szymaniak M.: CFD analysis of fluid flow in an axial multi-stage partial-admission ORC turbine. Open Eng. 5(2015), 1, 360–364.
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[6] Pan Y., Yuan Q., Zhu G.: Numerical Investigation on the Influence of Inlet Structure on Partial-admission Losses. Proc. Chin. Soc. Electr. Eng. 38(2018), 14, 4156– 4164.
[7] Sakai N., Harada T., Imai Y.: Numerical study of partial admission stages in steam turbine. JSME Int. J. B-Fluid T. 49(2006), 2, 212–217.
[8] Lampart P., Szymaniak M., Rzadkowski R.: Unsteady load of partial admission control stage rotor of a large power steam turbine. In Proc. ASME Turbo EXPO 2004, Power for Land, Sea and Air, Vienna, June 14–17, 2004, ASME GT-2004- 53886, 2004.
[9] Koprowski A., Rzadkowski R.: Computational fluid dynamics analysis of 1 MW steam turbine inlet geometries. Arch. Thermodyn. 42(2021), 1, 35–55.
[10] Rusanov A., Rusanov R.: The influence of stator-rotor interspace overlap of meridional contours on the efficiency of high-pressure steam turbine stages. Arch. Thermodyn. 42(2021), 1, 97–114.
[11] Dejch M.E., Filippov G.A., Lazarev L.Ja.: Collection of Profiles for Axial Turbine Cascades. Machinostroienie, Moscow 1965 (in Russian).
[12] Neuimin V.M.: Methods of evaluating power losses for ventilation in stages of steam turbines of TES. Therm. Eng.+ 61(2014), 10, 765–770.
[13] Ansys CFX, Release 18.2.
[14] Ansys DesignModeller, Release 18.2.
[15] Ansys TurboGrid, Release 18.2.
[16] Ansys CFX, Release 18.2, CFX documentation.
[17] Wagner W., Pruss A.: The IAPWS formulation 1995 for the thermodynamic properties of ordinary water substance for general and scientific use. J. Phys. Chem. Ref. Data 31(2002), 2, 387–535
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Authors and Affiliations

Arkadiusz Koprowski
1
Romuald Rządkowski
1 2

  1. Institute of Fluid-Flow Machinery Polish Academy of Sciences, Fiszera 14, 80-952 Gdansk, Poland
  2. Air Force Institute of Technology, Ksiecia Bolesława 6, 01-494 Warsaw, Poland
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Abstract

The paper deals with the wet steam flow in a steam turbine operating in a nuclear power plant. Using a pneumatic and an optical probe, the static pressure, steam velocity, steam wetness and the fine water droplets diameter spectra were measured before and beyond the last turbine low-pressure stage. The results of the experiment serve to understand better the wet steam flow and map its liquid phase in this area. The wet steam data is also used to modify the condensation model used in computational fluid dynamics simulations. The condensation model, i.e. the nucleation rate and the growth rate of the droplets, is adjusted so that results of the numerical simulations are in a good agreement with the experimental results. A 3D computational fluid dynamics simulations was performed for the lowpressure part of the turbine considering non-equilibrium steam condensation. In the post-processing of the of the numerical calculation result, the thermodynamic wetness loss was evaluated and analysed. Loss analysis was performed for the turbine outputs of 600, 800, and 1100 MW, respectively.
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Bibliography

[1] Walters P.T., Skingley P.C.: An optical instrument for measuring the wetness fraction and droplet size of wet steam flow in LP turbines. In: Proc. Conf. on Steam Turbines for the 1980s, Vol. 12, London, 9–12 Oct. 1979, C141, 337–348.
[2] Kleitz A., Laali, A.R., Courant J.J.: Fog droplet size measurement and calculation in wet steam turbines. In: Proc. Int. Conf. on Technology of Turbine Plant Operating in Wet Steam (J.M. Mitchell, Ed.), London, 11–13 October 1988, 201– 206.
[3] Petr V., Kolovratník M.: Modelling of the droplet size distribution in LP steam turbine. In: Proc. 3rd Eur. Conf. on Turbomachinery – B, Fluid Dynamics and Thermodynamics, London, 2–5 March 1999, 771–782.
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[5] Hideaki S., Tabata S. Tochitani N., Sasao Y., Takata R., Osako M.: Investigation of moisture removal on last stage stationary blade in actual steam turbine. In: Proc. ASME Turbo Expo 2020, virtual, online, Sept. 21–25, 2020, GT2020-14831.
[6] Grübel M., Starzmann J., Schatz M., Eberle T., Vogt D.M., Sieverding F.: Two-phase flow modeling and measurements in low-pressure turbines – Part I: numerical validation of wet steam models and turbine modeling. J. Eng. Gas Turbines Power 137(2015), 4, 042602 (11), GTP-14-1442.
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[8] Fendler Y., Dorey J.M., Stanciu M., Lance M., Léonard O.: developments for modeling of droplets deposition and liquid film flow in a throughflow code for steam turbines. In: Proc. ASME Turbo Expo 2012, Copenhagen, June 11–15, 2012, GT2012-68968, 537–547.
[9] Gyarmathy G.: Grundlagen einer Theorie der Nassdampfturbine. PhD thesis, ETH Zurich, Juris-Verlag, Zurich 1962.
[10] Laali A.R.: A new approach for assessment of the wetness losses in steam turbines. In Proc. IMechE Conf. Turbomachinery – Latest Developments in a Changing Scene, London, March, 1991, 155–166.
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[12] Petr V., Kolovratník M.: Wet steam energy loss and related Baumann rule in low pressure steam turbines. P. I. Mech. Eng. A-J. Pow. 228(2014), 2, 206–215.
[13] Holmberg H., Ruohonen P., Ahtila P.: Determination of the real loss of power for a condensing and a backpressure turbine by means of second law analysis. Entropy 11 (2009), 4, 702–712.
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[17] Finzel C., Schatz M., Casey M.V., Gloss D.: Experimental investigation of geometrical parameters on the pressure recovery of low pressure steam turbine exhaust hoods. In: Proc. ASME Turbo Expo 2011, Vancouver, June 6–10 2011, GT2011- 45302, 2255–2263.
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[19] Hoznedl M., Kolovratník M., Bartoš O., Sedlák K., Kalista R., Mrózek L.: Experimental research on the flow at the last stage of a 1090 MW steam turbine. P. I. Mech. Eng. A-J. Pow 232(2018), 5, 515–524.
[20] Štastný M.: Flow field in the last steam turbine stage. In: Proc. 7th Eur. Conf. on Turbomachinery Fluid Dynamics and Thermodynamics , Euroturbo 7, Athens, March 5–9, 2007, 867–876.
[21] Kolovratník M., Bartoš O.: CTU optical probes for liquid phase detection in the 1000 MW steam turbine. In: Proc. EFM14 – Experimental Fluid Mechanics 2014, EPJ Web Conf. 92(2015), 02035.
[22] Brüggemann C., Schatz M., Vogt D.M., Popig F.: A numerical investigation of the impact of part-span connectors on the flow field in a linear cascade. In: Proc.ASME Turbo Expo 2017, Charlotte, June 26–30, 2017, GT2017-63359, V02AT40A005.
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Authors and Affiliations

Gukchol Jun
1 2
Michal Kolovratník
2
Michal Hoznedl
1

  1. Czech Technical University in Prague, Technická 4, 160 00, Prague, Czech Republic
  2. Doosan Škoda Power s.r.o., Tylova 1/57, 301 28, Pilsen, Czech Republic
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Abstract

Turbine stages can be divided into two types: impulse stages and reaction stages. The advantages of one type over the second one are generally known based on the basic physics of turbine stage. In this paper these differences between mentioned two types of turbines were indicated on the example of single stage turbines dedicated to work in organic Rankine cycle (ORC) power systems. The turbines for two ORC cases were analysed: the plant generating up to 30 kW and up to 300 kW of net electric power, respectively. Mentioned ORC systems operate with different working fluids: DMC (dimethyl carbonate) for the 30 kW power plant and MM (hexamethyldisiloxane) for the 300 kW power plant. The turbines were compared according to three major issues: thermodynamic and aerodynamic performance, mechanical and manufacturing aspects. The analysis was performed by means of the 0D turbomachinery theory and 3D computational aerodynamic calculations. As a result of this analysis, the paper indicates conclusions which type of turbine is a recommended choice to use in ORC systems taking into account the features of these systems.

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Authors and Affiliations

Dawid Zaniewski
Piotr Klimaszewski
Łukasz Witanowski
Łukasz Jędrzejewski
Piotr Klonowicz
Piotr Lampart
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Abstract

Consumption of energy is one of the important indicators in developing countries, but a lot of companies from the energy sector have to cope with three key challenges, namely how to reduce their impact on the environment, how to ensure the low cost of the energy production and how to improve the system overall performance? For Polish energy market, the number of challenges is greater. The growing demand for electricity and contemporary development of nuclear power technology allow today’s design, implement new solutions for high energy conversion system low unit cost for energy and fuel production. In the present paper, numerical analysis of modular high-temperature nuclear reactor coupled with the steam cycle for electricity production has been presented. The analysed system consists of three independent cycles. The first two are high-temperature nuclear reactor cycles which are equipped with two high-temperature nuclear reactors, heat exchangers, blowers, steam generators. The third cycle is a Rankine cycle which is equipped with up to four steam turbines, that operate in the heat recovery system. The analysis of such a system shows that is possible to achieve significantly greater efficiency than offered by traditional nuclear reactor technology.

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Authors and Affiliations

Michał Dudek
ORCID: ORCID
Marek Jaszczur
Zygmunt Kolenda
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Abstract

This paper presents the origins of marine steam turbine application on liquefied natural gas carriers. An analysis of alternative propulsion plant trends has been made. The more efficient ones with marine diesel engines gradually began to replace the less efficient plants. However, because of many advantages of the steam turbine, further development research is in progress in order to achieve comparable thermal efficiency. Research has been carried out in order to achieve higher thermal efficiency throughout increasing operational parameters of superheated steam before the turbine unit; improving its efficiency to bring it nearer to the ideal Carnot cycle by applying a reheating system of steam and multi stage regenerative boiler feed water heating. Furthermore, heat losses of the system are reduced by: improving the design of turbine blades, application of turbine casing and bearing cooling, as well as reduction in steam flow resistance in pipe work and maneuvering valves. The article identifies waste energy sources using the energy balance of a steam turbine propulsion plant applied on the liquefied natural gas carrier which was made out basing on results of a passive operation experiment, using the measured and calculated values from behavioral equations for the zero-dimensional model. Thermodynamic functions of state of waste heat fluxes have been identified in terms of their capability to be converted into usable energy fluxes. Thus, new ways of increasing the efficiency of energy conversion of a steam turbine propulsion plant have been addressed.

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Authors and Affiliations

Andrzej Adamkiewicz
Szymon Grzesiak
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Abstract

An important operational task for thermal turbines during run-up and run-down is to keep the stresses in the structural elements at a right level. This applies not only to their instantaneous values, but also to the impact of them on the engine lifetime. The turbine shaft is a particularly important element. The distribution of stresses depends on geometric characteristics of the shaft and its specific locations. This means a groove manufactured for fixing the rotor blades. The extreme stresses in this place occur during the start-up and the shaft heating to normal operating temperature. The process needs optimisation. Optimization tasks are multidisciplinary issues and can be carried out using different methods. In recent years, particular attention in optimisation has been paid to the use of artificial intelligence methods. Among them, a special role is assigned to genetic algorithms. The paper presents a genetic algorithm method to optimise the steam turbine shaft heating process during its start-up phase. The presented optimization task of this algorithm is to carry out the process of the shaft heating as soon as possible at the conditions of not exceeding the stresses at critical locations at any heating phase.

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Authors and Affiliations

Krzysztof Dominiczak
Marta Drosińska-Komor
Romuald Rzadkowski
Jerzy Głuch
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Abstract

Paper is considering the purpose and the process of development of last stage blade for intermediate pressure module of 13K215 steam turbine. In the last 20–30 years most of the steam turbine manufacturers were focused on improving such a turbine mainly by upgrading low pressure module. In a result of such a modernization technology were changed from impulse to reaction. The best results of upgrading were given by developing low pressure last stage blade. With some uncertainty and based on state of art knowledge, it can be stand that improving of this part of steam turbine is close to the end. These above indicators show an element on which future research should be focused on – in the next step it should be intermediate pressure module. In the primary design the height of intermediate pressure last stage blade was 500 mm but because of change of technology this value was decreased to 400 mm. When to focus on reaction technology, the height of the last stage blade is related to output power and efficiency. Considered here is the checking the possibility of implementing blades, in a reaction technology, higher than 400 mm and potentially highest. Article shows a whole chosen methodology of topic described above. It leads through the reasons of research, limitations of 13K215 steam turbine, creation of three-dimensional models, fluid flow calculations, mechanical integrity calculations and proposed solutions of design.
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Bibliography

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Authors and Affiliations

Radoslaw Bondyra
1
Jan Przytulski
1
Krzysztof Dominiczak
2

  1. GE Power Ltd, Stoczniowa 2, 82-300 Elblag, Poland
  2. Institute of Fluid Flow Machinery Polish Academy of Sciences, Fiszera 14, 80-231 Gdansk, Poland
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Abstract

The results of a systematic study of the influence of meridional contours overlap in the stator-rotor axial interspace of the impulse and reactive type stages of a high-pressure steam turbine on the flow structure and gas-dynamic efficiency of the flow part are introduced. The studied flow parts of the impulse and reactive stages are typical for high-power high-pressure steam turbines. It is shown that the stages that have no overlaps and/or have a smooth shape of meridional contours have the best gasdynamic efficiency, and the most negative effect on the flow part is caused by the presence of caverns in the stator-rotor interspace. For cases where, due to technological limitations, it is impossible to avoid the presence of caverns and overlaps with a sharp (step-wise) change in the shape of the meridional contours, it is recommended to perform overlaps with positive size of overlap values near the rotor blades.
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Authors and Affiliations

Andrii Rusanov
1
Roman Rusanov
1

  1. The A. N. Pidgorny Institute of Mechanical Engineering Problems NAS of Ukraine, Dm. Pozharsky 2/10, 61046 Kharkiv, Ukraine
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Abstract

This paper presents the results of developing a methodology for assessing and predicting the technical condition of boiler plants and steam turbines. The proposed method is based on generalized experimental data on failures to predict the damage of the principal elements and components of thermal power plants by Monte-Carlo simulation. The proposed method considers the complexity of technological processes, turnaround time, failure rate, and condition of the residual metal life. It allows developing approaches to assessing each element’s safety to obtain a reliable and representative sample of failure statistics to reliability assessment of boilers and steam turbines of thermal power plants. According to the results, the probability of failure operation of steam boilers and turbines is 0.037 in the 100 MW conditions. The obtained results can be used to create predictive models that provide approaches to prolonging the operational state of elements of boiler plants and steam turbines of thermal power plants. It can be used in the implementation of projects of digital energy systems for monitoring and diagnostics of the main power equipment of thermal power plants.
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Authors and Affiliations

Makhsud Mansurovich Sultanov
1
Stepan Anatolyevich Griga
2
Maksim Sergeevich Ivanitckii
1
Anatoly Alekseevich Konstantinov
1

  1. National Research University MPEI, Krasnokazarmennaya 17, Moscow, 111250 Russia
  2. PJSC “Mosenergo”, Vernadsky Avenue 101/3, Moscow, 119526 Russia
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Abstract

The results of the gas-dynamic calculation of the low-pressure cylinder flow part of the K-220-44 type steam turbine intended for operation at nuclear power plants are presented. The ways of the flow part improvement were determined. Some of those ways include the use of innovative approaches that were not previously used in steam turbines. The design of the new flow part was carried out on the basis of a comprehensive methodology implemented in the IPMFlow software package. The methodology includes gas-dynamic calculations of various levels of complexity, as well as methods for analytical construction of the spatial shape of the blade tracts based on a limited number of parameterized values. The real thermodynamic properties of water and steam were taken into account in 3D calculations of turbulent flows. At the final step, end-to-end 3D calculations of the lowpressure cylinder that consists of 5 stages were performed. The technology of parallel computing was applied in those calculations. It is shown that due to the application of innovative solutions, a significant increase in efficiency can be achieved in the developed low-pressure cylinder.
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Authors and Affiliations

Andrii Rusanov
1
Viktor Subotin
2
Viktor Shvetsov
2
Roman Rusanov
1
Serhii Palkov
1 2
Ihor Palkov
1 2
Marina Chugay
1

  1. The A.N. Podgorny Institute for Mechanical Engineering Problems, National Academy of Sciences of Ukraine, Pozharsky 2/10, 61046 Kharkiv, Ukraine
  2. JSC “Ukrainian Energy Machines” Moskovsky 199, 61037 Kharkiv, Ukraine

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