Formation of Prospective l.P.C. Exhaust Compartment With the 1650 mm Blade Length
DOI:
https://doi.org/10.20998/2078-774X.2018.12.01Анотація
The results of computational design and numerical studies of the low-pressure cylinder exhaust chamber flow path with the last stage with a 1650 mm length blade are considered. The flow path of stage contained a suction of a moisture-intensive vapor from the interrow gap, a channel of the predetermined interstage gap with steam extraction, an exhaust pipe, taking into account the installation of the system cooling and transition nozzle. All the computations were based on the model of one speed wet steam flow without droplets and super cooling was not taken into account. The sectorial approach was applied to description of the interaction of the last stage and exhaust hood. The stages were considered in steady state formulation. The initial data and boundary conditions were taken basing on results of flow simulation of whole L.P.C flow path [1, 2]. Some methodological aspects and the directions of improving of studied facilities in numerical experiment by MTFS® code are discussed.
Посилання
Solodov, V., and Konev, V. (2017), "Improvement of the flow patр of L.P.C. of a powerful steamturbinetakingintoaccountleaksуstem", Bulletin of NTU "KhPI". Series: Hydraulic machines and hydrounits, 2017, no. 42(1264),pp.43–50.(InRussian)
Solodov, V., Shvetsov, V., and Konev, V. (2017), "Numerical model of L.P.C. flow path with leak system of powerfulsteamturbine unit", Bulletin of NTU "KhPI". Series: Power and heat engineering processes and equipment, 2017, no. 8(1230). pp. 6–12,ISSN 2078-774X, doi: 10.20998/2078-774x.2017.08.01 (In Russian).
RТМ 108.020.120-77 Aerodynamic profiling and calculation of exhaust nozzles of low-pressure cylinders of steam turbines.
(1980), Heat Turbine Stages Aerodynamical Characteristics, Ed. By V.A. Chernikov V.A, Mashinostroenie, Leningrad, 262 p.(In Russian).
Solodov, V.G., Starodubtsev, Yu.V. (2002), "The Scientific Application Software MTFS® for Calculation of 3DViscousTurbulent Liquid and Gas Flows in Arbitrary Shape Domains", Certificate of State Registration, UkrainianStateAgencyofCopyrightsandRelated Rights, No. 5921, 07.16.2002 (In Ukrainian).
Solodov, V.G., and Starodubtsev, Yu.V. (2004), "The experience of 3D modeling of compressible viscous turbulent flowsinturbomachinery", In book: Aerodynamics: Problems and Perspectives, National AerospaceUniversity"KhAI",Kharkov,2004,pp.134–157 (In Russian).
Solodov, V.G., (2011), Turbulent flow modeling. Large eddy simulation, Publishing house KhNAHU, Kharkov, 168 p.
Migai V. K., Gudkov E. I. (1981), Design and calculation of output diffusers of turbomachines. Machinоstroenie, Leningrad.