Experimental Study of Power Turbine with Adjustable Nozzle Guide Vanes
Authors: Troitskiy N.I., Molyakov V.D. | Published: 06.07.2021 |
Published in issue: #8(737)/2021 | |
Category: Energy and Electrical Engineering | Chapter: Heat Engines | |
Keywords: power turbine, adjustable nozzle guide vanes, law of profiling, parameters along the stage height, degree of reactivity, efficiency |
The article discusses the results of experimental research of the impact of the law of profiling along the stage height on the characteristics of a turbine with an adjustable nozzle guide vanes. The results of the design study have been confirmed, taking into account meridional streamline bending. It is shown that in the stage profiled according to the law of constancy of the product of the radius of the flow path and the tangent of the blade angle the degree of reactivity in the root sections of the blades increases provided that the degree of reactivity at the middle diameter is the same as in a turbine with a constant blade angle, which leads to an increase in the turbine efficiency in modes with a reduced angle of arrangement of blades of the adjustable nozzle guide vanes and the degree of pressure reduction.
References
[1] Varaksin A.Yu., ed. Teoriya i proektirovanie gazoturbinnykh i kombinirovannykh ustanovok [Theory and design of gas turbine and combined plants]. Moscow, Bauman MSTU Publ., 2017. 640 с. (In Russ.).
[2] Konyukov V.L. Effect of blades rotation angle in regulated nozzle of charging-turbine set on parameters of gas in front of a turbine. Vestnik Kerchenskogo Gosudarstvennogo morskogo tekhnologicheskogo universiteta [Bulletin of the Kerch State Marine Technological University], 2019, no. 2, pp. 54–64. URL: https://www.ejkgmtu.ru/?p=22262 (in Russ.).
[3] Popov N.S., Izotov S.P., eds. Transportnye mashiny s gazoturbinnymi dvigatelyami [Transport machines with gas-turbine engines]. Leningrad, Mashinostroenie Publ., 1987 (in Russ.).
[4] Troitskiy N.I., Molyakov V.D., Aseykina M.V. Design features of the power turbine stage of the transport gas turbine engine with variable-area nozzles. Izvestiya vysshikh uchebnykh zavedeniy. Mashinostroenie [Proceedings of Higher Educational Institutions. Machine Building], 2016, no. 3, pp. 30–38, doi: http://dx.doi.org/10.18698/0536-1044-2016-3-30-38 (in Russ.).
[5] Revzin S., Komarov O.V., Rozhkov A.V. Providing variable operating regimes for engine with regulated power turbine and blocked gas turbine engines. Gazoturbinnye tekhnologii, 2005, no. 2, pp. 32–34 (in Russ.).
[6] Emel’yanov N.E., Karyshev A.K. Special aspects of using regulated nozzle set in power turbine of gas-turbine plant. Aktual’nye problemy gumanitarnykh i estestvennykh nauk, 2017, no. 3-3, pp. 48–51 (in Russ.).
[7] Emel’yanov N.E., Karyshev A.K. Computational theoretical study on efficiency of using regulated nozzle set in power turbine of gas pumping unit. Aktual’nye problemy gumanitarnykh i estestvennykh nauk, 2017, no. 3-3, pp. 51–55 (in Russ.).
[8] Kryukov A.A. 3D gas-dynamic calculation of nozzle set for low-emission inflow turbine. Vestnik Astrakhanskogo gosudarstvennogo tekhnicheskogo universiteta. Ser. Morskaya tekhnika i tekhnologiya [Vestnik of Astrakhan State Technical University. Ser. Marine Engineering and Technologies], 2019, no. 4, pp. 89–95 (in Russ.).
[9] Eliseev Yu., Belyaev V. New application of forces. Dvigatel’, 2000, no. 4, pp. 16–18 (in Russ.).
[10] Eliseev Yu., Belyaev V., Sinkevich M. Development conception for 6RS gas turbine engine. Dvigatel’, 2001, no. 3, pp. 38–41 (in Russ.).
[11] Brodov Yu.M., Komarov O.V., Blinov V.L., et al. Technical performance estimation method for gas turbines with variable flow path geometry. Izvestiya vysshikh uchebnykh zavedeniy. Problemy energetiki [Power Engineering: Research, Equipment, Technology], 2016, no. 3-4, pp. 68–76. (In Russ.).