A Computational Study of Gas-Dynamic Parameters of Radial-Axial Turbines and Their Joint Operation with Piston Engines
Authors: Rusakov A.N. | Published: 26.08.2020 |
Published in issue: #8(725)/2020 | |
Category: Energy and Electrical Engineering | Chapter: Turbomachines and Combination Turbine Plants | |
Keywords: centripetal turbines, turbine characteristics, turbine efficiency, geometrical parameters, pulse turbine, four-stroke piston engine |
Radial-axial (centripetal) turbines are widely used in various fields of industry, energy and transport, but their characteristics require improvement, above all increasing the efficiency factor. A differential iterative calculation method is used to calculate the gas dynamic parameters and characteristics of centripetal turbines. The joint operation of a pulsed centripetal turbine and a four-stroke piston engine is examined. The efficiency of the centripetal turbine is strongly dependent on the combination of the turbine’s and piston engine’s geometric features. The study examines the influence of the rotor blades curvature, the ratio of the height of the impeller blades at the outlet to the height of the blades at the entrance, and the number of blades of the impeller and the nozzle device on the turbine efficiency. An approach to the selection of the optimal geometric parameters that provide the highest efficiency of the designed centripetal turbine when it is used jointly with a four-stroke piston engine is proposed.
References
[1] Boyce Meherwan P. Gas Turbine Engineering Handbook. Houston, Butterworth-Heinemann, 2001. 799 p.
[2] Samarskiy A.A. Vvedeniye v chislennyye metody [Introduction to Numerical Methods]. Sankt-Petersburg, Lan’ publ., 2005. 271 p.
[3] Chernyak V.G., Suyetin P.E. Mekhanika sploshnykh sred [Continuum mechanics]. Moscow, Fizmatlit publ., 2006. 352 p.
[4] Cohen H., Rogers G.F.C., Saravanamuttoo H.I.H. Gas Turbine Theory. Longman, Harlow, T.J. Press, 1996. 442 p.
[5] Sherstyuk A.N., Zaryankin A.E. Radial’no-osevyye turbiny maloy moshchnosti [Low Power Radial-Axial Turbines]. Moscow, Mashinostroyeniye publ., 1976. 207 p.
[6] Takao M., Setoguchi T. Air turbines for wave energy conversion. International Journal of Rotating Machinery, 2012, vol. 12, no. 717398, doi: 10.1155/2012/717398
[7] Dovgyallo A.I., Shimanov A.A. Possibility of using a bi-directional impulse turbine in a thermo-acoustic engine. Vestnik of Samara University. Aerospace and Mechanical Engineering, 2015, vol. 14, no. 1, pp. 132–138 (in Russ.).
[8] Takao M., Fujioka Y., Homma H., Kim T.-W., Setoguchi T. Experimental Study of a Radial Turbine Using Pitch -Controlled Guide Vanes for Wave Power Conversion. International Journal of Rotating Machinery, 2006, vol. 2006, no. 17379, doi: 10.1155/IJRM/2006/17379
[9] Motorin A.V., Raspopov I.V., Fursov I.D. Parovyye turbiny [Steam turbines]. Barnaul, AltSTU publ., 2004. 127 p.
[10] Kostyuk A.G., Frolov V.V., Bulkin A.E., Trukhniy A.D. Parovyye i gazovyye turbiny dlya elektrostantsiy [Steam and gas turbines for power plants]. Moscow, MPEI publ., 2016. 557 p.
[11] Li P.-Y., Gu C.-W., Song Y. A new optimization method for centrifugal compressors based on 1D calculations and analyses. Energies, 2015, vol. 8(5), pp. 4317–4334, doi: 10.3390/en8054317
[12] Mitrokhin V.T. Vybor parametrov i rasch?t radial’noy tsentrostremitel’noy turbiny na statsionarnykh i perekhodnykh rezhimakh [Parameter selection and calculation of a centripetal radial turbine in stationary and transient conditions]. Moscow, Mashinostroyeniye publ., 1974. 228 p.
[13] Rangwala A.S. Turbo-machinery dynamics. McGraw-Hill Companies, 2005. 535 p.
[14] Tarnawski P., Ostapski W. Pulse powered turbine engine concept — numerical analysis of influence of different valve timing concepts on thermodynamic performance. Bulletin of the Polish Academy of Sciences: Technical Sciences, 2018, vol. 66, no. 3, pp. 373–382, doi: 10.24425/123444
[15] Teoriya porshnevykh i kombinirovannykh dvigateley [Theory of piston and combined engines]. Ed. Orlin A.S., Kruglov M.G. Moscow, Mashinostroyeniye publ., 1983. 372 p.