Prototyping and Study of Mesh Turbomachinery Based on the Euler Turbine
Author:
Sazonov Yuri Appolonievich,Mokhov Mikhail Albertovich,Gryaznova Inna Vladimirovna,Voronova Victoria Vasilievna,Mulenko Vladimir Valentinovich,Tumanyan Khoren Arturovich,Frankov Mikhail Alexandrovich,Balaka Nikolay Nikolaevich
Abstract
This paper presents a scientific development aimed at improving the efficiency of turbomachines through the joint use of rotary-vane and vortex workflows. In the well-known Euler turbine, the rotor flow channels represent a set of curved pipes. The authors propose to consider in more detail the possibilities of using such rotating pipes in the implementation of an ejection (vortex) workflow. A hybrid pump was considered with the conclusion that its workflow can be described using two Euler equations. The results of computer simulation indicate that hybrid turbomachines are promising. The use of additive technology allowed the creation of micromodels of the Euler turbine with various rotor designs. Laboratory hydraulic tests showed that the liquid inlet to the rotor is possible in pulse mode. Laboratory tests of micromodels using compressed air showed that gas (or liquid) motion through curved pipes could be carried out from the rotor periphery to its center and then back, albeit through another curved pipe. The research results demonstrated that the scientific and technical potential of the Euler turbine is not yet fully unlocked, and research in this direction should continue. The study results are applicable in various industries including the energyeconomy, robotics, aviation, and water transport industries.
Funder
Ministry of Education and Science of the Russian Federation
Subject
Energy (miscellaneous),Energy Engineering and Power Technology,Renewable Energy, Sustainability and the Environment,Electrical and Electronic Engineering,Control and Optimization,Engineering (miscellaneous)
Reference56 articles.
1. PROTOTYPING MESH TURBINE WITH THE JET CONTROL SYSTEM
2. Fundamentals of Calculation and Design of Pump-Ejector Installations;Sazonov,2012
3. Calculation of the minimum drag of lattice wings and their elements and comparison of the calculated results with the experiment at M = 0.6 ÷ 4.0;Konovalova;Air Fleet Tech.,2005
4. Method of determining the full-scale aerodynamic performance of an airplane with lattice wings based on the results of its model wind-channel tests;Drozdov;TsAGI Sci. J.,2002
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