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All articles by "Troitskiy N.I."
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 |
Analysis of Physical Processes in the Flow Parts of Gas Turbines with Different Blade Chords
Authors: Molyakov V.D., Kunikeev B.A., Troitskiy N.I. | Published: 28.06.2021 |
Published in issue: #7(736)/2021 | |
Category: Energy and Electrical Engineering | Chapter: Heat Engines | |
Keywords: gas turbine, blade chords, relative elongation of the blades, сhanging geometry of channels, flow parameter restructuring |
The Efficiency of Closed-Cycle Gas Turbines Controlled by Different Methods and Programs
Authors: Molyakov V.D., Kunikeev B.A., Troitskiy N.I. | Published: 05.03.2020 |
Published in issue: #3(720)/2020 | |
Category: Energy and Electrical Engineering | Chapter: Turbomachines and Combination Turbine Plants | |
Keywords: closed gas turbine unit, CGTU control, control method, control program, gas-dynamic similarity in CGTU nodes, change in gas pressure upstream |
The Influence of the Open Axial Clearance on the Gas Flow and Energy Losses in the Turbine Stage with a Shroud on Working Blades
Authors: Molyakov V.D., Kunikeev B.A., Troitskiy N.I. | Published: 08.10.2018 |
Published in issue: #9(702)/2018 | |
Category: Energy and Electrical Engineering | Chapter: Turbomachines and Combination Turbine Plants | |
Keywords: turbine stage, turbine flow passage, closed axial clearance, open axial clearance, peritricha, rotor blades bandage |
Design Features of the Power Turbine Stage of the Transport Gas Turbine Engine with Variable-Area Nozzles
Authors: Troitskiy N.I., Molyakov V.D., Aseikina M.V. | Published: 04.03.2016 |
Published in issue: #3(672)/2016 | |
Category: Transportation and Power Engineering | |
Keywords: design law, gas turbine, turbine stage, variable nozzle assembly, profiling law, reaction degree, losses |