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Review of Advanced Effusive Cooling for Gas Turbine Blades
Turbine inlet temperature has continuously increased to improve gas turbine performance during the past few decades. Although internal convection cooling and traditional film cooling have contributed significantly to the current achievement, advanced ...
Wen Wang +3 more
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A Numerical Study on the Cooling Efficiency of the Gas Turbine Vane with the Film Cooling Hole Shape [PDF]
Research on advanced cooling system design is significant in achieving a high turbine inlet temperature in the gas turbine industry. The higher turbine inlet temperature of the gas turbine increases thermal efficiency. However, it also aggravates the gas
Jaehun Choi, Hwabhin Kwon, Heesung Park
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Effect of Vane Thermal Emission Cooling on the Efficiency of the Gas Turbine Power Plant [PDF]
The work is devoted to the problem of increasing efficiency of power gas turbine units (microturbines). One of ways to improve efficiency is to increase gas temperature in front of the turbine. Cooling of gas turbine elements is difficult.
Kolychev A.V. +3 more
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Development Trend of Cooling Technology for Turbine Blades at Super-High Temperature of above 2000 K
Aeroengines and heavy-duty gas turbines are the core power equipment in the field of national defense and energy. Their research and development (R&D) level and manufacturing level represent the status of a country’s heavy industry in the world.
Liang Xu +5 more
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A thermoelastohydrodynamic (TEHD) coupling model is developed to study the static performance of a heavy-duty tilting pad thrust bearing (TPTB) under the effect of axis misalignment.
Binbin Liu +5 more
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Experimental Investigation of the Exhaust Device of Turbocharger for Marine Engines [PDF]
In order to reduce the temperature in the marine engine cabin, improve the working environment of the staff and meet the economy and emission requirements, the cooling system of the engine was experimentally investigated in the present study.
S. Li +6 more
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Turbine nozzle blocks were tested and, as a result, problems of nozzle block lower platform alligatoring were detected. In the course of the research possible variants of cooling high pressure turbine nozzle block vane platforms were investigated ...
Yu. G. Gorelov +2 more
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Several studies have previously been conducted to improve the cooling performance of film cooling. However, most of the research has conducted experiments with film cooling holes on flat plates, and thus, the results of these studies do not encompass the
Seokmin Kim +3 more
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Cooling Process of Gas Turbine Blade: A Comparison Study
The gas turbine engines are occupied an important sector in the energy production and aviation industry and this important increase day after day for their features.
Akram Luabi a, Naseer Hamza a
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Improvements in the efficiency of gas turbine engines over the decades have led to increasing turbine inlet temperatures. This, in turn, has resulted in the need to cool the turbine blades themselves to avoid damage to them.
Zhao Wang, Ali Turan, Timothy Craft
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