Enhancing the Trailing-Edge Cooling Performance of Gas Turbine Blade Using Cylindrical Pin-Fins Cooling

被引：0
|
作者：
Effendy, Marwan [1 ]
机构：
[1] Univ Muhammadiyah Surakarta, Fac Engn, Dept Mech Engn, Jl Ahmad Yani, Pabelan 57102, Surakarta, Indonesia
来源：
ADVANCED SCIENCE LETTERS | 2018年 / 24卷 / 12期
关键词：
Trailing-Edge Cutback; Film Cooling Effectiveness; Cylindrical Pin Fins Cooling; DETACHED-EDDY SIMULATION; CUTBACK;
D O I：
10.1166/asl.2018.12081
中图分类号：
O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];
学科分类号：
07 ; 0710 ; 09 ;
摘要：
One of the important aspects on design the cooling system of gas turbine blade is the configuration inside the cooling passage as the coolant exit-slot before mixing process with the main hot gas. This paper presents the mixing characteristic between the mainstream flow and the coolant over the trailing-edge surface of gas turbine blade due to the existence of pin-fin cooling compared to the empty duct. This research was numerically performed by Detached Eddy Simulation (DES) based on SST k-omega, turbulence model. The results show that the blade trailing-edge (TE) cutback cooling can be improved by installing the cylindrical pin-fin cooling. The film-cooling effectiveness increases up to 19 percent by the existence of pin-fin cooling.
引用
收藏
页码：9049 / 9053
页数：5
相关论文
共 50 条
  • [1] Effect of the multiple rows of pin-fins on the cooling performance of cutback trailing-edge
    Ye, Lin
    Liu, Cun-liang
    Zhang, Fan
    Li, Ji-chen
    Zhou, Tian-liang
    [J]. INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2021, 170
  • [2] EXPLORING THE EFFECTS OF PIN-FINS IN A GAS TURBINE BLADE INTERNAL COOLING CHANNEL
    Nourin, Farah Nazifa
    Amano, Ryoichi S.
    [J]. PROCEEDINGS OF ASME TURBO EXPO 2023: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2023, VOL 7B, 2023,
  • [3] Lower pressure drop turbine blade trailing-edge cooling configuration
    Grazieli Luiza Costa Carosio
    Marcio Teixeira de Mendonca
    [J]. Journal of the Brazilian Society of Mechanical Sciences and Engineering, 2015, 37 : 1217 - 1233
  • [4] Lower pressure drop turbine blade trailing-edge cooling configuration
    Costa Carosio, Grazieli Luiza
    de Mendonca, Marcio Teixeira
    [J]. JOURNAL OF THE BRAZILIAN SOCIETY OF MECHANICAL SCIENCES AND ENGINEERING, 2015, 37 (04) : 1217 - 1233
  • [5] Trailing-edge cooling for gas turbines
    Cunha, FJ
    Chyu, MK
    [J]. JOURNAL OF PROPULSION AND POWER, 2006, 22 (02) : 286 - 300
  • [6] Effects of pin-fins with trapezoidal endwall on heat transfer characteristics in gas turbine blade internal cooling channels
    Cong-Truong Dinh
    Khanh-Duy Cong Do
    Duy-Hung Chung
    Hoanh-Son Truong
    [J]. Journal of Mechanical Science and Technology, 2023, 37 : 2199 - 2210
  • [7] Effects of pin-fins with trapezoidal endwall on heat transfer characteristics in gas turbine blade internal cooling channels
    Dinh, Cong-Truong
    Do, Khanh-Duy Cong
    Chung, Duy-Hung
    Truong, Hoanh-Son
    [J]. JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY, 2023, 37 (05) : 2199 - 2210
  • [8] Simulation of Turbine Blade Trailing Edge Cooling
    Joo, Jongwook
    Durbin, Paul
    [J]. JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2009, 131 (02): : 0211021 - 02110214
  • [9] COMPUTATIONAL ANALYSIS OF TRAILING EDGE INTERNAL COOLING OF A GAS TURBINE BLADE WITH PIN-FIN ARRAYS
    Moon, Mi-Ae
    Kim, Kwang-Yong
    [J]. JOURNAL OF ENHANCED HEAT TRANSFER, 2013, 20 (02) : 137 - 151
  • [10] Detached-Eddy Simulation of Trailing-Edge (TE) Cutback Turbine Blade Cooling
    Effendy, Marwan
    Yao, Yufeng
    Marchant, Denis R.
    [J]. 8TH INTERNATIONAL CONFERENCE ON MECHANICAL AND MANUFACTURING ENGINEERING 2017 (ICME'17), 2017, 135
12345