Optimization Design of Lattice Structures in Internal Cooling Channel with Variable Aspect Ratio of Gas Turbine Blade

被引:18
|
作者
Xu, Liang [1 ]
Ruan, Qicheng [1 ]
Shen, Qingyun [1 ]
Xi, Lei [1 ]
Gao, Jianmin [1 ]
Li, Yunlong [1 ]
机构
[1] Xi An Jiao Tong Univ, State Key Lab Mech Mfg Syst Engn, Xian 710049, Peoples R China
基金
国家重点研发计划; 中国国家自然科学基金;
关键词
lattice structure; internal cooling channel; heat transfer; mechanical performances; integral optimization model; HEAT-TRANSFER CHARACTERISTICS; FLUID-FLOW; SANDWICH PANEL; TRANSFER ENHANCEMENT; METALLIC LATTICE; TRUSS CORE; X-LATTICE; PIN FINS; PERFORMANCE; TOPOLOGY;
D O I
10.3390/en14133954
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
Traditional cooling structures in gas turbines greatly improve the high temperature resistance of turbine blades; however, few cooling structures concern both heat transfer and mechanical performances. A lattice structure (LS) can solve this issue because of its advantages of being lightweight and having high porosity and strength. Although the topology of LS is complex, it can be manufactured with metal 3D printing technology in the future. In this study, an integral optimization model concerning both heat transfer and mechanical performances was presented to design the LS cooling channel with a variable aspect ratio in gas turbine blades. Firstly, some internal cooling channels with the thin walls were built up and a simple raw of five LS cores was taken as an insert or a turbulator in these cooling channels. Secondly, relations between geometric variables (height (H), diameter (D) and inclination angle(omega)) and objectives/functions of this research, including the first-order natural frequency (freq1), equivalent elastic modulus (E), relative density ((rho) over bar) and Nusselt number (Nu), were established for a pyramid-type lattice structure (PLS) and Kagome-type lattice structure (KLS). Finally, the ISIGHT platform was introduced to construct the frame of the integral optimization model. Two selected optimization problems (Op-I and Op-II) were solved based on the third-order response model with an accuracy of more than 0.97, and optimization results were analyzed. The results showed that the change of Nu and freq1 had the highest overall sensitivity Op-I and Op-II, respectively, and the change of D and H had the highest single sensitivity for Nu and freq1, respectively. Compared to the initial LS, the LS of Op-I increased Nu and E by 24.1% and 29.8%, respectively, and decreased (rho) over bar by 71%; the LS of Op-II increased Nu and E by 30.8% and 45.2%, respectively, and slightly increased (rho) over bar; the LS of both Op-I and Op-II decreased freq1 by 27.9% and 19.3%, respectively. These results suggested that the heat transfer, load bearing and lightweight performances of the LS were greatly improved by the optimization model (except for the lightweight performance for the optimal LS of Op-II, which became slightly worse), while it failed to improve vibration performance of the optimal LS.
引用
收藏
页数:27
相关论文
共 50 条
  • [41] Heat transfer characteristics of an internal cooling channel with pin- fins and ribbed endwalls in gas turbine blade
    Co, Vu T. A.
    Hoang, Hung C.
    Do, Duy C. K.
    Truong, Son H.
    Pham, Diem G.
    Le, Nhung T. T.
    Dinh, Truong C.
    Nh, Linh T.
    ADVANCES IN AIRCRAFT AND SPACECRAFT SCIENCE, 2024, 11 (02): : 153 - 175
  • [42] Flow and Heat Transfer Characteristics of the Turbine Blade Variable Cross-Section Internal Cooling Channel with Turning Vane
    Xu, Tao
    Shi, Dongbo
    Zhang, Di
    Xie, Yonghui
    APPLIED SCIENCES-BASEL, 2023, 13 (03):
  • [43] Effect of Rotation on a Gas Turbine Blade Internal Cooling System: Experimental Investigation
    Massini, Daniele
    Burberi, Emanuele
    Carcasci, Carlo
    Cocchi, Lorenzo
    Facchini, Bruno
    Armellini, Alessandro
    Casarsa, Luca
    Furlani, Luca
    JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2017, 139 (10):
  • [44] EFFECT OF ROTATION ON A GAS TURBINE BLADE INTERNAL COOLING SYSTEM: EXPERIMENTAL INVESTIGATION
    Massini, Daniele
    Burberi, Emanuele
    Carcasci, Carlo
    Cocchi, Lorenzo
    Facchini, Bruno
    Armellini, Alessandro
    Casarsa, Luca
    Furlani, Luca
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2016, VOL 5B, 2016,
  • [45] EFFECT OF ROTATION ON A GAS TURBINE BLADE INTERNAL COOLING SYSTEM: NUMERICAL INVESTIGATION
    Burberi, E.
    Massini, D.
    Cocchi, L.
    Mazzei, L.
    Andreini, A.
    Facchini, B.
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2016, VOL 5B, 2016,
  • [46] Effect of Rotation on a Gas Turbine Blade Internal Cooling System: Numerical Investigation
    Burberi, E.
    Massini, D.
    Cocchi, L.
    Mazzei, L.
    Andreini, A.
    Facchini, B.
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2017, 139 (03):
  • [47] Study of design and technology factors influencing gas turbine blade cooling
    Shevchenko, I. V.
    Garanin, I. V.
    Rogalev, A. N.
    Kindra, V. O.
    Khudyakova, V. P.
    INTERNATIONAL CONFERENCE PROBLEMS OF THERMAL PHYSICS AND POWER ENGINEERING (PTPPE-2017), 2017, 891
  • [48] A conjugate BEM optimization algorithm for the design of turbine blade cooling channels
    Nordlund, RS
    Kassab, AJ
    BOUNDARY ELEMENT TECHNOLOGY XI, 1996, : 237 - 246
  • [49] Exploring the Effects of Guide Vane on Dimpled Cooling Channel of Gas Turbine Blade
    Nourin, Farah Nazifa
    Blum, Brinn Leighton
    Amano, Ryoichi S.
    JOURNAL OF ENERGY RESOURCES TECHNOLOGY-TRANSACTIONS OF THE ASME, 2023, 145 (05):
  • [50] COOLING STRUCTURE OPTIMIZATION FOR A RIB-ROUGHED CHANNEL IN A TURBINE ROTOR BLADE
    Chi, Zhongran
    Ren, Jing
    Jiang, Hongde
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2013, VOL 3B, 2013,