Heat transfer, thermal stress and failure analyses in a TiB2 gas turbine stator blade

被引:83
作者
Vaferi, Kourosh [1 ]
Nekahi, Sahar [1 ]
Vajdi, Mohammad [1 ]
Moghanlou, Farhad Sadegh [1 ]
Shokouhimehr, Mohammadreza [2 ]
Motallebzadeh, Amir [3 ]
Sha, Jianjun [4 ]
Asl, Mehdi Shahedi [1 ]
机构
[1] Univ Mohaghegh Ardabili, Dept Mech Engn, Ardebil, Iran
[2] Seoul Natl Univ, Dept Mat Sci & Engn, Res Inst Adv Mat, Seoul 08826, South Korea
[3] Koc Univ Surface Sci & Technol Ctr KUYTAM, TR-34450 Istanbul, Turkey
[4] Dalian Univ Technol, State Key Lab Struct Anal Ind Equipment, Dalian 116024, Peoples R China
关键词
Titanium diboride; Principle stresses; Gas turbine blade; Brittle material; Coulomb-Mohr theory; GRAPHITE NANO-FLAKES; MECHANICAL-PROPERTIES; FRACTOGRAPHICAL CHARACTERIZATION; MICROSTRUCTURAL DEVELOPMENT; PARTICLE-SIZE; PLASMA; COMPOSITES; TEMPERATURE; ZRB2; DENSIFICATION;
D O I
10.1016/j.ceramint.2019.06.184
中图分类号
TQ174 [陶瓷工业]; TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
Gas turbine stator blades do not experience centrifugal force contrary to the rotor blades; but they are exposed to high-temperature combustion gases causing thermal stresses. In the present work, a series of numerical simulations were carried out to clarify the feasibility of TiB2 utilization as an appropriate material for gas turbine stator blades. The governing equations of heat transfer and solid mechanics were discretized by the finite element method and solved using Comsol Multiphysics software. The boundary conditions were applied, and temperature, displacement and maximum principle stress were obtained. The results showed that using ceramics such as TiB2 instead of conventional alloys can enhance the maximum displacement. Temperature distribution in the blade is more uniform than that of alloys, and consequently, the thermal stresses are reduced. The TiB2 can withstand the applied stresses according to the Coulomb-Mohr theory with a safety factor of 2.4.
引用
收藏
页码:19331 / 19339
页数:9
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