Effects of the Coordinates Planes Crystal Orientation on the Structural Strength of Single-Crystal Turbine Vanes and Blades
スポンサーリンク
概要
- 論文の詳細を見る
The effects of crystal orientation (θ) on the structural strength of single crystal turbine vanes and blades calculated with the finite element method (FEM) are discussed in this paper. TMS-75, a 3rd generation single-crystal Ni-base superalloy, is chosen as the model material for turbine vanes and blades. It became clear that, (1) the elastic constant matrix changes were equivalence for each of three coordinate due to the orientation variation (0° < θ < 90°), and the strength of the turbine vane and blade were strongly related to θ, and also depended on the load and model shape. (2) The strength dependence of the turbine vane on the crystal orientation was depended on coordinate plane: there are lower Mises stress in XY plane and maximum Mises stress in near the θ=45° at both YZ and ZX Planes. (3) In the case of a blade, the influence is similar to the vane on blade tip, but the converse holds for the blade root. It is clear that the creep rupture time can be extended, when the <100> crystallographic axes is the Y or X axis of the blade under higher rotation speed.
著者
-
Matsushita Masahiro
Aeronautical Envi. Tech. Center Japan Aerospace Exploration Agency
-
Osawa Makoto
Materials Eng. Lab. High Temperature Materials Group National Inst. For Materials Sci.
-
HARADA Hiroshi
Materials Eng. Lab., High Temperature Materials Group, National Inst. for Materials Sci.
-
Chen Jinxiang
Aeronautical Envi. Tech. Center Japan Aerospace Exploration Agency
-
Yokokawa Tadaharu
Materials Eng. Lab. High Temperature Materials Group National Inst. For Materials Sci.
-
Hashimoto Ryosaku
Aeronautical Envi. Tech. Center Japan Aerospace Exploration Agency
-
Fukuyama Yoshitaka
Aeronautical Envi. Tech. Center Japan Aerospace Exploration Agency
-
OGAWA Akinori
Aeronautical Environment technology Center, Japan Aerospace Exploration Agency
-
FUKUYAMA Yoshitaka
Aeronautical Environment technology Center, Japan Aerospace Exploration Agency
-
OSAWA Makoto
Materials Engineering laboratory, High Temperature Materials Group, National Institute for Materials Science
-
HARADA Hiroshi
Materials Engineering laboratory, High Temperature Materials Group, National Institute for Materials Science
関連論文
- Effects of the Coordinates Planes Crystal Orientation on the Structural Strength of Single-Crystal Turbine Vanes and Blades
- Effects of the Cross-Sectional In-Plane Crystal Orientation on the Structural Strength of Single-Crystal Turbine Vanes
- Thermal-Mechanical Fatigue Property of Ni-Base Single Crystal Superalloys TMS-82+ and TMS-75