A software tool for parametric design of turbomachinery blades

被引:51
|
作者
Koini, Georgia N. [1 ]
Sarakinos, Sotirios S. [1 ]
Nikolos, Ioannis K. [1 ]
机构
[1] Tech Univ Crete, Dept Prod Engn & Management, GR-73100 Kounoupidiana, Chania, Greece
关键词
Turbomachinery design; Blade definition; Parametric design; NURBS; CASCADES;
D O I
10.1016/j.advengsoft.2008.03.008
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
This paper presents a software tool for the conceptual design of turbomachinery bladings named "T4T" (Tools for Turbomachinery). It provides the ability to interactively construct parametric 3D blade rows of various types, including for multistage machines. The design procedure is parametric and a variety of different rotating machinery components may be produced. The design parameters used for the blades as well as the hub and shroud surfaces construction correspond to 2D sections. However, the resulting geometries are modeled as NURBS 3D surfaces and can be imported to other CAD or analysis software via standard exchange protocols. The geometry definition is empowered by the object oriented structure of the software and an easy-to-use graphical interface, which makes the design phase a straightforward procedure. The software's structure and geometric algorithms, the blading design procedure, along with sample designs which demonstrate the capabilities of the software, are presented in this paper. (C) 2008 Elsevier Ltd. All rights reserved.
引用
收藏
页码:41 / 51
页数:11
相关论文
共 50 条
  • [1] Parametric design of turbomachinery blades
    Koini, GN
    Sarakinos, SS
    Nikolos, IK
    Eurocon 2005: The International Conference on Computer as a Tool, Vol 1 and 2 , Proceedings, 2005, : 539 - 542
  • [2] Versatile Tool for Parametric Smooth Turbomachinery Blades
    Siddappaji, Kiran
    Turner, Mark G.
    AEROSPACE, 2022, 9 (09)
  • [3] Design of the optimal blades for the axial turbomachinery
    Matijasevic, B
    Guzovic, Z
    Novko, I
    PROCEEDINGS OF THE 5TH INTERNATIONAL DESIGN CONFERENCE DESIGN 98, 1998, : 451 - 460
  • [4] Study on Aerodynamic Design Optimization of Turbomachinery Blades
    Naixing CHEN Hongwu ZHANG Weiguang HUANG YanjiXU Institute of Engineering Thermophysics
    Journal of Thermal Science, 2005, (04) : 298 - 304
  • [5] Multiobjective optimization approach to turbomachinery blades design
    Li Jun
    Li Guojun
    Feng Zhenping
    Liu Lijun
    Proceedings of the ASME Turbo Expo 2005, Vol 6, Pts A and B, 2005, : 1051 - 1058
  • [6] Study on Aerodynamic Design Optimization of Turbomachinery Blades
    Chen, Naixing
    Zhang, Hongwu
    Huang, Weiguang
    Xu, Yanji
    JOURNAL OF THERMAL SCIENCE, 2005, 14 (04) : 298 - U105
  • [7] GENERAL CAPABILITY OF PARAMETRIC 3D BLADE DESIGN TOOL FOR TURBOMACHINERY
    Siddappaji, Kiran
    Turner, Mark G.
    Merchant, Ali
    PROCEEDINGS OF THE ASME TURBO EXPO 2012, VOL 8, PTS A-C, 2012, : 2331 - 2344
  • [8] Study on aerodynamic design optimization of turbomachinery blades
    Naixing Chen
    Hongwu Zhang
    Weiguang Huang
    Yanji Xu
    Journal of Thermal Science, 2005, 14 : 298 - 304
  • [9] Inverse problem in aerodynamic shape design of turbomachinery blades
    Li, Yingchen
    Yang, Dianliang
    Feng, Zhenping
    Proceedings of the ASME Turbo Expo 2006, Vol 6, Pts A and B, 2006, : 1535 - 1543
  • [10] Multiple objective optimization and inverse design of axial turbomachinery blades
    Larocca, Francesco
    JOURNAL OF PROPULSION AND POWER, 2008, 24 (05) : 1093 - 1099