The Application of Feature Mapping in Model Transformation of Turbine blade

被引：0
作者：
Cheng, Rong [1 ]
机构：
[1] Shaanxi Radio Broadcasting & Televis Univ, Xian 710068, Shaanxi, Peoples R China
来源：
INFORMATION TECHNOLOGY FOR MANUFACTURING SYSTEMS, PTS 1 AND 2 | 2010年
关键词：
Model Transformation; Turbine Blade; Feature Mapping; Investment Casting Mold;
D O I：
10.4028/www.scientific.net/AMM.20-23.898
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
A transformation technology for part model to blank model based on feature mapping of turbine blade was prompted to improve the design efficiency of investment casting mold. The definition, feature presentation and feature mapping theory were researched. The feature and the geometry structure of turbine blade's part mold, blank model and cavity mold were analyzed, and the feature mapping technology was prompted. At last, a mold transformation system was developed based on UG. Experiment result shows that with the help of this system, designers can improve design efficiency of investment casting mold of turbine blade.
引用
收藏
页码：898 / 904
页数：7
相关论文
共 50 条
[31]   CONSTRUCTING SECTION PROFILE CURVE OF TURBINE BLADE [J].
Liu, Yuan-Peng ;
Zhao, Song ;
Dong, Xiao-Yan .
PROCEEDINGS OF THE 2010 INTERNATIONAL CONFERENCE ON WAVELET ANALYSIS AND PATTERN RECOGNITION, 2010, :211-215
[32]   Calculation of the VKI turbine blade with LES and DES [J].
Magagnato, F. ;
Pritz, B. ;
Gabi, M. .
JOURNAL OF THERMAL SCIENCE, 2007, 16 (04) :321-327
[33]   Rapid modeling of impingement pipe in turbine blade [J].
Li J. ;
Xi P. .
Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2016, 42 (06) :1149-1155
[34]   Calculation of the VKI turbine blade with LES and DES [J].
F.Magagnato ;
B.Pritz ;
M.Gabi .
JournalofThermalScience, 2007, (04) :321-327
[35]   Turbine blade failure in a thermal power plant [J].
Das, G ;
Chowdhury, SG ;
Ray, AK ;
Das, SK ;
Bhattacharya, DK .
ENGINEERING FAILURE ANALYSIS, 2003, 10 (01) :85-91
[36]   Influence of milling toolpaths in machining of the turbine blade [J].
Jarolmasjed, Seyedamin ;
Davoodi, Behnam ;
Alamdari, Babak Pourebrahim .
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2019, 91 (10) :1327-1339
[37]   Analysis of the fracture of a turbine blade on a turbojet engine [J].
Song, Kyo-Soo ;
Kim, Seon-Gab ;
Jung, Daehan ;
Hwang, Young-Ha .
ENGINEERING FAILURE ANALYSIS, 2007, 14 (05) :877-883
[38]   Calculation of the VKI turbine blade with LES and DES [J].
F. Magagnato ;
B. Pritz ;
M. Gabi .
Journal of Thermal Science, 2007, 16 :321-327
[39]   Research on modeling turbine blade in reverse engineering [J].
Zhang, Lining ;
Zhang, Dinghua ;
Liu, Yuanpeng .
ADVANCES IN MATERIALS MANUFACTURING SCIENCE AND TECHNOLOGY II, 2006, 532-533 :777-+
[40]   Aero-engine turbine blade life assessment using the Neu/Sehitoglu damage model [J].
Abu, Abdullahi O. ;
Eshati, Samir ;
Laskaridis, Panagiotis ;
Singh, Riti .
INTERNATIONAL JOURNAL OF FATIGUE, 2014, 61 :160-169
12345