TY - GEN
T1 - Parameter extraction of featured section in turbine blade inspection
AU - Chen, Lei
AU - Li, Bing
AU - Jiang, Zhuangde
AU - Ding, Jianjun
AU - Zhang, Fei
PY - 2010
Y1 - 2010
N2 - As a widely used part in turbomachinery, the inspection of free-form shaped turbine blade is a very critical and tough work. Based on the parameter evaluation idea, the aim of this study is to develop methods for extracting key parameters of a turbine blade, which is probably the most important in the whole inspection process. After analyzing the definition, new extraction methods of several section parameters are presented in this paper, including chord length, leading/trailing edge and twist of airfoil surface. The proposed algorithms are developed and implemented using C++ language and OpenGL. Some case studies are investigated to validate the approach.
AB - As a widely used part in turbomachinery, the inspection of free-form shaped turbine blade is a very critical and tough work. Based on the parameter evaluation idea, the aim of this study is to develop methods for extracting key parameters of a turbine blade, which is probably the most important in the whole inspection process. After analyzing the definition, new extraction methods of several section parameters are presented in this paper, including chord length, leading/trailing edge and twist of airfoil surface. The proposed algorithms are developed and implemented using C++ language and OpenGL. Some case studies are investigated to validate the approach.
KW - Blade inspection
KW - Parameter extraction
KW - Twist analysis
UR - https://www.scopus.com/pages/publications/78149449131
U2 - 10.1109/ICAL.2010.5585336
DO - 10.1109/ICAL.2010.5585336
M3 - 会议稿件
AN - SCOPUS:78149449131
SN - 9781424483754
T3 - 2010 IEEE International Conference on Automation and Logistics, ICAL 2010
SP - 501
EP - 505
BT - 2010 IEEE International Conference on Automation and Logistics, ICAL 2010
T2 - 2010 IEEE International Conference on Automation and Logistics, ICAL 2010
Y2 - 16 August 2010 through 20 August 2010
ER -