DocumentCode :
2863654
Title :
An engineering rules based parameterization approach for turbine blade reverse engineering
Author :
Li, Yongqing ; Huang, Xiaoping ; Gong, Chunhe ; Wang, Kelvin
Author_Institution :
Digital Manuf. Lab., GE Global Res. Center, Shanghai, China
fYear :
2004
fDate :
2004
Firstpage :
311
Lastpage :
318
Abstract :
A parameterization approach is presented for turbine blade reverse engineering in this paper. The solution starts with some key features extracted from the point cloud and then the imported sketch templates are optimized to best fit the cross sectional points while satisfying the geometric constraints among the geometry elements of the sketch. In addition, a typical aerodynamic rule (equal circulation rule) is first introduced to the final parametric model, which enables the user to edit the model and redesign a new blade according to the engineering parameters more quickly and conveniently.
Keywords :
computational geometry; curve fitting; engineering graphics; feature extraction; reverse engineering; splines (mathematics); turbines; aerodynamic rule; cross sectional points; engineering rule; equal circulation rule; feature extraction; geometric constraints; geometry elements; parameterization approach; parametric model; point cloud; reverse engineering; sketch template optimization; turbine blade; Aerodynamics; Blades; Clouds; Design engineering; Geometry; Laboratories; Parametric statistics; Reverse engineering; Solid modeling; Turbines;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Geometric Modeling and Processing, 2004. Proceedings
Print_ISBN :
0-7695-2078-2
Type :
conf
DOI :
10.1109/GMAP.2004.1290052
Filename :
1290052
Link To Document :
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