DocumentCode :
1887361
Title :
Parametric geometry representation to support aircraft design
Author :
Soulat, Marcos Elgueta
Author_Institution :
Aeronaut. & Aerosp. Eng., Loiter Syst. Ltda., Santiago, Chile
fYear :
2012
fDate :
3-10 March 2012
Firstpage :
1
Lastpage :
17
Abstract :
Knowledge Based Engineering (KBE) plays an important role in automation and optimization of the aircraft design process. But the lack of real KBE tools limits the promise of Knowledge Based Engineering. To address this deficiency, we propose using the Python programming language to develop viable KBE application tools for aircraft design. Selecting geometric parameterization algorithms is fundamental to automation and optimization of aircraft design. Here the Class-Shape Transformation (CST) method has been selected, and is contrasted to previous research results using a commercial KBE tool called the General-Purpose Declarative Language (GDL). As a result, an application, named the Parameterized Aircraft Builder (PAB), has been developed based on the CST algorithm. With the PAB we are able to generate, visualize, and export Blended Wing Body (BWB) aircraft configuration geometries. In conclusion this research demonstrates that automation and optimization of the aircraft design process may be improved through development of open source KBE Tools.
Keywords :
CAD; aerospace components; aerospace computing; aircraft; knowledge engineering; Python programming language; aircraft design process automation; aircraft design process optimization; blended wing body aircraft configuration geometry; class-shape transformation method; geometric parameterization algorithm; knowledge based engineering; parameterized aircraft builder; parametric geometry representation; Aircraft; Aircraft propulsion; Design automation; Geometry; Object oriented modeling; Shape; Solid modeling;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2012 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
978-1-4577-0556-4
Type :
conf
DOI :
10.1109/AERO.2012.6187342
Filename :
6187342
Link To Document :
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