DocumentCode
2998558
Title
Aero-engine Blade Design System Based on Knowledge Integration
Author
ZeFeng, Chen ; HaiCheng, Yang ; Rong, Mo ; DanChen, Zheng
Author_Institution
Key Lab. of Contemporary Design & Integrated Manuf. Technol., Northwestern Polytech. Univ., Xi´´an, China
fYear
2010
fDate
25-27 June 2010
Firstpage
2651
Lastpage
2654
Abstract
This paper studies knowledge integration technologies for aero-engine blade design process. The problems of the traditional blade design system are analyzed. The concept and pattern of knowledge integration are introduced. The blade design knowledge is described with OWL, and the prototype system is realized.
Keywords
aerospace components; aerospace computing; aerospace engines; blades; design engineering; knowledge representation languages; OWL; aero-engine blade design system; knowledge integration; prototype system; Blades; Design automation; Knowledge based systems; Shape; Solid modeling; Surface treatment; OWL; blade design; knowledge discovery; knowledge integration;
fLanguage
English
Publisher
ieee
Conference_Titel
Electrical and Control Engineering (ICECE), 2010 International Conference on
Conference_Location
Wuhan
Print_ISBN
978-1-4244-6880-5
Type
conf
DOI
10.1109/iCECE.2010.648
Filename
5630797
Link To Document