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
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;
Conference_Titel :
Electrical and Control Engineering (ICECE), 2010 International Conference on
Conference_Location :
Wuhan
Print_ISBN :
978-1-4244-6880-5
DOI :
10.1109/iCECE.2010.648
