Aero-engine Blade Design System Based on Knowledge Integration

Zefeng Chen; Haicheng Yang; Rong Mo; Zheng DanChen

doi:10.1109/icece.2010.648

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JOURNAL ARTICLE

Aero-engine Blade Design System Based on Knowledge Integration

Zefeng Chen Haicheng Yang Rong Mo Zheng DanChen

Year: 2010 Pages: 2651-2654

DOI: 10.1109/icece.2010.648

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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:

Blade (archaeology) Computer science System integration Process (computing) Knowledge-based systems Aero engine Design process Knowledge integration Engineering Systems engineering Knowledge base Mechanical engineering Artificial intelligence Process integration Database

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Diverse Interdisciplinary Research Innovations

Social Sciences → Decision Sciences → Management Science and Operations Research

Extenics and Innovation Methods

Physical Sciences → Engineering → Computational Mechanics

Industrial Technology and Control Systems

Physical Sciences → Engineering → Control and Systems Engineering

Aero-engine Blade Design System Based on Knowledge Integration

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