MDO Technology Applied to The Aeroengine Turbine Blade Design

WU Li-qiang; YIN Ze-yong; CAI Xian-xin

Volume 20 Issue 5

Oct. 2005

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Article Navigation > Journal of Aerospace Power > 2005 > 20(5): 795-801

WU Li-qiang, YIN Ze-yong, CAI Xian-xin. MDO Technology Applied to The Aeroengine Turbine Blade Design[J]. Journal of Aerospace Power, 2005, 20(5): 795-801.

Citation:

WU Li-qiang, YIN Ze-yong, CAI Xian-xin. MDO Technology Applied to The Aeroengine Turbine Blade Design[J]. Journal of Aerospace Power, 2005, 20(5): 795-801.

WU Li-qiang, YIN Ze-yong, CAI Xian-xin. MDO Technology Applied to The Aeroengine Turbine Blade Design[J]. Journal of Aerospace Power, 2005, 20(5): 795-801.

Citation:

WU Li-qiang, YIN Ze-yong, CAI Xian-xin. MDO Technology Applied to The Aeroengine Turbine Blade Design[J]. Journal of Aerospace Power, 2005, 20(5): 795-801.

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MDO Technology Applied to The Aeroengine Turbine Blade Design

China Aviation Power Plant Research Institute,Hunan Zhuzhou412002,China

Received Date: 2004-07-26
Rev Recd Date: 2004-11-15
Publish Date: 2005-10-28

Abstract

Abstract

Research of Multidisciplinary Design Optimization(MDO) technology applied to the aeroengine turbine blade design was presented.The idiographic implementing process was introduced.Theory and methodology of multidisciplinary coupling optimization design taking account of aerodynamics,heat transfer,structure,vibration and life prediction and optimum algorithm,were discussed.Finally,an example was given.
- aerospace propulsion system,
- Multidisciplinary Design Optimization(MDO),
- turbine blade design,
- aerodynamics,
- heat transfer,
- strength,
- vibration