To fabricate near net-shape nickel alloy turbine blade airfoil with complex internal structure, process of laser net shape manufacturing (LNSM) is studied in two aspects. One is steady process analysis to establish transfer functions between dimension and process parameters. Another one is dynamic process analysis focusing on decreasing defects in the region of special geometry features. Two solutions, path planning with process parameters optimization and vision based closed loop control are implemented to keep the process stable in those areas. Both solutions are applied successfully in nickel alloy turbine blade airfoil deposition with LNSM system. Geometric inspection shows good dimensional accuracy and surface quality can be achieved with this technology.
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2nd Pacific International Conference on Laser Materials Processing, Micro, Nano and Ultrafast Fabrication
April 3–5, 2006
Melbourne, Australia
ISBN:
978-0-912035-84-0
PROCEEDINGS PAPER
Laser near net shape manufacturing for nickel alloy parts with complex structure Available to Purchase
Xiaoping Huang;
Xiaoping Huang
1
GE (China) Research & Development Center Co. Ltd
. No.1800 Cailun Road, Shanghai, 201203, China
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Yanmin Li;
Yanmin Li
1
GE (China) Research & Development Center Co. Ltd
. No.1800 Cailun Road, Shanghai, 201203, China
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Yong Liu;
Yong Liu
1
GE (China) Research & Development Center Co. Ltd
. No.1800 Cailun Road, Shanghai, 201203, China
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Henry Peng;
Henry Peng
1
GE (China) Research & Development Center Co. Ltd
. No.1800 Cailun Road, Shanghai, 201203, China
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Magdi Azer
Magdi Azer
2
GE Global Research Center
, Niskayuna, NY, 12309-1027, USA
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Published Online:
April 01 2006
Citation
Xiaoping Huang, Yanmin Li, Yong Liu, Henry Peng, Magdi Azer; April 3–5, 2006. "Laser near net shape manufacturing for nickel alloy parts with complex structure." Proceedings of the 2nd Pacific International Conference on Laser Materials Processing, Micro, Nano and Ultrafast Fabrication. PICALO 2006: 2nd Pacific International Conference on Laser Materials Processing, Micro, Nano and Ultrafast Fabrication. Melbourne, Australia. (pp. pp. 196-200). ASME. https://doi.org/10.2351/1.5056926
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