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  HomeContents of Chinese Journal of Mechanical Engineering (English Edition),2003 No.1SUPERPLASTIC FORMING AND AP-PLICATION OF GH4169 SUPERALLOY

Lü Hongjun 

School of Material Science
and Engineering,

Harbin Institute of Technology,

Harbin 150001, China

Yao Caogen

 

Jia Xinchao

Aerospace Research Institute of Materials and Processing Technology,

 Beijing 100076, China

Zhang Kaifeng

School of Material Science
 and Engineering,

Harbin Institute of Technology,

Harbin 150001, China

 

 

SUPERPLASTIC FORMING AND APPLIC-ATION OF GH4169 SUPERALLOY


Abstract: The superplastic forming and application of GH4169 superalloy are studied. It is shown that for the typical superplastic forming strain rates of 10–3 s–1 to 10–4 s–1, the available engineering strains of the fine-grain GH4169 super-alloy are always higher than 250% within wide temperature scopes (920~980℃), and the maximum elongation to failure obtained is 513%. Dynamic grain growth is presented during superplastic deforming for the alloy, and the grain becomes larger with the increase of the strain. A GH4169 fuel manifold of an aerocraft is superplastically formed, and the superplastically formed GH4169 mainfold is tested by 30 MPa hydraulic pressure for 10 min. So some GH4169 alloy complex components can be superplastically formed in the aerospace industry to decrease the costs of fabricating these components.

Key words: Superalloy GH4169  Superplastic forming  Application

 


Received July 12, 2001; received in revised form November 12, 2001; accepted September 10, 2002

 

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