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首页> 外文期刊>Chinese Journal of Mechanical Engineering >SUPERPLASTIC FORMING AND APPLICATION OF GH4169 SUPERALLOY
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SUPERPLASTIC FORMING AND APPLICATION OF GH4169 SUPERALLOY

机译:GH4169高温合金的超塑性成形与应用

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摘要

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 superalloy 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.
机译:研究了GH4169高温合金的超塑性成形及其应用。结果表明,典型的超塑性成形应变率为10〜(-3)s〜(-1)至10〜(-4)s〜(-1),细晶粒GH4169高温合金的可用工程应变为在较宽的温度范围(920〜980℃)内总是高于250%,最大断裂伸长率为513%。合金在超塑性变形过程中会出现动态晶粒长大,并且随着应变的增加晶粒变大。超塑性地形成了飞机的GH4169燃料歧管,并在30 MPa的液压下测试了超塑性形成的GH4169主折叠10分钟。因此,某些GH4169合金复杂部件可以在航空航天工业中超塑成型,以降低制造这些部件的成本。

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