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GH4169 Wrought Superalloy
Overview of GH4169 Wrought Superalloy
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GH4169 is the most widely used Nickel-based superalloy for turbine disc in gas turbine and jet engines with service temperatures up to 923 K because of its high temperature strength and corrosion resistance. Similar alloy's names in different standards:

Beiye designation

China Standard designation

America designation

France designation

GH4169

GH4169

Inconel 718

NC19FeNb



rene superalloy

The Typical Applications of This Alloy are

  • Turbine disk

  • Rocket motor

  • Nuclear reactor


Typical Chemical Composition in Percent


C

0.04

Cr

18.56

Ti

1.02

Al

0.57

Mo

3.06

Ni

52.89

Nb

5.10

Fe

bal.



Typical Mechanical Properties


Hardness

Hot-working

HRC20

GR

HRC18

Aging Treatment

HRC42

Breaking Strength At 25℃

Cold-working

1250Mpa

Yield Strength At 25℃

Cold-working

1100Mpa

Elongation At 25℃

Cold-working

15%

Breaking Strength At 25℃

Aging Treatment

1300/18000Mpa

Yield Strength At 25℃

Aging Treatment

1150/1700Mpa

Elongation At 25℃

Aging Treatment

6% 24%

Breaking Strength At 650℃

Aging Treatment

1100Mpa

Yield Strength At 650℃

Aging Treatment

900Mpa

Elongation At 650℃

Aging Treatment

18%



Typical Physical Properties

The melting temperature

1260~1320℃

Density

8.3g/cm3

Linear expansivity

400℃

500℃

600℃

14.5

14.9

15.2



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