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Nimonic80A is a nickel-based superalloy consisting of nickel-chromium. Nickel-based superalloys with excellent high-temperature mechanical properties, high creep strength, high corrosion resistance and oxidation resistance under high temperature and high pressure, these advantages make Nimonic80A widely used in aviation, aerospace, power stations, transportation and other high-temperature hot forgings. The addition of aluminum and titanium to form a gamma phase dispersion strengthened high tempe

Nimonic80A

产品详情

Nimonic80A(UNS N07080)GH4180

Similar Specification:

UNS N07080NA 20BS 3076, HR1, HR201, HR401, HR601
ASTM B637Werkstoff Nr. 2.4631 and 2.4952
AFNOR NC 20TANIMONIC Alloy80A,MSRR 7095 and MSRR 7011
AECMA Pr EN 2188, 2189, 2190, 2191, 2396d 2397VAT80A

Characteristic as below:
A nickel-chromium alloy similar to NIMONIC alloy 75 but made precipitation hardenable by additions of aluminum and titanium. The alloy has good corrosion and oxidation resistance and high tensile and creep-rupture properties at temperatures1500 °F(815°C).

Nimonic80AChemaical composition:

Alloy

%

Ni

Cr

Fe

Mn

Si

P

S

Al

Ti

C

Co

B

Zr

Cu

80A

Min.

Balance

18

1.0

1.8

Max.

21

3.0

1.0

1.0

0.02

0.015

1.8

2.7

0.1

2.0

0.008

0.15

0.2

Nimonic80APhysical properties:

Density

8.19g/cm3

Melting point

1320-1365°C

Nimonic80Aminimum mechanical properties in the room temperature:

Status

Tensile strength
Rm N/mm2

Yield strength
RP0.2N/mm2

Elongation
A5%

Nimonic80A

930

620

20

Application:

Used for gas-turbine components (blades, rings, and discs)bolts, tube supports in nuclear steam generators, die-casting inserts and cores, and exhaust valves in internal-combustion engines.

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