Nimonic901
Nimonic901
Category:Nimonic
Phone :+86 17863510107
WhatsApp : +86 17863510107
Email : cici@hamanjinshu.com
Add : Hunan Road,Liaocheng Shandong,China P.C.252000
Contact us

Product Parameter :

Nimonic901 Material introduction

Nimonic901 It is a Fe Ni Cr based precipitation hardening deformed superalloy. Alloy with metastable γ' [Ni3 (Ti, Al)] phase is aging strengthened, and a little aluminum is inhibited γ' towards η- Transformation of Ni3Ti phase. The alloy has high yield strength and rupture strength below 650 ℃, good oxidation resistance below 760 ℃, and stable structure after long-term use. The main products are turbine disk, compressor disk, journal, static structural parts, turbine outer ring and fasteners.

The alloy has been used to make rotating parts and fasteners of aeroengines and ground gas turbines, and the service life of alloy parts is long.


Nimonic901 chemical composition

element

C

Cr

Ni

Mo

Al

Ti

B

Fe

mass fraction%

0.02-0.06

11.0-14.0

40.0-45.0

5.0-6.5

≤0.3

2.8-3.1

0.01-0.02

element

Mn

Si

P

S

Cu

B1

Pb


mass fraction%

≤0.5

≤0.4

≤0.02

≤0.008

≤0.2

≤0.0001

≤0.001



Nimonic901 Physical and mechanical properties

density

melting point

8. 21g/cm3

1360℃



varieties

heat treatment

θ/℃

Ób/Mpa

Óp0.2/Mpa

δ5/%

Ψ/%

HBS

Disk forging

Standard heat treatment

20

≥1130

≥810

≥9.0

≥12

≥341

575

≥960

≥690

≥8

-

Annular piece


Hot rolled and forged bars

575

≥960

≥690

≥8

-

≥341

Shaft bar

Bars for rotating parts

20

≥1130

≥810

≥9.0

≥12

≥341

575

≥960

≥690

≥8

-


Nimonic901 Heat treatment system

Aviation products

Standard heat treatment system: 1090 ℃± 10 ℃ × 3h/WQ or OQ+775 ℃± 5 ℃ × 4h/AC+(705~ 725)℃±5℃ × 24 h/AC, suitable for disk forgings, rings, bars for shafts, bars for rotating parts, hot rolled and forged bars.

Steam turbine and gas turbine products

System I: 1080 ℃± 15 ℃ × (≥ l h)/AC (or faster)+(775~800) ℃ × (2~4) h/AC (or faster)+(705~745) ℃ × 24h/AC, suitable for hot rolled and forged bars for steam turbine valve stems;

System II: 1090 ℃± 10 ℃ × (≥ 2 h)/OQ or WQ+(775~800) ℃ × (2~4) h/AC+(705~745)℃ × 14h/AC, applicable to hot rolled and forged bars for gas turbine.