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Aermet 100 Stainless Steel

Typical Applications

Landing Gear

Drive Shafts

Fasteners

Actuators

Jet Engine Shafts

AMS 6532 Suppliers and Stockholders

Dynamic Metals is a specialist supplier and stockholder of AerMet 100 steel, supplying aerospace and defence industries with certified material to AMS 6532 since 1997. No minimum order quantities.

AerMet 100 is an ultrahigh-strength secondary-hardening steel to specification AMS 6532 (UNS K92580). It is a nickel-cobalt-chromium-molybdenum alloy with a unique combination of characteristics – tensile strength of 1931 MPa and high values of fracture toughness and resistance to stress corrosion cracking.

AerMet 100 is special because it combines extreme strength and absence of brittleness characteristic for usual high-strength steels. Fracture toughness (KIC) is about 110 MPa√m – much more than in many other steels with comparable strength levels, thus making AerMet 100 a very reliable material for the production of critical parts.

These qualities of AerMet 100 make it an ideal choice for aerospace structures requiring maximum strength: landing gears, jet engine shafts, drive shafts, actuators, and high-performance fasteners. Moreover, fatigue resistance to cyclic loading increases the operating life of components.

However, processing of AerMet 100 is rather complicated since the material has to be first subjected to solution treatment, then cryogenic and ageing treatments. Machining of the steel should be performed in the state of solution treatment prior to heat treatment.

Technical specification

Related Specifications

AMS 6532
UNS K92580

Specific Gravity

7.9 g/cm3

Chemical Composition (WT %)

 
Min  
Max  
C  
0.21  
0.25  
AI  
-  
0.015  
Co  
13  
14  
Cr  
2.9  
3.3  
Mn  
-  
0.1  
Mo  
1.1  
1.3  
N  
-  
0.0015  
Ni  
11  
12  
O  
-  
0.002  
P  
-  
0.008  
S  
-  
0.005  
S+P  
-  
0.01  
Si  
-  
1.00  
Ti  
-  
0.015  
Fe  
Bal  
-  

Typical Mechanical Properties in the Annealed Condition

 
 
 
Longitudinal  
Transverse  
0.2% Proof Stress  
MPA  
Min  
1620  
1620  
Tensile Strength  
MPA  
Min  
1931  
1931  
Elongation  
%  
Min  
10  
8  
Reduction of area  
%  
Min  
55  
45  

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