This age hardenable nickel base super alloy has very good strength in temperatures up to about 980°C (1800°F).  It’s strength is generally comparable to that of Rene 41 and is generally superior to that of Alloy 718 at temperatures exceeding 650 – 705°C (1200 – 1300°F).   Applications include: Gas turbine engine parts, aerospace components, springs and fasteners.

Composição química aproximada (%)
Ni
Co
Fe
Cr
Mo
Al
Ti
bal
13.5
2 max
19
4.3
1.5
3
   
 
Densidade
(g/cm3)
8.16 Ponto de
fusão (°C)
1330°C
 
Coeficiente de dilatação 12.2 µ m/m °C at 21 - 93°C
 
Misurare la Gamma
0.025mm – 5.0mm (.001” - .197”)
Normas
AMS 5708
 
Tracção aprox. Solution Annealed Stabilize at 843°C (1550°F) for 4 hours and air cool and
age harden at 760°C (1400°F) for 16 hours and air cool
  Spring Temper Anneal at 1050°C (1920°F) for 4 hours and air cool and
stabilize at 843°C (1550°F) for 24 hours and air cool and
age harden at 760°C (1400°F) for 16 hours and air cool
 
Avvicinarsi Estensibile Solution Annealed 800 - 1100 N/mm2
  Solution Annealed + Aged 1300 - 1500 N/mm2
  Spring Temper 1300 - 1600 N/mm2
  Spring Temper +
Annealed + Aged
1300 - 1500 N/mm2
 
Módulo de Young 211 kN/mm2  
 
Temperatura de trabalho aproximada Up to 550°C dipendere dal progetto primaverile e le condizioni operative
   
     
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