Specification for nickel-iron-chromium-molybdenum-aluminium-titanium heat-resisting alloy billets, bars, forgings and parts (Ni/Co 43.5, Cr 16.5, Mo 3. 3, Al 1.2, Ti 1.2, Fe remainder)
British Standard Aerospace Series : Specification for
Nickel-iron-chromium-molybdenum-aluminium-titanjum heat-resisting alloy billets, bars, forgings and parts
(Ni/Co 43.5, Cr 16.5, Mo 3.3, Al 1.2, Ti 1.2, Fe remainder)
1. Inspection and testing procedure
2. Manufacture
3. Chemical composition
4. Condition
5. Heat treatment
6. Mechanical properties