BS HR 4:1972 Specification for nickel-chromium-cobalt-aluminium-molybdenum-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 15, Co 14. 2, Al 5, Mo 4, Ti 4)
BRITISH STANDARD: AEROSPACE SERIES SPECIFICATION FOR
NICKEL-CHROMIUM-COBALT-ALUMINIUM-MOLYBDENUM-TITANIUM HEAT-RESISTING ALLOY BILLETS, BARS, FORGINGS AND PARTS
(Nickel base, Cr 15, Co 14.2, Al 5, Mo 4, Ti 4)
1. INSPECTION AND TESTING PROCEDURE
2. MANUFACTURE
3. CHEMICAL COMPOSITION
4. CONDITION
5. HEAT TREATMENT
6. MECHANICAL PROPERTIES
BS HR 4:1972 history
2010BS 2HR 4:2010 Specification for nickel-chromium-cobalt-aluminium-molybdenum-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 15, Co 14. 2, Al 5, Mo 4, Ti 4)
1972BS HR 4:1972 Specification for nickel-chromium-cobalt-aluminium-molybdenum-titanium heat-resisting alloy billets, bars, forgings and parts (nickel base, Cr 15, Co 14. 2, Al 5, Mo 4, Ti 4)