BS HR 10:1972 Specification for nickel-cobalt-chromium-molybdenum-titanium-aluminium heat-resisting alloy billets, bars, forgings and parts (nickel base, Co 20, Cr 20, Mo 5.9, Ti 2.1, Al 0.5)
BRITISH STANDARD : AEROSPACE SERIES SPECIFICATION FOR
NICKEL-COBALT-CHROMIUM-MOLYBDENUM-TITANIUM-ALUMINIUM HEAT-RESISTING ALLOY BILLETS, BARS, FORGINGS AND PARTS
(Nickel base, Co 20, Cr 20, Mo 5.9, Ti 2.1, Al 0.5)
1. INSPECTION AND TESTING PROCEDURE
2. MANUFACTURE
3. CHEMICAL COMPOSITION
4. CONDITION
5. HEAT TREATMENT
6. MECHANICAL PROPERTIES
BS HR 10:1972 history
2010BS 2HR 10:2010 Specification for nickel-cobalt-chromium-molybdenum-titanium-aluminium heat-resisting alloy billets, bars, forgings and parts (nickel base, Co 20, Cr 20, Mo 5.9, Ti 2.1, Al 0.5)
1972BS HR 10:1972 Specification for nickel-cobalt-chromium-molybdenum-titanium-aluminium heat-resisting alloy billets, bars, forgings and parts (nickel base, Co 20, Cr 20, Mo 5.9, Ti 2.1, Al 0.5)