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WL 2.4668-2 : 1984

Current
Current

The latest, up-to-date edition.

HIGH TEMPERATURE NICKEL ALLOY WITH ABOUT 0,05C-19CR-18FE-5NB-3MO; RODS AND FORGINGS
Published date

01-12-2013

DocumentType
Standard
PublisherName
German Institute for Standardisation (Deutsches Institut für Normung)
Status
Current

17/30369678 DC : 0 PREN 7010 - AEROSPACE SERIES - USER GUIDE FOR CREATION AND DESIGNATION OF BOLTS
DIN EN 2952:1996-03 (Draft) AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2601 - SOLUTION TREATED AND COLD WORKED - BAR FOR FORGED FASTENERS D <= 50 MM, 1270 MPA <= R[M] <= 1550 MPA
DIN 65442:2016-08 Aerospace - bihexagonal head bolts, close tolerance, with medium-length MJ thread, corrosion resisting nickel alloy - nominal tensile strength 1 550 MPa, for temperatures up to 315 C; Inactive for new design
DIN 65538:1987-08 AEROSPACE - CHEESE HEAD BOLTS, CLOSE TOLERANCE, WITH BIHEXAGON SOCKET AND MJ THREAD, SHORT THREAD, NICKEL ALLOY - NOMINAL TENSILE STRENGTH 1250 MPA, FOR TEMPERATURES UP TO 315 DEGREES C/425 DEGREES C
DIN 65537:1987-08 AEROSPACE - CHEESE HEAD BOLTS WITH BIHEXAGON SOCKET AND MJ THREAD, SHORT THREAD, NICKEL ALLOY; NOMINAL TENSILE STRENGTH 1250 MPA, FOR TEMPERATURES UP TO 315 DEGREES C/425 DEGREES C

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