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
12-01-2013
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| 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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