EN 4632-006:2013
Current
Current
The latest, up-to-date edition.
Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 006: Homogeneous assemblies of titanium alloys
Published date
03-20-2013
Publisher
Foreword
1 Scope
2 Normative references
3 Terms, definitions, symbols and abbreviations
4 Use of this standard
5 Updating of this standard
6 List of titanium alloys sheets
7 Material sheets
Bibliography
This European Standard defines degrees of weldability and brazeability for materials or families of materials used in the aerospace applications.It comprises a series of sheets, by materials or by material family, which:- indicate the main titles, the typical chemical composition and the main characteristics,- contain recommendations for welding and brazing,- indicate a degree of weldability or brazeability for a given process under defined conditions.It is applicable without restriction for the manufacturing of new parts or for repair.
| Committee |
ASD-STAN
|
| DevelopmentNote |
Supersedes PREN 4632-006. (04/2013)
|
| DocumentType |
Standard
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Current
|
| Supersedes |
| Standards | Relationship |
| NEN EN 4632-006 : 2013 | Identical |
| UNI EN 4632-006 : 2014 | Identical |
| DIN EN 4632-006:2013-11 | Identical |
| BS EN 4632-006:2013 | Identical |
| NS EN 4632-006 : 2013 | Identical |
| NF EN 4632-006 : 2018 | Identical |
| SN EN 4632-006:2013 | Identical |
| UNE-EN 4632-006:2013 | Identical |
| I.S. EN 4632-006:2013 | Identical |
| PN EN 4632-006 : 2013 | Identical |
| NBN EN 4632-006 : 2013 | Identical |
| 09/30197751 DC : 0 | BS EN 4678 - AEROSPACE SERIES - WELDMENTS AND BRAZEMENTS FOR AEROSPACE STRUCTURES - JOINTS OF METALLIC MATERIALS BY LASER BEAM WELDING - QUALITY OF WELDMENTS |
| 14/30301120 DC : 0 | BS EN 4677-001 - AEROSPACE SERIES - WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - JOINTS OF METALLIC MATERIALS BY ELECTRON BEAM WELDING - PART 001: QUALITY OF WELDED ASSEMBLIES |
| 17/30361562 DC : 0 | BS EN 4677-001 - AEROSPACE SERIES - WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - JOINTS OF METALLIC MATERIALS BY ELECTRON BEAM WELDING - PART 001: QUALITY OF WELDED ASSEMBLIES |
| SAE AMS 4930 : 2015 | TITANIUM ALLOY BARS, WIRE, FORGINGS, AND RINGS, 6AL - 4V, EXTRA LOW INTERSTITIAL, ANNEALED |
| PREN 3455 : 200P2 | AEROSPACE SERIES - TITANIUM ALLOY TI-P19001 - NOT HEAT TREATED - GRADE 2 FORGING STOCK, FOR SOLUTION TREATED AND AGED FORGINGS A OR D <= 300 MM |
| PREN 3464 : 200P3 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - PLATE - 6 MM < A <= 100 MM |
| EN 10052:1993 | Vocabulary of heat treatment terms for ferrous products |
| PREN 3313 : 200P2 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 - NOT HEAT TREATED - GRADE 2 FORGING STOCK, FOR SOLUTION TREATED AND AGED FORGINGS - A OR D <= 360 MM |
| PREN 3453 : 200P2 | AEROSPACE SERIES - TITANIUM TI-P99003 - NOT HEAT TREATED - GRADE 2 FORGING STOCK, FOR ANNEALED FORGINGS A OR D <= 300 MM |
| EN ISO 24034:2010 | Welding consumables - Solid wire electrodes, solid wires and rods for fusion welding of titanium and titanium alloys - Classification (ISO 24034:2010) |
| EN 3311:2009 | Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Bar for machining - D < 110 mm |
| PREN 3736 : 200P1 | AEROSPACE SERIES - TITANIUM ALLOY TI-P65002 - GRADE 2 - SOLUTION TREATED AND AGED - FORGINGS - D[E] <= 75 MM |
| SAE AMS 4981 : 2014 | TITANIUM ALLOY BARS, WIRE, AND FORGINGS, 6.0AL - 2.0SN - 4.0ZR - 6.0MO, SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 4911 : 2014 | TITANIUM ALLOY, SHEET, STRIP, AND PLATE, 6AL - 4 V, ANNEALED |
| ASTM B 265 : 2015 : REDLINE | Standard Specification for Titanium and Titanium Alloy Strip, Sheet, and Plate |
| PREN 3463 : 200P2 | AEROSPACE SERIES - TITANIUM ALLOY TI-P19001 - SOLUTION TREATED AND AGED - BAR FOR MACHINING - D <= 75 MM |
| EN 4632-001:2008 | Aerospace series - Welded and brazed assemblies for aerospace constructions - Weldability and brazeability of materials - Part 001: General requirements |
| EN 3355 : 2012 | Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Extruded section - De ≤ 150 mm - 900 MPa ≤ Rm ≤ 1 160 MPa |
| PREN 3456 : 200P3 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - ANNEALED - SHEET AND STRIP, HOT ROLLED - A <= 6 MM |
| SAE AMS 4966 : 2013 | TITANIUM ALLOY, FORGINGS, 5AL - 2.5SN, ANNEALED, 110 KSI (758 MPA) YIELD STRENGTH |
| AWS A5.16/A5.16M : 2013 | SPECIFICATION FOR TITANIUM AND TITANIUM-ALLOY WELDING ELECTRODES AND RODS |
| PREN 3499 : 200P2 | AEROSPACE SERIES - TITANIUM TI-P99003 - ANNEALED - SHEET AND STRIP, COLD ROLLED - A <= 6 MM - 570 MPA <= R[M] <= 730 MPA |
| PREN 3314 : 200P2 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 - SOLUTION TREATED AND AGED - BAR FOR MACHINING - D <= 75 MM |
| EN ISO 4063:2010 | Welding and allied processes - Nomenclature of processes and reference numbers (ISO 4063:2009, Corrected version 2010-03-01) |
| SAE AMS4897D : 2016 | TITANIUM ALLOY, SHEET AND STRIP, 15MO - 3.0AL - 2.8CB - 0.20SI |
| PREN 3315 : 200P2 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 - SOLUTION TREATED AND AGED - FORGINGS - D[E] <= 75 MM |
| PREN 3442 : 200P2 | AEROSPACE SERIES - TITANIUM TI-P99002 - ANNEALED - SHEET AND STRIP, HOT ROLLED - A <= 6 MM - 390 MPA <= R[M] <= 540 MPA |
| PREN 3498 : 200P2 | AEROSPACE SERIES - TITANIUM TI-P99002 - ANNEALED - SHEET AND STRIP, COLD ROLLED - A <= 6 MM - 390 MPA <= R[M] <= 540 MPA |
| SAE AMS 4965 : 2014 | TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS, 6.0AL 4.0V, SOLUTION HEAT TREATED AND AGED |
| SAE AMS 4920 : 2015 | TITANIUM ALLOY, FORGINGS, 6AI - 4V, ALPHA-BETA OR BETA PROCESSED, ANNEALED |
| SAE AMS 4995 : 1998 | BILLETS AND PREFORMS - 5AL 2SN 2ZR 4CR 4MO 0.10O, PREMIUM QUALITY, POWDER-METALLURGY PRODUCT |
| PREN 3443 : 200P2 | AEROSPACE SERIES - TITANIUM TI-P99003 - ANNEALED - SHEET AND STRIP, HOT ROLLED - A <= 6 MM - 570 MPA <= R[M] <= 730 MPA |
| PREN 3460 : 200P2 | AEROSPACE SERIES - TITANIUM TI-P99002 - ANNEALED - BAR FOR MATCHING - A OR D <= 150 MM - R[M] >= 390 MPA |
| EN 3965:2001 | Aerospace series - Titanium alloy TI-B17001 - Filler metal for brazing - Rolled foil |
| PREN 3321 : 200P2 | AEROSPACE SERIES - TITANIUM ALLOY TI-P65001 - AS FORGED - GRADE 1 FORGING STOCK, FOR SOLUTION TREATED AND AGED FORGINGS - A OR D <= 360 MM |
| PREN 3735 : 200P1 | AEROSPACE SERIES - TITANIUM ALLOY TI-P65002 - SOLUTION TREATED AND AGED - BAR FOR MACHINING - D <= 75 MM |
| PREN 3870 : 200P1 | AEROSPACE SERIES - TITANIUM ALLOY TI-P19001 - SOLUTION TREATED AND AGED - SHEET AND STRIP, HOT ROLLED - A <= 6 MM |
| SAE AMS 4935 : 2014 | TITANIUM ALLOY EXTRUSIONS AND FLASH WELDED RINGS, 6AL - 4V, ANNEALED, BETA PROCESSED |
| PREN 3859 : 200P1 | AEROSPACE SERIES - TITANIUM ALLOY TI-P19001 - ANNEALED - SHEET AND STRIP, HOT ROLLED - A <= 6 MM |
| PREN 3860 : 200P1 | AEROSPACE SERIES - TITANIUM ALLOY TI-P19001 - ANNEALED - SHEET AND STRIP, COLD ROLLED - A <= 6 MM |
| PREN 3322 : 200P2 | AEROSPACE SERIES - TITANIUM ALLOY TI-P65001 - SOLUTION TREATED AND AGED - GRADE 1 - FORGINGS - D[E] <= 75 MM |
| SAE AMS 4985 : 2014 | TITANIUM ALLOY, INVESTMENT CASTINGS 6AL - 4V 130 UTS, 120 YS, 6% EL HOT ISOSTATICALLY PRESSED ANNEAL OPTIONAL OR WHEN SPECIFIED |
| ISO 24034:2010 | Welding consumables Solid wire electrodes, solid wires and rods for fusion welding of titanium and titanium alloys Classification |
| PREN 3461 : 200P2 | AEROSPACE SERIES - TITANIUM TI-P99003 - ANNEALED - BAR FOR MACHINING D <= 150 MM - 540 MPA <= R[M] <= 740 MPA |
| PREN 3462 : 200P2 | AEROSPACE SERIES - TITANIUM ALLOY TI-P19001 - ANNEALED - BAR FOR MACHINING D <= 150 MM |
| PREN 3494 : 200P2 | AEROSPACE SERIES - TITANIUM ALLOY TI-P19001 - GRADE 2 - SOLUTION TREATED AND AGED - FORGINGS - D[E] <= 75 MM |
| EN 3354 : 2013 | AEROSPACE SERIES - TITANIUM ALLOY TI-6AL-4V - ANNEALED - SHEET FOR SUPERPLASTIC FORMING - A <= 6 MM |
| PREN 3495 : 200P2 | AEROSPACE SERIES - TITANIUM ALLOY TI-P19001 - GRADE 2 - ANNEALED - FORGINGS - D[E] <= 150 MM |
| PREN 3737 : 200P1 | AEROSPACE SERIES - TITANIUM ALLOY TI-P65002 - NOT HEAT TREATED - GRADE 2 FORGING STOCK, FOR SOLUTION TREATED AND AGED FORGINGS - A OR D <= 360 MM |
| PREN 3496 : 200P2 | AEROSPACE SERIES - TITANIUM TI-P99003 - GRADE 2 - ANNEALED - FORGINGS - D[E] <= 150 MM |
| PREN 3871 : 200P1 | AEROSPACE SERIES - TITANIUM ALLOY TI-P19001 - SOLUTION TREATED AND AGED - SHEET AND STRIP, COLD ROLLED - A <= 6 MM |
| ISO 4063:2009 | Welding and allied processes — Nomenclature of processes and reference numbers |
| EN 3310 : 2011 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 (TI-6AL-4V) - NOT HEAT TREATED - FORGING STOCK, FOR ANNEALED FORGINGS - D[E] <= 360 MM |
| EN 3120 : 2012 | Aerospace series - Titanium alloy TI-P64003 - Cold worked and stress relieved - Seamless tube for pressure systems - 4 mm ≤ D ≤ 51 mm - 690 MPa ≤ Rm ≤ 1 030 MPa |
| SAE AMS 4966 : 2013 | TITANIUM ALLOY, FORGINGS, 5AL - 2.5SN, ANNEALED, 110 KSI (758 MPA) YIELD STRENGTH |
| SAE AMS 4967 : 2014 | TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS 6.0AL - 4.0V ANNEALED, HEAT TREATABLE |
| SAE AMS 4991 : 2014 | TITANIUM ALLOY CASTINGS, INVESTMENT 6AL - 4V HOT ISOSTATIC PRESSED, ANNEAL OPTIONAL |
| EN 3892:2001 | Aerospace series - Titanium alloy TI-W64001 - Filler metal for welding |
| PREN 3451 : 200P2 | AEROSPACE SERIES - TITANIUM TI-P99002 - NOT HEAT TREATED - GRADE 2 FORGING STOCK, FOR ANNEALED FORGINGS A OR D <= 300 MM |
| SAE AMS 4934 : 2015 | TITANIUM ALLOY, EXTRUSIONS AND FLASH WELDED RINGS, 6AL - 4V, SOLUTION HEAT TREATED AND AGED |
| SAE AMS 4928 : 2016 | TITANIUM ALLOY BARS, WIRE, FORGINGS, RINGS, AND DRAWN SHAPES, 6AL - 4V, ANNEALED |
| PREN 3454 : 200P2 | AEROSPACE SERIES - TITANIUM ALLOY TI-P19001 - NOT HEAT TREATED - GRADE 2 FORGING STOCK, FOR ANNEALED FORGINGS A OR D <= 300 MM |
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