NFL 06 380-24 : 2008
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AEROSPACE SERIES - WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - WELDABILITY AND BRAZEABILITY OF MATERIALS - PART 24: HOMOGENEOUS ASSEMBLIES TITANIUM ALLOYS
Published date
01-12-2013
Publisher
Withdrawn date
08-12-2017
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Avant-propos
1 Domaine d'application
2 Références normatives
3 Définitions, symboles et abréviations
4 Utilisation de la présente norme
5 Mise à jour de la présente norme
6 Index des fiches alliages de titane
7 Fiches de matériaux
Bibliographie
Describes degrees of weldability and brazeability for materials or families of materials used in the aerospace industry.
| DevelopmentNote |
Indice de classement: L06-380-24. PR NFL 06 380-24 March 2007 (03/2007)
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| DocumentType |
Standard
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| PublisherName |
Association Francaise de Normalisation
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| Status |
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| NFL 06 380-10 : 2003 | WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - WELDABILITY AND BRAZEABILITY OF MATERIALS - PART 10: GENERAL REQUIREMENTS |
| NFL 06 387 : A2007 | WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - JOINTS OF METALLIC MATERIALS BY ELECTRON BEAM WELDING - QUALITY OF WELDED ASSEMBLIES |
| NFL 06 394 : 2010 | WELDMENTS AND BRAZEMENTS FOR AEROSPACE STRUCTURES - ASSEMBLY OF METALLIC MATERIALS WELDED BY TIG METHOD - QUALITY OF WELDMENTS |
| SAE AMS4930H | Titanium Alloy Bars, Wire, Forgings, and Rings 6Al - 4V, Extra Low Interstitial Annealed |
| EN 10052:1993 | Vocabulary of heat treatment terms for ferrous products |
| 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) |
| SAE AMS4981G | Titanium Alloy Bars, Wire, and Forgings 6.0Al - 2.0Sn - 4.0Zr - 6.0Mo Solution and Precipitation Heat Treated |
| SAE AMS4911N | Titanium Alloy, Sheet, Strip, and Plate 6Al - 4V Annealed |
| ASTM B 265 : 2015 : REDLINE | Standard Specification for Titanium and Titanium Alloy Strip, Sheet, and Plate |
| EN 4632-001:2008 | Aerospace series - Welded and brazed assemblies for aerospace constructions - Weldability and brazeability of materials - Part 001: General requirements |
| SAE AMS 4966 : 2013 | TITANIUM ALLOY, FORGINGS, 5AL - 2.5SN, ANNEALED, 110 KSI (758 MPA) YIELD STRENGTH |
| EN 3456:2012 | Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Sheet and strip, hot rolled — a ≤ 6 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 | Titanium Alloy, Sheet and Strip 15Mo - 3.0AI - 2.8Cb - 0.20Si |
| SAE AMS4965L | Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al 4.0V Solution Heat Treated and Aged |
| SAE AMS4920F | Titanium Alloy, Forgings 6AI - 4V Alpha-Beta or Beta Processed, Annealed |
| EN 3965:2001 | Aerospace series - Titanium alloy TI-B17001 - Filler metal for brazing - Rolled foil |
| SAE AMS4935K | Titanium Alloy Extrusions and Flash Welded Rings 6Al - 4V Annealed Beta Processed |
| 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 AMS4967L | Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al - 4.0V Annealed, Heat Treatable |
| SAE AMS4991E | Titanium Alloy Castings, Investment 6Al - 4V Hot Isostatic Pressed, Anneal Optional |
| EN 3892:2001 | Aerospace series - Titanium alloy TI-W64001 - Filler metal for welding |
| SAE AMS4934G | Titanium Alloy, Extrusions and Flash Welded Rings 6Al - 4V Solution Heat Treated and Aged |
| SAE AMS4928V | Titanium Alloy Bars, Wire, Forgings, Rings, and Drawn Shapes 6Al - 4V Annealed |
Summarise
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