NFL 06 380-24 : 2008
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
AEROSPACE SERIES - WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - WELDABILITY AND BRAZEABILITY OF MATERIALS - PART 24: HOMOGENEOUS ASSEMBLIES TITANIUM ALLOYS
12-01-2013
12-08-2017
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 |
Withdrawn
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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 |
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