NFL 06 380-24 : 2008

Withdrawn

AEROSPACE SERIES - WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - WELDABILITY AND BRAZEABILITY OF MATERIALS - PART 24: HOMOGENEOUS ASSEMBLIES TITANIUM ALLOYS

Withdrawn date

12-08-2017

Published date

12-01-2013

Publisher

Association Francaise de Normalisation

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)
DocumentType	Standard
PublisherName	Association Francaise de Normalisation
Status	Withdrawn

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 AMS 4930 : 2015	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 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
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
AWS A5.16/A5.16M : 2013	SPECIFICATION FOR TITANIUM AND TITANIUM-ALLOY WELDING ELECTRODES AND RODS
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 : 2016	TITANIUM ALLOY, SHEET AND STRIP, 15MO - 3.0AL - 2.8CB - 0.20SI
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
EN 3965:2001	Aerospace series - Titanium alloy TI-B17001 - Filler metal for brazing - Rolled foil
SAE AMS 4935 : 2014	TITANIUM ALLOY EXTRUSIONS AND FLASH WELDED RINGS, 6AL - 4V, ANNEALED, BETA PROCESSED
SAE AMS 4985 : 2014	TITANIUM ALLOY, INVESTMENT CASTINGS 6AL - 4V 130 UTS, 120 YS, 6% EL HOT ISOSTATICALLY PRESSED ANNEAL OPTIONAL OR WHEN SPECIFIED
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 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
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