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  • SAE AMS 4934 : 2015

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    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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    TITANIUM ALLOY, EXTRUSIONS AND FLASH WELDED RINGS, 6AL - 4V, SOLUTION HEAT TREATED AND AGED

    Available format(s):  Hardcopy, PDF

    Superseded date:  03-06-2019

    Language(s):  English

    Published date:  01-01-2015

    Publisher:  SAE International

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    Table of Contents - (Show below) - (Hide below)

    1. SCOPE
    2. APPLICABLE DOCUMENTS
    3. TECHNICAL REQUIREMENTS
    4. QUALITY ASSURANCE PROVISIONS
    5. PREPARATION FOR DELIVERY
    6. ACKNOWLEDGMENT
    7. REJECTIONS
    8. NOTES

    Abstract - (Show below) - (Hide below)

    Specifies a titanium alloy in the form of extruded bars, and shapes, flash welded rings up through 3.000 inches (76.20 mm) inclusive, in nominal diameter or least distance between parallel sides, and stock for flash welded rings of any size.

    General Product Information - (Show below) - (Hide below)

    Committee AMS-G
    Document Type Standard
    Publisher SAE International
    Status Superseded
    Superseded By

    Standards Referenced By This Book - (Show below) - (Hide below)

    09/30199811 DC : 0 BS EN 4632-006 - AEROSPACE SERIES - WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - WELDABILITY AND BRAZEABILITY OF MATERIALS - PART 6: HOMOGENEOUS ASSEMBLIES TITANIUM ALLOYS
    I.S. EN 4632-006:2013 AEROSPACE SERIES - WELDABILITY AND BRAZEABILITY OF MATERIALS IN AEROSPACE CONSTRUCTIONS - PART 006: HOMOGENEOUS ASSEMBLIES OF TITANIUM ALLOYS
    NFL 06 380-24 : 2008 AEROSPACE SERIES - WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - WELDABILITY AND BRAZEABILITY OF MATERIALS - PART 24: HOMOGENEOUS ASSEMBLIES TITANIUM ALLOYS
    BS EN 4632-006:2013 Aerospace series. Weldability and brazeability of materials in aerospace constructions Homogeneous assemblies of titanium alloys
    EN 4632-006:2013 Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 006: Homogeneous assemblies of titanium alloys
    PREN 4632-006 : DRAFT 2008 WELDED AND BRAZED ASSEMBLIES FOR AEROSPACE CONSTRUCTIONS - WELDABILITY AND BRAZEABILITY OF MATERIALS - PART 006: HOMOGENEOUS ASSEMBLIES TITANIUM ALLOYS
    UNI EN 4632-006 : 2014 AEROSPACE SERIES - WELDABILITY AND BRAZEABILITY OF MATERIALS IN AEROSPACE CONSTRUCTIONS - PART 006: HOMOGENEOUS ASSEMBLIES OF TITANIUM ALLOYS

    Standards Referencing This Book - (Show below) - (Hide below)

    ASTM E 2371 : 2013 Standard Test Method for Analysis of Titanium and Titanium Alloys by Direct Current Plasma and Inductively Coupled Plasma Atomic Emission Spectrometry (Performance-Based Test Methodology)
    SAE AMS 2245 : 2017 TOLERANCES, TITANIUM AND TITANIUM ALLOY EXTRUDED BARS, RODS, AND SHAPES
    SAE AMS 2809 : 2007(R2011) IDENTIFICATION, TITANIUM AND TITANIUM ALLOY WROUGHT PRODUCTS
    SAE AMS 2750 : 2012 PYROMETRY
    ASTM E 1409 : 2013 : REDLINE Standard Test Method for Determination of Oxygen and Nitrogen in Titanium and Titanium Alloys by Inert Gas Fusion
    SAE AMS 7498 : 2016 RINGS, FLASH WELDED TITANIUM AND TITANIUM ALLOYS
    SAE AS 6279 : 2016 STANDARD PRACTICE FOR PRODUCTION, DISTRIBUTION, AND PROCUREMENT OF METAL STOCK
    SAE AMS 2249 : 2013 CHEMICAL CHECK ANALYSIS LIMITS, TITANIUM AND TITANIUM ALLOYS
    ASTM E 8/E8M : 2016-09 TEST METHODS FOR TENSION TESTING OF METALLIC MATERIALS
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