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ASTM B 348 : 2013 : REDLINE

ASTM B 348 : 2013 : REDLINE

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

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Standard Specification for Titanium and Titanium Alloy Bars and Billets

Available format(s)

PDF

Language(s)

English

Published date

01-07-2013

Publisher

American Society for Testing and Materials

Superseded date

13-02-2020

Superseded by

ASTM B 348/B348M : 2019 : REDLINE

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CONTAINED IN VOL. 02.04, 2015 Defines annealed titanium and titanium alloy bars and billets.

Committee
B 10
DocumentType
Redline
Pages
11
PublisherName
American Society for Testing and Materials
Status
Superseded
SupersededBy

1.1This specification2 covers annealed titanium and titanium alloy bars and billets as follows:

1.1.1Grade 1—UNS R50250. Unalloyed titanium,

1.1.2Grade 2—UNS R50400. Unalloyed titanium,

1.1.2.1Grade 2H—UNS R50400. Unalloyed titanium (Grade 2 with 58 ksi (400 MPa) minimum UTS),

1.1.3Grade 3—UNS R50550. Unalloyed titanium,

1.1.4Grade 4—UNS R50700. Unalloyed titanium,

1.1.5Grade 5—UNS R56400. Titanium alloy (6 % aluminum, 4 % vanadium),

1.1.6Grade 6—UNS R54520. Titanium alloy (5 % aluminum, 2.5 % tin),

1.1.7Grade 7—UNS R52400. Unalloyed titanium plus 0.12 to 0.25 % palladium,

1.1.7.1Grade 7H—UNS R52400. Unalloyed titanium plus 0.12 to 0.25 % palladium (Grade 7 with 58 ksi (400 MPa) minimum UTS),

1.1.8Grade 9—UNS R56320. Titanium alloy (3 % aluminum, 2.5 % vanadium),

1.1.9Grade 11—UNS R52250. Unalloyed titanium plus 0.12 to 0.25 % palladium,

1.1.10Grade 12—UNS R53400. Titanium alloy (0.3 % molybdenum, 0.8 % nickel),

1.1.11Grade 13—UNS R53413. Titanium alloy (0.5 % nickel, 0.05 % ruthenium),

1.1.12Grade 14—UNS R53414. Titanium alloy (0.5 % nickel, 0.05 % ruthenium),

1.1.13Grade 15—UNS R53415. Titanium alloy (0.5 % nickel, 0.05 % ruthenium),

1.1.14Grade 16—UNS R52402. Unalloyed titanium plus 0.04 to 0.08 % palladium,

1.1.14.1Grade 16H—UNS R52402. Unalloyed titanium plus 0.04 to 0.08 % palladiumm (Grade 16 with 58 (400 MPa) ksi minimum UTS),

1.1.15Grade 17—UNS R52252. Unalloyed titanium plus 0.04 to 0.08 % palladium,

1.1.16Grade 18—UNS R56322. Titanium alloy (3 % aluminum, 2.5 % vanadium) plus 0.04 to 0.08 % palladium,

1.1.17Grade 19—UNS R58640. Titanium alloy (3 % aluminum, 8 % vanadium, 6 % chromium, 4 % zirconium, 4 % molybdenum),

1.1.18Grade 20—UNS R58645. Titanium alloy (3 % aluminum, 8 % vanadium, 6 % chromium, 4 % zirconium, 4 % molybdenum) plus 0.04 %–0.08 % palladium,

1.1.19Grade 21—UNS R58210. Titanium alloy (15 % molybdenum, 3 % aluminum, 2.7 % niobium, 0.25 % silicon),

1.1.20Grade 23—UNS R56407. Titanium alloy (6 % aluminum, 4 % vanadium with extra low interstitial elements, ELI),

1.1.21Grade 24—UNS R56405. Titanium alloy (6 % aluminum, 4 % vanadium) plus 0.04 % to 0.08 % palladium,

1.1.22Grade 25—UNS R56403. Titanium alloy (6 % aluminum, 4 % vanadium) plus 0.3 % to 0.8 % nickel and 0.04 % to 0.08 % palladium,

1.1.23Grade 26—UNS R52404. Unalloyed titanium plus 0.08 to 0.14 % ruthenium,

1.1.23.1Grade 26H—UNS R52404. Unalloyed titanium plus 0.08 to 0.14 % ruthenium (Grade 26 with 58 ksi (400 MPa) minimum UTS),

1.1.24Grade 27—UNS R52254. Unalloyed titanium plus 0.08 to 0.14 % ruthenium,

1.1.25Grade 28—UNS R56323. Titanium alloy (3 % aluminum, 2.5 % vanadium plus 0.08–0.14 % ruthenium),

1.1.26Grade 29—UNS R56404. Titanium alloy (6 % aluminum, 4 % vanadium, extra low interstitial, ELI plus 0.08 to 0.14 % ruthenium),

1.1.27Grade 30—UNS R53530. Titanium alloy (0.3 % cobalt, 0.05 % palladium),

1.1.28Grade 31—UNS R53532. Titanium alloy (0.3 % cobalt, 0.05 % palladium),

1.1.29Grade 32—UNS R55111. Titanium alloy (5 % aluminum, 1 % tin, 1 % zirconium, 1 % vanadium, 0.8 % molybdenum),

1.1.30Grade 33—UNS R53442. Titanium alloy (0.4 % nickel, 0.015 % palladium, 0.025 % ruthenium, 0.15 % chromium),

1.1.31Grade 34—UNS R53445. Titanium alloy (0.4 % nickel, 0.015 % palladium, 0.025 % ruthenium, 0.15 % chromium),

1.1.32Grade 35—UNS R56340. Titanium alloy (4.5 % aluminum, 2 % molybdenum, 1.6 % vanadium, 0.5 % iron, 0.3 % silicon),

1.1.33Grade 36—UNS R58450. Titanium alloy (45 % niobium),

1.1.34Grade 37—UNS R52815. Titanium alloy (1.5 % aluminum), and

1.1.35Grade 38—UNS R54250. Titanium alloy (4 % aluminum, 2.5 % vanadium, 1.5 % iron).

Note 1—H grade material is identical to the corresponding numeric grade (that is, Grade 2H = Grade 2) except for the higher guaranteed minimum UTS, and may always be certified as meeting the requirements of its corresponding numeric grade. Grades 2H, 7H, 16H, and 26H are intended primarily for pressure vessel use.

1.2The values stated in inch-pound units are to be regarded as standard. The values given in parentheses are mathematical conversions to SI units that are provided for information only and are not considered standard.

Standards Relationship
UNE 38730:1987 Identical
UNE 38715:1985 Identical

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BS ISO 27186:2010 Active implantable medical devices. Four-pole connector system for implantable cardiac rhythm management devices. Dimensional and test requirements
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ASTM F 1155 : 2010 Standard Practice for Selection and Application of Piping System Materials
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ASTM F 1155 : 2010 : R2015 Standard Practice for Selection and Application of Piping System Materials
I.S. EN ISO 7153-1:2016 SURGICAL INSTRUMENTS - MATERIALS - PART 1: METALS (ISO 7153-1:2016)
ASME B31.1 : 2016 POWER PIPING
BS PD5500(2015) : 2015 SPECIFICATION FOR UNFIRED FUSION WELDED PRESSURE VESSELS
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MIL-DTL-32528 Base Document:2015 Rod, Bar, and Billet, Titanium Alloy TI-5111 for Use in Critical Seawater Application
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ASTM B 363 : 2014 : REDLINE Standard Specification for Seamless and Welded Unalloyed Titanium and Titanium Alloy Welding Fittings
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I.S. EN ISO 4126-2:2003 SAFETY DEVICES FOR PROTECTION AGAINST EXCESSIVE PRESSURE - PART 2: BURSTING DISC SAFETY DEVICES
ASTM B 381 : 2013 : REDLINE SPECIFICATION FOR TITANIUM AND TITANIUM ALLOY FORGINGS
ISO 27186:2010 Active implantable medical devices — Four-pole connector system for implantable cardiac rhythm management devices - Dimensional and test requirements
NASA HDBK 6025 : 2014 GUIDELINES FOR THE SPECIFICATION AND CERTIFICATION OF TITANIUM ALLOYS FOR NASA FLIGHT APPLICATIONS
MIL-HDBK-270 Revision A:1991 Metallic Materials for Low Magnetic Applications, Magnetic Permeability and Electrical Conductivity, Characteristics of (Metric)
10/30191247 DC : DRAFT APR 2010 BS EN ISO 13628-16 - PETROLEUM AND NATURAL GAS INDUSTRIES - DESIGN AND OPERATION OF SUBSEA PRODUCTION SYSTEMS - PART 16: SPECIFICATION FOR FLEXIBLE PIPE ANCILLARY EQUIPMENT
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TR 4661 : 2009 AEROSPACE SERIES - HINGES, FLIGHT CONTROLS MATERIALS AND SURFACE TREATMENTS
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ISO 7153-1:2016 Surgical instruments — Materials — Part 1: Metals
NF EN ISO 9693 : 2000 METAL-CERAMIC DENTAL RESTORATIVE SYSTEMS
EN ISO 7153-1:2016 Surgical instruments - Materials - Part 1: Metals (ISO 7153-1:2016)
AAMI ISO 27186 : 2010 ACTIVE IMPLANTABLE MEDICAL DEVICES - FOUR-POLE CONNECTOR SYSTEM FOR IMPLANTABLE CARDIAC RHYTHM MANAGEMENT DEVICES - DIMENSIONAL AND TEST REQUIREMENTS
PREN 6122 : 200P1 AEROSPACE SERIES - BLIND BOLT, 130 DEGREES FLUSH HEAD, HIGH STRENGTH, PREFERABLE IN COMPOSITE APPLICATION
SAE AS4604B Hose Assembly, 3000 psi, Polytetrafluoroethylene, Metallic Reinforced, 400 °F, Heavy Duty, Aircraft Hydraulic Systems
SAE MA4623 Hose Assembly, Polytetrafluoroethylene, Para Aramid Reinforced Heavy-Duty, 21 000 kPa, 135 °C, Aircraft Hydraulic Systems, Metric
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