ASTM B 348 : 2013 : REDLINE
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
Standard Specification for Titanium and Titanium Alloy Bars and Billets
13-02-2020
English
01-07-2013
CONTAINED IN VOL. 02.04, 2015 Defines annealed titanium and titanium alloy bars and billets.
1.1This specification2 covers annealed titanium and titanium alloy bars and billets as follows:
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,
1.1.25Grade 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),
1.1.29Grade 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),
Committee |
B 10
|
DocumentType |
Redline
|
Pages |
11
|
PublisherName |
American Society for Testing and Materials
|
Status |
Superseded
|
SupersededBy |
Standards | Relationship |
UNE 38730:1987 | Identical |
UNE 38715:1985 | Identical |
15/30314608 DC : 0 | BS EN ISO 7153-1 - SURGICAL INSTRUMENTS - MATERIALS - PART 1: METALS |
SAE AS 5951 : 2017 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA-ARAMID REINFORCED, 5080 PSI (35,000 KPA), 275 DEGREES F (135 DEGREES C), AIRCRAFT HYDRAULIC SYSTEMS |
BS EN ISO 4126-2:2003 | Safety devices for protection against excessive pressure Bursting disc safety devices |
ASTM F 3302 : 2018 | Standard for Additive Manufacturing – Finished Part Properties – Standard Specification for Titanium Alloys via Powder Bed Fusion |
ASTM F 1511 : 2016-11 | SPECIFICATION FOR MECHANICAL SEALS FOR SHIPBOARD PUMP APPLICATIONS |
BS EN ISO 9693:2000 | Metal-ceramic dental restorative systems |
ISO 9693:1999 | Metal-ceramic dental restorative systems |
BS EN ISO 7153-1:2016 | Surgical instruments. Materials Metals |
EN ISO 9693 : 2000 | METAL-CERAMIC DENTAL RESTORATIVE SYSTEMS |
MIL-DTL-1222 Revision J:2000 | STUDS, BOLTS, SCREWS AND NUTS FOR APPLICATIONS WHERE A HIGH DEGREE OF RELIABILITY IS REQUIRED; GENERAL SPECIFICATION FOR |
DEFSTAN 02-862(PT1)/3(2011) : 2011 | NAVAL FASTENERS - PART 1: MATERIAL SELECTION AND USE |
DEFSTAN 02-862(PT3)/3(2011) : 2011 | NAVAL FASTENERS - PART 3: PROCUREMENT OF FIRST LEVEL FASTENERS |
DEFSTAN 02-862(PT2)/3(2011) : 2011 | NAVAL FASTENERS - PART 2: PROCUREMENT OF NON-FIRST LEVEL FASTENERS |
BS ISO 23933:2006 | Aerospace series. Aramid reinforced lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 135°C/20 684 kPa (275°F/3 000 psi) and 135°C/21 000 kPa (275°F/3 046 psi). Procurement specification |
08/30191626 DC : DRAFT OCT 2008 | BS ISO 27186 - ACTIVE IMPLANTABLE MEDICAL DEVICES - FOUR-POLE CONNECTOR SYSTEM FOR IMPLANTABLE CARDIAC RHYTHM MANAGEMENT DEVICES - DIMENSIONAL AND TEST REQUIREMENTS |
BS ISO 27186:2010 | Active implantable medical devices. Four-pole connector system for implantable cardiac rhythm management devices. Dimensional and test requirements |
AWS D1.9/D1.9M:2015 | STRUCTURAL WELDING CODE - TITANIUM |
ISO 23933:2006 | Aerospace Aramid reinforced lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 135 degrees C/20 684 kPa (275 degrees F /3 000 psi) and 135 degrees C/21 000 kPa (275 degrees F/3 046 psi) Procurement specification |
SAE AS 4623 : 2016 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA-ARAMID REINFORCED, 3,000 PSI, 275 DEGREES F, HEAVY DUTY, AIRCRAFT HYDRAULIC SYSTEMS |
ASTM F 1155 : 2010 | Standard Practice for Selection and Application of Piping System Materials |
EN ISO 4126-2:2003/AC:2006 | SAFETY DEVICES FOR PROTECTION AGAINST EXCESSIVE PRESSURE - PART 2: BURSTING DISC SAFETY DEVICES |
ASTM B 988 : 2013 | Standard Specification for Powder Metallurgy (PM) Titanium and Titanium Alloy Structural Components |
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 |
BS PD5500(2018) : 2018 | SPECIFICATION FOR UNFIRED FUSION WELDED PRESSURE VESSELS |
MIL-DTL-32528 Base Document:2015 | Rod, Bar, and Billet, Titanium Alloy TI-5111 for Use in Critical Seawater Application |
05/30128217 DC : DRAFT JAN 2005 | ISO/DIS 23933 - AEROSPACE - ARAMID REINFORCED LIGHTWEIGHT POLYTETRAFLUOROETHYLENE (PTFE) HOSE ASSEMBLIES, CLASSIFICATION 135 DEGREE C/20 684 KPA (275 DEGREE F/3 000 PSI) AND 135 DEGREE C/21 000 KPA (275 DEGREE F/3 046 PSI) - PROCUREMENT SPECIFICATION |
ASTM F 3122 : 2014 | Standard Guide for Evaluating Mechanical Properties of Metal Materials Made via Additive Manufacturing Processes |
ASTM B 363 : 2014 : REDLINE | Standard Specification for Seamless and Welded Unalloyed Titanium and Titanium Alloy Welding Fittings |
SAE AS 1975 : 2016 | Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems |
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 |
SAE AS 5960 : 2013 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC BRAID REINFORCED, 5080 PSI (35000 KPA), 400 DEGREES F (204 DEGREES C), AIRCRAFT HYDRAULIC SYSTEMS |
ISO 4126-2:2003 | Safety devices for protection against excessive pressure Part 2: Bursting disc safety devices |
TR 4661 : 2009 | AEROSPACE SERIES - HINGES, FLIGHT CONTROLS MATERIALS AND SURFACE TREATMENTS |
API 17L1 : 2013 | SPECIFICATION FOR FLEXIBLE PIPE ANCILLARY EQUIPMENT |
SAE MA 1975 : 2015 | HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE, ARAMID REINFORCED, 135 DEGREE C, STANDARD DUTY, 28000/21000 KPA, HYDRAULIC, AIRCRAFT SYSTEMS |
I.S. EN ISO 9693:2000 | METAL-CERAMIC DENTAL RESTORATIVE SYSTEMS |
ISO 7153-1:2016 | Surgical instruments Materials Part 1: Metals |
UNE-EN ISO 7153-1:2017 | Surgical instruments - Materials - Part 1: Metals (ISO 7153-1:2016) |
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 AS 4604 : 2003 | HOSE ASSEMBLY, 3000 PSI, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 400 DEGREES F, HEAVY DUTY, AIRCRAFT HYDRAULIC SYSTEMS |
UNI EN ISO 4126-2 : 2003 | SAFETY DEVICES FOR PROTECTION AGAINST EXCESSIVE PRESSURE - BURSTING DISC SAFETY DEVICES |
SAE MA 4623 : 2015 | Hose Assembly, Polytetrafluoroethylene, Para Aramid Reinforced Heavy-Duty, 21 000 kPa, 135 °C, Aircraft Hydraulic Systems, Metric |
ASTM F 67 : 2013 | Standard Specification for Unalloyed Titanium, for Surgical Implant Applications (UNS R50250, UNS R50400, UNS R50550, UNS R50700) |
NORSOK M 630 : REV 6 | MATERIAL DATA SHEETS AND ELEMENT DATA SHEETS FOR PIPING |
ASTM F 67 : 2013 : R2017 | Standard Specification for Unalloyed Titanium, for Surgical Implant Applications (UNS R50250, UNS R50400, UNS R50550, UNS R50700) |
PREN 6129 : 200P1 | AEROSPACE SERIES - BLIND BOLT, PROTRUDING HEAD, HIGH STRENGTH |
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) |
ASTM E 1409 : 2013 : REDLINE | Standard Test Method for Determination of Oxygen and Nitrogen in Titanium and Titanium Alloys by Inert Gas Fusion |
ASTM E 8 : 2004 | Standard Test Methods for Tension Testing of Metallic Materials |
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