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1.1 This specification covers annealed titanium and titanium alloy bars and billets as follows:
1.1.1 Grade 1—Unalloyed titanium,
1.1.2 Grade 2—Unalloyed titanium,
1.1.2.1 Grade 2H—Unalloyed titanium (Grade 2 with 58 ksi minimum UTS),
1.1.3 Grade 3—Unalloyed titanium,
1.1.4 Grade 4—Unalloyed titanium,
1.1.5 Grade 5—Titanium alloy (6 % aluminum, 4 % vanadium),
1.1.6 Grade 6—Titanium alloy (5 % aluminum, 2.5 % tin),
1.1.7 Grade 7—Unalloyed titanium plus 0.12 to 0.25 % palladium,
1.1.7.1 Grade 7H—Unalloyed titanium plus 0.12 to 0.25 % palladium (Grade 7 with 58 ksi minimum UTS),
1.1.8 Grade 9—Titanium alloy (3 % aluminum, 2.5 % vanadium),
1.1.9 Grade 11—Unalloyed titanium plus 0.12 to 0.25 % palladium,
1.1.10 Grade 12—Titanium alloy (0.3 % molybdenum, 0.8 % nickel),
1.1.11 Grade 13—Titanium alloy (0.5 % nickel, 0.05 % ruthenium),
1.1.12 Grade 14—Titanium alloy (0.5 % nickel, 0.05 % ruthenium),
1.1.13 Grade 15—Titanium alloy (0.5 % nickel, 0.05 % ruthenium),
1.1.14 Grade 16—Unalloyed titanium plus 0.04 to 0.08 % palladium,
1.1.14.1 Grade 16H—Unalloyed titanium plus 0.04 to 0.08 % palladiumm (Grade 16 with 58 ksi minimum UTS),
1.1.15 Grade 17—Unalloyed titanium plus 0.04 to 0.08 % palladium,
1.1.16 Grade 18—Titanium alloy (3 % aluminum, 2.5 % vanadium) plus 0.04 to 0.08 % palladium,
1.1.17 Grade 19—Titanium alloy (3 % aluminum, 8 % vanadium, 6 % chromium, 4 % zirconium, 4 % molybdenum),
1.1.18 Grade 20—Titanium alloy (3 % aluminum, 8 % vanadium, 6 % chromium, 4 % zirconium, 4 % molybdenum) plus 0.04 %–0.08 % palladium,
1.1.19 Grade 21—Titanium alloy (15 % molybdenum, 3 % aluminum, 2.7 % niobium, 0.25 % silicon),
1.1.20 Grade 23—Titanium alloy (6 % aluminum, 4 % vanadium with extra low interstitial elements, ELI),
1.1.21 Grade 24—Titanium alloy (6 % aluminum, 4 % vanadium) plus 0.04 % to 0.08 % palladium,
1.1.22 Grade 25—Titanium alloy (6 % aluminum, 4 % vanadium) plus 0.3 % to 0.8 % nickel and 0.04 % to 0.08 % palladium,
1.1.23 Grade 26—Unalloyed titanium plus 0.08 to 0.14 % ruthenium,
1.1.23.1 Grade 26H—Unalloyed titanium plus 0.08 to 0.14 % ruthenium (Grade 26 with 58 ksi minimum UTS),
1.1.24 Grade 27—Unalloyed titanium plus 0.08 to 0.14 % ruthenium,
1.1.25 Grade 28—Titanium alloy (3 % aluminum, 2.5 % vanadium plus 0.08–0.14 % ruthenium),
1.1.26 Grade 29—Titanium alloy (6 % aluminum, 4 % vanadium, extra low interstitial, ELI plus 0.08 to 0.14 % ruthenium),
1.1.27 Grade 30—Titanium alloy (0.3 % cobalt, 0.05 % palladium),
1.1.28 Grade 31—Titanium alloy (0.3 % cobalt, 0.05 % palladium),
1.1.29 Grade 32—Titanium alloy (5 % aluminum, 1 % tin, 1 % zirconium, 1 % vanadium, 0.8 % molybdenum),
1.1.30 Grade 33—Titanium alloy (0.4 % nickel, 0.015 % palladium, 0.025 % ruthenium, 0.15 % chromium),
1.1.31 Grade 34—Titanium alloy (0.4 % nickel, 0.015 % palladium, 0.025 % ruthenium, 0.15 % chromium),
1.1.32 Grade 35—Titanium alloy (4.5 % aluminum, 2 % molybdenum, 1.6 % vanadium, 0.5 % iron, 0.3 % silicon),
1.1.33 Grade 36—Titanium alloy (45 % niobium),
1.1.34 Grade 37—Titanium alloy (1.5 % aluminum), and
1.1.35 Grade 38—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.
The H grades were added in response to a user association request based on its study of over 5200 commercial Grade 2, 7, 16, and 26 test reports, where over 99 % met the 58 ksi minimum UTS.
1.2 The 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.
This specification covers annealed bars and grills made from titanium or its alloys. All material grades covered should conform to the required chemical composition requirements. Elements that are intentionally added to the melt should be identified, analyzed and reported in the chemical analysis. Specimens for tension tests should be machined and the tensile properties determined using a specified strain rate through the yield strength and at an increasing rate. Each annealed material may be furnished as either descaled, sandblasted, ground, or rough turned.
| SDO | ASTM: ASTM International |
| Document Number | B348 |
| Publication Date | June 1, 2009 |
| Language | en - English |
| Page Count | 8 |
| Revision Level | 09 |
| Supercedes | |
| Committee | B10.01 |