ASTM F67-06
(Specification)Standard Specification for Unalloyed Titanium, for Surgical Implant Applications (UNS R50250, UNS R50400, UNS R50550, UNS R50700)
Standard Specification for Unalloyed Titanium, for Surgical Implant Applications (UNS R50250, UNS R50400, UNS R50550, UNS R50700)
ABSTRACT
This specification covers the chemical, mechanical, and metallurgical requirements for four grades of unalloyed titanium strips, sheets, plates, bars, billets, forgings, and wires used for the manufacture of surgical implants. The four grades identified here are defined as follows: Grade 1—UNS R50250; Grade 2—UNS R50400; Grade 3—UNS R50550; and Grade 4—UNS R50700. Mill products may be supplied with a descaled or pickled, abrasive blasted, chemically milled, ground, machined, peeled, or polished finish, or as specified by the purchaser. Materials shall be furnished in the hotworked, cold-worked, forged, annealed, or stress-relieved condition. Mechanical properties to which the titanium materials shall conform are ultimate tensile strength, yield strength, elongation, and reduction of area.
SCOPE
1.1 This specification covers the chemical, mechanical, and metallurgical requirements for four grades of unalloyed titanium strip, sheet, plate, bar, billet, forging, and wire used for the manufacture of surgical implants.
1.2 The values stated in inch-pound units are to be regarded as the standard. The SI equivalents in parentheses are for information only.
General Information
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Standards Content (Sample)
NOTICE: This standard has either been superseded and replaced by a new version or withdrawn.
Contact ASTM International (www.astm.org) for the latest information
Designation:F67 −06
StandardSpecification for
Unalloyed Titanium, for Surgical Implant Applications (UNS
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R50250, UNS R50400, UNS R50550, UNS R50700)
ThisstandardisissuedunderthefixeddesignationF67;thenumberimmediatelyfollowingthedesignationindicatestheyearoforiginal
adoptionor,inthecaseofrevision,theyearoflastrevision.Anumberinparenthesesindicatestheyearoflastreapproval.Asuperscript
epsilon (´) indicates an editorial change since the last revision or reapproval.
1. Scope* Materials on Muscle and Bone
2.2 Aerospace Material Specification:
1.1 This specification covers the chemical, mechanical, and
AMS 2249Chemical Check Analysis Limits, Titanium and
metallurgical requirements for four grades of unalloyed tita-
3
Titanium Alloys
nium strip, sheet, plate, bar, billet, forging, and wire used for
2.3 ISO Standards:
the manufacture of surgical implants.
ISO 5832-2Implants for Surgery—Metallic Materials—
1.2 Thevaluesstatedininch-poundunitsaretoberegarded 4
Unalloyed Titanium
as the standard. The SI equivalents in parentheses are for
ISO 6892Metallic Materials—Tensile Testing at Ambient
information only. 4
Temperature
4
ISO 9001Quality Management Systems
2. Referenced Documents
2.4 American Society for Quality (ASQ) Standard:
2
2.1 ASTM Standards:
C1Specifications of General Requirements for a Quality
4
B265Specification for Titanium and Titanium Alloy Strip,
Program
Sheet, and Plate
3. Terminology
B348Specification for Titanium and Titanium Alloy Bars
and Billets
3.1 Definitions of Terms Specific to This Standard:
B381Specification for Titanium and Titanium Alloy Forg-
3.1.1 lot, n—the total number of mill products produced
ings
from the same melt heat under the same conditions at essen-
E8Test Methods for Tension Testing of Metallic Materials
tially the same time.
E29Practice for Using Significant Digits in Test Data to
4. Product Classification
Determine Conformance with Specifications
E290Test Methods for Bend Testing of Material for Ductil-
4.1 ProductclassificationsareconsistentwithSpecifications
ity
B265, B348, and B381.
E1409TestMethodforDeterminationofOxygenandNitro-
4.1.1 Strip—Anyproduct0.1875in.(4.76mm)andunderin
gen in Titanium and Titanium Alloys by the Inert Gas
thickness and less than 24 in. (610 mm) in width.
Fusion Technique
4.1.2 Sheet—Any product 0.1875 in. (4.76 mm) and under
E1447Test Method for Determination of Hydrogen in Tita-
in thickness and 24 in. (610 mm) or more in width.
nium and Titanium Alloys by Inert Gas Fusion Thermal
4.1.3 Plate—Any product 0.1875 in. (4.76 mm) thick and
Conductivity/Infrared Detection Method
over and 10 in. (254 mm) wide and over, with widths greater
E2371Test Method for Analysis of Titanium and Titanium
than five times thickness. Plate up to 4 in. (101.60 mm), thick
Alloys by Atomic Emission Plasma Spectrometry
inclusive is covered by this specification.
F981Practice for Assessment of Compatibility of Biomate-
4.1.4 Bar—Rounds, flats, or other shapes from 0.1875 in.
rials for Surgical Implants with Respect to Effect of
(4.76 mm) to 4 in. (101.60 mm) in diameter or thickness.
(Other sizes and shapes by special order.)
4.1.5 Billet—A solid semi-finished section hot rolled or
1
This specification is under the jurisdiction of ASTM Committee F04 on
forgedfromaningot,withacrosssectionalareagreaterthan16
Medical and Surgical Materials and Devices and is the direct responsibility of
2 2
in. (10322 mm ) whose width is less than 5 times its
Subcommittee F04.12 on Metallurgical Materials.
Current edition approved June 1, 2006. Published June 2006. Originally thickness.
approved in 1966. Last previous edition approved in 2000 as F67–00. DOI:
10.1520/F0067-06.
2 3
For referenced ASTM standards, visit the ASTM website, www.astm.org, or Available from Society of Automotive Engineers (SAE), 400 Commonwealth
contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM Dr., Warrendale, PA 15096-0001.
4
Standards volume information, refer to the standard’s Document Summary page on Available from American Society for Quality (ASQ), 600 N. Plankinton Ave.,
the ASTM website. Milwaukee, WI 53203.
*A Summary of Changes section appears at the end of this standard
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
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F67−06
TABLE 1 Chemical Requirements
A
Composition , % (mass/mass)
Element
Grade 1 Grade 2 Grade 3 Grade 4
UNS R50250 UNS R50400 UNS R50550 UNS R50700
Nitrogen, max 0.03 0.03 0.05 0.05
Carbon, max 0.08 0.08 0.08 0.08
B
Hydrogen, max 0.015 0.015 0.015 0.015
Iron, max 0.20 0.30 0.30 0.50
Oxygen, max 0.18 0.25 0.35 0.40
Titanium balance balance balance balance
A
Forgings are designated Grade F-1, F-2, F-3, or F-4 respectively. Forging compositions are as specified in Table 1.
B
Maximum hydrogen conte
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