ASTM F562-02
(Specification)Standard Specification for Wrought 35Cobalt-35Nickel-20Chromium-10Molybdenum Alloy for Surgical Implant Applications (UNS R30035)
Standard Specification for Wrought 35Cobalt-35Nickel-20Chromium-10Molybdenum Alloy for Surgical Implant Applications (UNS R30035)
SCOPE
1.1 This specification covers requirements of wrought 35cobalt-35nickel-20chromium-10molybdenum alloy (UNS R30035) in the form of bar and wire, used for the manufacture of surgical implants. This alloy depends on combinations of work-strengthening, and work-strengthening and aging to attain a variety of combinations of strength and ductility.
1.2 The values stated in inch-pound units are to be regarded as the standard. The SI equivalents of the inch-pound units may be approximate.
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Designation: F 562 – 02
Standard Specification for
Wrought 35Cobalt-35Nickel-20Chromium-10Molybdenum
1
Alloy for Surgical Implant Applications (UNS R30035)
This standard is issued under the fixed designation F 562; the number immediately following the designation indicates the year of
original adoption or, in the case of revision, the year of last revision. A number in parentheses indicates the year of last reapproval. A
superscript epsilon (e) indicates an editorial change since the last revision or reapproval.
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1. Scope* Nickel Alloys and Cobalt Alloys
2.4 American Society for Quality Standard:
1.1 This specification covers requirements of wrought
ASQ C1 Specification of General Requirements for a Qual-
35cobalt-35nickel-20chromium-10molybdenum alloy (UNS
8
ity Program
R30035) in the form of bar and wire, used for the manufacture
2.5 Society of Automotive Engineers:
of surgical implants. This alloy depends on combinations of
SAE J1086 Practice for Numbering Metals and Alloys
work-strengthening, and work-strengthening and aging to at-
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(UNS)
tain a variety of combinations of strength and ductility.
1.2 The values stated in inch-pound units are to be regarded
3. Classification
asthestandard.TheSIequivalentsoftheinch-poundunitsmay
3.1 Bar—Round Bars and Flats from 0.1875 in. (4.75 mm)
be approximate.
to 4.00 in. (101.60 mm) in diameter or thickness (other shapes
2. Referenced Documents by special order).
3.2 Wire—Rounds less than 0.1875 in. (4.75 mm) in diam-
2.1 ASTM Standards:
eter.
A 751 Test Methods, Practices, and Terminology for
2
Chemical Analysis of Steel Products
4. Ordering Information
3
E8 TestMethodsforTensionTestingofMetallicMaterials
4.1 Inquiries and orders for material under this specification
E112 Test Methods for Determining the Average Grain
3 shall include the following information:
Size
4.1.1 Quantity,
E 354 Test Methods for Chemical Analysis of High-
4.1.2 ASTM designation and date of issue,
Temperature, Electrical, Magnetic, and Other Similar Iron,
4 4.1.3 Mechanical properties (Section 7),
Nickel, and Cobalt Alloys
4.1.4 Form (bar or wire),
F 981 Practice for Assessment of Compatibility of Bioma-
4.1.5 Applicable dimensions, including size, thickness,
terials for Surgical Implants with Respect to Effect of
5 width, and length (exact, random, multiples), or drawing
Materials on Muscle and Bone
number,
2.2 ISO Standards:
4.1.6 Condition (5.1),
ISO 5832/6 Implants for Surgery—Metallic Materials Part
6 4.1.7 Finish (5.2),
6: Wrought cobalt-nickel-chromium-molybdenum alloy
4.1.8 Special tests, if applicable, and
ISO 6892 Metallic Materials—Tensile Testing at Ambient
6 4.1.9 Other requirements.
Temperature
2.3 Aerospace Material Specification:
5. Materials and Manufacture
AMS 2269 Chemical Check Analysis Limits—Wrought
5.1 Condition—Bar and wire shall be furnished, as speci-
fied, in the solution-annealed, cold-worked, or cold-worked
1
and aged condition.
This specification is under the jurisdiction of ASTM Committee F04 on
Medical and Surgical Materials and Devices and is the direct responsibility of
5.2 Finish—Types of finish available in bar and wire
Subcommittee F04.12 on Metallurgical Materials.
productsarecolddrawn,pickled,ground,groundandpolished,
Current edition approved April 10, 2002. Published June 2002. Originally
or as specified by the purchaser.
published as F 562 – 78. Last previous edition F 562 – 00.
2
Annual Book of ASTM Standards, Vol 01.03.
3
Annual Book of ASTM Standards, Vol 03.01.
4 7
Annual Book of ASTM Standards, Vol 03.05. Available from Society of Automotive Engineers, Inc., 400 Commonwealth
5
Annual Book of ASTM Standards, Vol 13.01. Drive, Warrendale, PA 15096–0001.
6 8
AvailablefromStandardizationDocumentsOrderDesk,Bldg.4SectionD,700 Available from American Society for Quality, 600 N. Plankinton Ave.,
Robbins Ave., Philadelphia, PA 19111-5094, Attn: NPODS. 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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F562–02
A,B
TABLE 2 Product Analysis Tolerances
6. Chemical Requirements
Tolerance Under the Minimum or
6.1 Chemical analysis shall be in accordance with Test
Element
C
Over the Maximum Limit % (mass/mass)
Methods E 354 and A 751.
Carbon 0.01
6.2 The cobalt-35nickel-20chromium-10molybdenum alloy
Manganese 0.03
shall conform to the chemical requirements prescribed inTable
Silicon 0.02
Phosphorus 0.005
1. The supplier shall not ship material that is outside the limits
Sulfur 0.005
specified in Table 1.
Chromium 0.25
6.2.1 Requirements for the major and minor elemental
Nickel 0.30
Molybdenum 0.15
constituents are listed in Table 1. Also listed are important
Iron 0.05
residual elements.Analysis for elem
...
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