ISO/TC 150/SC 1/WG 4 - Metals
Matériaux
General Information
This document establishes a method for detecting and evaluating internal imperfections of cast metallic surgical implants and related weldments. The procedures established in this document apply to film-based methods. The recommendations on the acceptance limits for internal imperfections in cast metallic surgical implants are given in Annex A. NOTE In this document, when not otherwise specified, the term “manufacturer” refers to the “implant manufacturer”, and the term “product” refers to the “metallic cast implant for surgery” or to the “component of metallic cast implant for surgery”.
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This document specifies the characteristics of, and corresponding test methods for, the wrought titanium alloy known as titanium 6-aluminium 4-vanadium alloy (Ti-6Al-4V alloy) for use in the manufacture of surgical implants. NOTE The mechanical properties of a sample obtained from a finished product made of this alloy might not necessarily comply with the specifications given in this document.
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This document specifies the characteristics of, and corresponding test methods for, unalloyed tantalum sheet, rod and wire used in the manufacture of surgical implants. NOTE 1 Provision is made for two grades of tantalum.
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This document specifies the requirements for two wrought cobalt 28-chromium 6-molybdenum alloys used for surgical implants. The properties apply specifically to wrought bar, rod and wire. NOTE 1 The mechanical properties of a sample obtained from a finished product made of this alloy can differ from those specified in this document. NOTE 2 The high carbon content of this alloy produces a structure containing a significant carbide distribution. This can be adjusted either in the production of the bar or in subsequent thermomechanical processing to produce the final device. Carbide distribution in the final device is not included as part of this document.
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This document specifies the characteristics of, and corresponding test methods for, wrought stainless steel containing a mass fraction of 0,25 % to 0,50 % nitrogen for use in the manufacture of surgical implants for which high levels of strength and corrosion resistance are required. NOTE 1 The mechanical properties of a sample obtained from a finished product made of this alloy can differ from those specified in this document. NOTE 2 Requirements for other stainless steels for implants for surgery can be found in ISO 5832-1.
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This document specifies the characteristics of, and corresponding test methods for, the wrought titanium 15-molybdenum 5-zirconium 3-aluminium alloy for use in the manufacture of surgical implants. This document applies to materials in bar form up to a maximum diameter of 100 mm. NOTE The mechanical properties of a sample obtained from a finished product made of this alloy can differ from those specified in this document.
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ISO 5832-2:2018 specifies the characteristics of, and corresponding test methods for, unalloyed titanium for use in the manufacture of surgical implants. Six grades of titanium based on tensile strength are listed in Table 2. NOTE The mechanical properties of a sample obtained from a finished product made of this metal do not necessarily comply with those specified in ISO 5832-2:2018.
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ISO 5832-7:2016 specifies the characteristics of, and corresponding test methods for, forgeable and cold-formed cobalt-chromium-nickel-molybdenum-iron alloy for use in the manufacture of surgical implants.
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ISO 5832-1:2016 specifies the characteristics of, and corresponding test methods for, wrought stainless steel for use in the manufacture of surgical implants. NOTE 1 The mechanical properties of a sample obtained from a finished product made of this alloy can differ from those specified in this part of ISO 5832. NOTE 2 The alloy described in this part of ISO 5832 corresponds to UNS S31673 referred to in ASTM F138/ASTM F139 and to alloy code 1.4441 given in the withdrawn DIN 17443.
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ISO 5832-3:2016 specifies the characteristics of, and corresponding test methods for, the wrought titanium alloy known as titanium 6-aluminium 4-vanadium alloy (Ti 6-AI4-V alloy) for use in the manufacture of surgical implants. NOTE The mechanical properties of a sample obtained from a finished product made of this alloy may not necessarily comply with the specifications given in this part of ISO 5832.
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