4. ÀÇ·á¿ë ÇձݼÒÀç(ASTM F2036,F1472,F67,F136,F1713,F1813)
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ASTM F2063 ,Wrought Nickel-Titanium Shape Memory Alloys for Medical Devices
and Surgical Implants. This specification covers the chemical, physical, mechanical,
and metallurgical requirements for wrought nickel-titanium bar, flat rolled products,
and tubing containing nominally 54.5 % to 57.0 % nickel and used for the manufacture
of medical devices and surgical implants. The material shall be made from ingot
made from nickel and titanium with no other intentional alloy additions. The material
shall be vacuum or inert atmosphere melted to control metallurgical cleanliness
and alloy chemistry. Bar, plate, and tubing shall be supplied as hot finished or
cold finished and annealed or heat treated. Surface condition may be oxidized,
descaled, pickled, blasted, machined, ground, mechanically polished, or
electropolished. Major elements shall be analyzed by direct current plasma
spectrometry, atomic absorption, inductively coupled plasma spectrometry,
X-ray spectrometer, glow discharge mass spectrometry, or an equivalent method.
Carbon shall be measured by combustion and hydrogen shall be measured by inert
gas fusion or vacuum hot extraction. Nitrogen and oxygen shall be measured
by inert gas fusion. The nickel and titanium contents of nickel-titanium shape
memory alloys cannot be measured to a precision required to guarantee shape
memory or superelastic properties. Calorimetry or an equivalent thermomechanical
test method must be used to assure the alloy formulation in terms of transformation
temperature. Mechanical properties of the samples such as tensile strength
and elongation shall be determined after annealing.
ASTM F1472 Wrought Titanium-6Aluminum-4Vanadium Alloy for Surgical Implant
Applications (UNS R56400). This specification covers the requirements for wrought
titanium-6aluminum-4vanadium alloy for use in surgical implant applications.
The material shall be manufactured by multiple melting in plasma arc and electron
beam furnaces into strip, sheet, plate, bar, forging bar, or wire. The material shall be
available in the annealed or cold-worked condition, with the surface mechanically
descaled or pickled, sandblasted, chemically milled, ground, machined, peeled,
polished, or a combination of these. Heat and product analyses as well as tension
and bend (for sheet, strip, and plate) tests shall be performed and shall conform
to the requirements specified. In addition, the material shall have a microstructure
consisting of a fine dispersion of alpha and beta phases as a result of processing
in the alpha plus beta field, with no continuous alpha network at prior beta grain
boundaries and no coarse, elongated alpha platelets.
ASTM F136 Wrought Titanium-6 Aluminum-4 Vanadium ELI (Extra Low Interstitial)
Alloy for Surgical Implant Applications (UNS R56401).This specification covers
the chemical, mechanical, and metallurgical requirements for wrought annealed
titanium-6aluminum-4vanadium ELI (extra low interstitial) alloy (R56401) to be
used in the manufacture of surgical implants. The products are classified into:
strip, sheet, plate, bar, forging bar, and wire. The heat analysis shall conform
to the chemical composition requirements specified. Product analysis tolerances
do not broaden the specified heat analysis requirements but cover variations
between laboratories in the measurement of chemical content. Tension test
and bend test shall be performed to meet the requirements specified.
ASTM F1713 Wrought Titanium-13Niobium-13Zirconium Alloy for Surgical Implan
Applications (UNS R58130). This specification covers the chemical, mechanical,
and metallurgical requirements for wrought titanium-13niobium-13zirconium
alloy (UNS R58130) bars and wires to be used in the manufacture of surgical
implants. The mill products may be supplied as specified by the purchaser
with a descaled or pickled, abrasive blasted, chemically milled, ground, machined,
peeled, or polished finish. Materials shall be furnished in the unannealed,
solution-treated, or capability-aged condition. The mechanical properties
to which the alloys shall conform are tensile strength, yield strength, elongation,
and reduction of area.
ASTM F1813 Wrought Titanium-12 Molybdenum-6 Zirconium-2 Iron Alloy
for Surgical Implant (UNS R58120). This specification covers the chemical,
mechanical, and metallurgical requirements for wrought titanium-12
molybdenum- 6 zirconium-2 iron alloy for surgical implants to be used
in the manufacture of surgical implants. The heat analysis shall conform
to the chemical composition requirements prescribed. Ingot analysis may be
used for reporting all chemical requirements, except hydrogen. The wrought
titanium-12 molybdenum-6 zirconium-2 iron alloy are classified as bar,
forging bar and wire. The ultimate tensile strength, yield strength, elongation,
and area reduction of the material shall be tested to meet the requirements prescribed.