Preparation method of titanium alloy powders
US-12083602-B2 · Sep 10, 2024 · US
US9624565B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9624565-B2 |
| Application number | US-201113988123-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 22, 2011 |
| Priority date | Nov 22, 2010 |
| Publication date | Apr 18, 2017 |
| Grant date | Apr 18, 2017 |
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An alloy having an α′ martensite which is a processing starting structure is hot worked. The alloy is heated at a temperature increase rate of 50 to 800° C./sec, and strain is given at not less than 0.5 by a processing strain rate of from 0.01 to 10/sec in a case of a temperature range of 700 to 800° C., or by a processing strain rate of 0.1 to 10/sec in a case of a temperature range of 800° C. to 1000° C. By generating equiaxial crystals having average crystal particle diameters of less than 1000 nm through the above processes, a titanium alloy having high strength and high fatigue resistant property can be obtained, in which hardness is less than 400 HV, tensile strength is not less than 1200 MPa, and static strength and dynamic strength are superior.
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The invention claimed is: 1. A titanium alloy having a structure classified as near α, and comprising 4 to 9 mass % of Al, 2 to 10 mass % of V and the remainder of Ti and inevitable impurities, the alloy further comprising: structure in which equiaxial crystals having average crystal particle diameter less than 1000 nm are uniformly dispersed, hardness less than 400 HV, an area ratio of a β phase is more than 0% and not more than 1.0%, by measurement of a phase map by an electron backscatter diffraction (EBSD) method, and tensile strength not less than 1200 MPa, wherein the titanium alloy is formed by performing hot working of a processing starting material in which an α′ martensite phase is generated by rapid cooling from a temperature not less than a β transits temperature. 2. The titanium alloy according to claim 1 , wherein an area ratio of crystals of orientation angles having a difference of less than 3° in crystal particles of the equiaxial crystal is not less than 80% by measurement of a GOS map by an electron backscatter diffraction (EBSD) method. 3. The titanium alloy according to claim 1 , wherein a structure accounts for not less than 80% of area ratio, and the structure in which equiaxial crystals having average particle diameter of less than 1000 nm are uniformly dispersed freely at a cross section of a part at which structure is deformed by processing. 4. The titanium alloy according to claim 1 , wherein the average crystal particle diameter of the equiaxial crystal is not more than 600 nm. 5. The titanium alloy according to claim 1 , wherein the hardness is not less than 360 HV. 6. A production method for a titanium alloy according to claim 1 , comprising a step of: processing a titanium alloy having a composition of 4 to 9 mass % of Al, 2 to 10 mass % of V, and the remainder of Ti and inevitable impurities having an α′ martensite phase generated by rapid cooling from a temperature not less than β transus temperature, by a processing method that can develop dynamic recrystallization, so that the titanium alloy has a hardness less than 400 HV and a tensile strength not less than 1200 MPa. 7. The production method for a titanium alloy according to claim 6 , wherein the method comprises the steps of: heating at a temperature increase rate of 50 to 800° C./sec, processing of strain of not less than 0.5 in a temperature range from 700 to 800° C. and a strain rate from 0.01 to 10/sec or in a temperature range of 800° C. to 1000° C. and a strain rate from 0.1 to 10/sec, and cooling at cooling rate not less than 20° C./sec. 8. The production method for a titanium alloy according to claim 7 , wherein the method comprises a step of: processing of strain of not less than 0.8 at a temperature range of 700 to 800° C. and a strain rate of 0.01 to 10/sec.
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