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Titanium alloy having high ductility, fatigue strength and rigidity and method of manufacturing same

a technology of titanium alloy and ductility, which is applied in the field of titanium alloys having high ductility, fatigue strength and rigidity and manufacturing methods, can solve the problems of not developing high hot workability and ductility, no improvement has been succeeded in achieving high ductility and ductility, and the effect of reducing fatigue strength and ductility

Inactive Publication Date: 2003-05-08
SUMITOMO METAL IND LTD +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

[0007] On the other hand, it is required that the structural elements may be used in a much severer environment and the manufacturing cost may also be reduced, along with an excellent hot workability and mechanical strength. For instance, a high hot workability, a high rigidity, an excellent ductility and fatigue strength are all required for a connecting rod of an automobile, although it can be used in such a sever environment and the manufacturing cost is further reduced. Nevertheless, any titanium alloy having such properties has not developed yet.
[0041] Elements V, Mo, Cr, Fe, Nb, Ni or W may be used as a .beta. phase stabilizing element. The .beta. phase stabilizing element included in the alloy decreases the .beta. transus temperature and improves the hot workability. These elements are solved in the matrix and suppress an excessive generation of metallic compound (Ti.sub.3Al), thereby enabling a greater content of Al to be solved. However, an excessive content of these elements causes the Young's modulus to be markedly reduced. Accordingly, one or more than two of these elements should be added to the alloy within a range not more than 10% in the v equivalent given by the below equation (a), and more preferably not more than 5% in the V equivalent: 2 V equivalent = V + 15 10 Mo + 15 6.3 Cr + 15 4.0 Fe + 15 36 Nb + 15 9 Ni + 15 25 W ( a )

Problems solved by technology

As described above, there is a problem that titanium alloy has a relatively higher mechanical strength, but a smaller Young's modulus, compared with the iron or steel materials.
However, no improvement has been succeeded yet to obtain a high hot workability and a high ductility.
Nevertheless, any titanium alloy having such properties has not developed yet.

Method used

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  • Titanium alloy having high ductility, fatigue strength and rigidity and method of manufacturing same
  • Titanium alloy having high ductility, fatigue strength and rigidity and method of manufacturing same
  • Titanium alloy having high ductility, fatigue strength and rigidity and method of manufacturing same

Examples

Experimental program
Comparison scheme
Effect test

example 1

[0053] A titanium alloy having the composition shown in Table 1 was arc-melted in a vacuum melting furnace to form an ingot having a 140 mm diameter. The .beta. transus temperature of the titanium alloy used in the test was 1070.degree. C.

1TABLE 1 Composition of elements (mass %) Al V Mo B O H Ti 7.72 0.41 0.50 0.90 0.094 0.014 Bal.

[0054] By applying twice the hot forging and the solution treatment to the alloy ingot obtained under the following conditions, test pieces were produced:

[0055] 1. Rough-Forging

[0056] Size after forging: outside diameter 80 mm (working rate 68%, forging rate 3)

[0057] Heating temperature: 1170.degree. C. (the .beta. transus temperature+100.degree. C.)

[0058] 2. Finish Forging

[0059] Size after forging: outside diameter 25 mm (working rate 90%, forging rate 10)

[0060] Heating temperature: 1040.degree. C. to 1170.degree. C. (the respective heating temperatures being indicated in FIG. 1)

[0061] 3. Solution Treatment

[0062] Heating temperature: 700.degree. C. to 11...

example 2

[0067] Utilizing the alloy ingot obtained in Example 1, the effect of the aging treatment after the solution treatment was studied by varying the conditions of hot forging. The titanium alloys used to test were treated according to the following processes A to D.

[0068] 1. Process A (Comparative Example)

[0069] 1-1. Finishing Forging

[0070] Size after forging: outside diameter 25 mm (working rate 97%, forging rate 30)

[0071] Heating temperature: 1170.degree. C. (the .beta. transus temperature+100.degree. C.)

[0072] 1-2. Solution Treatment

[0073] Condition of treatment: 900.degree. C..times.2 hours

[0074] 2. Process B (Comparative Example)

[0075] 2-1. Finishing Forging

[0076] Size after forging: outside diameter 25 mm (working rate 97%, forging rate 30)

[0077] Heating temperature: 1170.degree. C. (the .beta. transus temperature+100.degree. C.)

[0078] 2-2. Solution Treatment

[0079] Treatment condition: 900.degree. C..times.2 hours

[0080] 2-3. Aging Treatment

[0081] Treatment condition: 580.degree. ...

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Abstract

A titanium alloy is provided wherein metal boride is uniformly crystallized and / or precipitated in the matrix. The heating temperature in the finishing hot working is set smaller than the beta transus temperature by not less than 10° C., thereby causing the matrix to include an equiaxial alpha structure in a rate of not less than 40 vol %. This titanium alloy has excellent properties, i.e., high rigidity, ductility and fatigue strength, which are all required for structural components, and therefore can be widely applied to a mechanical component such as an engine of an automobile, a structural component in an aircraft as well as a component for a high speed rail vehicle.

Description

[0001] The present invention relates to a titanium alloy having a high ductility, fatigue strength and rigidity, which alloy is used in a mechanical component requiring excellent mechanical properties and a light weight as well, for instance, a connecting rod, valve, camshaft, crankshaft and push rod in an engine of an automobile or a structural component in an aircraft, a high-speed rail vehicle or the like. The present invention also relates to a method of manufacturing such a titanium alloy.[0002] A titanium alloy has excellent properties for the corrosion resistance and the heat resistance, along with a high mechanical strength and a lightweight property, so that an application of the alloy to various mechanical components in an automobile, an aircraft and a high-speed rail vehicle is now widely extending. However, titanium alloy has a relatively small Young's modulus, i.e., about half of that in iron or steel materials. Accordingly, buckling and bending must be taken into accou...

Claims

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Application Information

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IPC IPC(8): C22C14/00C22F1/18
CPCC22F1/183C22C14/00
Inventor ARIYASU, NOZOMUMATSUMOTO, SATOSHI
Owner SUMITOMO METAL IND LTD
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