This application claims the benefit of priority to Taiwan Patent Application No. 107129622, filed on Aug. 24, 2018. The entire content of the above identified application is incorporated herein by reference.
Some references, which may include patents, patent applications and various publications, may be cited and discussed in the description of this disclosure. The citation and/or discussion of such references is provided merely to clarify the description of the present disclosure and is not an admission that any such reference is “prior art” to the disclosure described herein. All references cited and discussed in this specification are incorporated herein by reference in their entireties and to the same extent as if each reference was individually incorporated by reference.
The present disclosure relates to a titanium based product and a method for manufacturing the same, and more particularly to a two-stage sintered titanium based product and a method for manufacturing the same.
Titanium and its alloys have many advantages such as stable chemical properties, high strength, low weight, high temperature resistance, high corrosion resistance, and high biocompatibility. In recent years, the application industries of titanium alloys widely include automobile, ship, medicine, entertainment equipment, and mobile electronic device.
The main methods for shaping titanium and its alloys include casting, forging and powder metallurgy. Although the casting and forging methods have simpler operations, it is difficult to produce products having complex structures and shapes therewith, and the products produced thereby may have poor precision. The powder metallurgy method is a technique that uses a powder material to form a metal product by shaping and sintering. In contrast, the powder metallurgy method can solve shaping problems associated with components with complex shapes. However, the conventional powder metallurgy method is provided with only one sintering step for the formation of the titanium or titanium alloy material. The one-stage sintered titanium or titanium alloy material is difficult to be precisely processed. In addition, the equipment used to process the one-stage sintered titanium or titanium alloy material may have a high wear rate and thus result in a high processing cost.
Therefore, there is an urgent need to reduce the processing difficulty and cost of the titanium and titanium alloy products having required mechanical properties.
In response to the above-referenced technical inadequacies, the present disclosure provides a method for manufacturing a titanium based product, which can overcome the problems associated with the shaping of titanium or titanium alloy products, and a titanium based product manufactured by the method.
In one aspect, the present disclosure provides a method for manufacturing a titanium based product, including: providing a titanium hydride ingot; pre-sintering the titanium hydride ingot to dehydrogenate the titanium hydride ingot according to a first temperature control mode, so as to form a titanium ingot; machining the titanium ingot to form a titanium semi-product having a desired shape; and post-sintering the titanium semi-product according to a second temperature control mode that is different from the first temperature control mode, so as to form the titanium based product.
In one aspect, the present disclosure provides a titanium based product manufactured by the aforesaid method. The titanium based product has a Vickers hardness between 200 HV and 250 HV, a tensile strength between 600 MPa and 650 MPa, and a yield strength between 500 MPa and 550 MPa.
One of the advantages of the present disclosure is that the method of the present disclosure, which pre-sinters the titanium hydride ingot according to a first temperature control mode, then machines the titanium ingot formed, and subsequently post-sinters the titanium semi-product according to a second temperature control mode formed, can reduce the wear rate of the processing equipment, thereby reducing the cost.
These and other aspects of the present disclosure will become apparent from the following description of the embodiment taken in conjunction with the following drawings and their captions, although variations and modifications therein may be affected without departing from the spirit and scope of the novel concepts of the disclosure.
The present disclosure will become more fully understood from the following detailed description and accompanying drawings.
The present disclosure is more particularly described in the following examples that are intended as illustrative only since numerous modifications and variations therein will be apparent to those skilled in the art. Like numbers in the drawings indicate like components throughout the views. As used in the description herein and throughout the claims that follow, unless the context clearly dictates otherwise, the meaning of “a”, “an”, and “the” includes plural reference, and the meaning of “in” includes “in” and “on”. Titles or subtitles can be used herein for the convenience of a reader, which shall have no influence on the scope of the present disclosure.
The terms used herein generally have their ordinary meanings in the art. In the case of conflict, the present document, including any definitions given herein, will prevail. The same thing can be expressed in more than one way. Alternative language and synonyms can be used for any term(s) discussed herein, and no special significance is to be placed upon whether a term is elaborated or discussed herein. A recital of one or more synonyms does not exclude the use of other synonyms. The use of examples anywhere in this specification including examples of any terms is illustrative only, and in no way limits the scope and meaning of the present disclosure or of any exemplified term. Likewise, the present disclosure is not limited to various embodiments given herein. Numbering terms such as “first”, “second” or “third” can be used to describe various components, signals or the like, which are for distinguishing one component/signal from another one only, and are not intended to, nor should be construed to impose any substantive limitations on the components, signals or the like.
Referring to
Reference is made to
In the present embodiment, the titanium hydride powder has an average particle size between 3 μm and 500 μm, and preferably between 100 μm and 300 μm. If the average particle size is less than 1 μm, the titanium hydride powder may spontaneously ignite. If the average particle size is greater than 400 μm, the titanium hydride powder is difficult to be densely pressed, so that the titanium hydride ingot 102 does not have a required density.
The titanium hydride powder can be made by the following steps. Firstly, a titanium sponge is hydrogenated under a vacuum condition and an atmosphere of a substantially pure hydrogen gas (purity >99.9%) to form a titanium hydride sponge. The titanium sponge is preferably a zero-order titanium sponge that has a low oxygen-content. Subsequently, the titanium hydride sponge is crushed by being ball-milled under a protective atmosphere, and the titanium hydride particles thus obtained are classified by particle size.
Reference is made to
As shown in
Reference is made to
Reference is made to
As shown in
It should be noted that, if predetermined amounts of other metal powders such as 6 wt % of an aluminum powder and 4 wt % of a vanadium powder are mixed into the titanium hydride powder 100 in the step S1, the titanium based product 108 obtained by the step S4 would contain other metal components except for titanium.
Referring now to
One of the advantages of the present disclosure is that the method of the present disclosure, which pre-sinters the titanium hydride ingot according to a first temperature control mode, then machines the titanium ingot formed, and subsequently post-sinters the titanium semi-product according to a second temperature control mode formed, can reduce the wear rate of the processing equipment, thereby reducing costs.
Furthermore, by using the aforesaid technical solution, the process time can be reduced and the processing precision and structural complexity of the titanium based product can be increased.
In addition, the titanium based product of the present disclosure, compared with the conventional titanium substrate, has more excellent mechanical properties. The comparison between the titanium based product of the present disclosure and the commercial titanium substrates is shown in Table 1.
As shown in Table 1, the titanium based product of the present disclosure, compared with the commercial titanium substrate, has an improved hardness, tensile strength, and yield strength. The tensile strength of the titanium based product is between 600 MPa and 650 MPa and the yield strength of the titanium based product is between 500 MPa and 550 MPa.
The foregoing description of the exemplary embodiments of the disclosure has been presented only for the purposes of illustration and description and is not intended to be exhaustive or to limit the disclosure to the precise forms disclosed. Many modifications and variations are possible in light of the above teaching.
The embodiments were chosen and described in order to explain the principles of the disclosure and their practical application so as to enable others skilled in the art to utilize the disclosure and various embodiments and with various modifications as are suited to the particular use contemplated. Alternative embodiments will become apparent to those skilled in the art to which the present disclosure pertains without departing from its spirit and scope.
Number | Date | Country | Kind |
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107129622 | Aug 2018 | TW | national |