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US20140193662A1 - Stainless steel-and-amorphous alloy composite and method for manufacturing - Google Patents

Stainless steel-and-amorphous alloy composite and method for manufacturing Download PDF

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Publication number
US20140193662A1
US20140193662A1 US14/208,052 US201414208052A US2014193662A1 US 20140193662 A1 US20140193662 A1 US 20140193662A1 US 201414208052 A US201414208052 A US 201414208052A US 2014193662 A1 US2014193662 A1 US 2014193662A1
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Prior art keywords
amorphous alloy
stainless steel
composite
steel part
nano
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Abandoned
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US14/208,052
Inventor
Huann-Wu Chiang
Cheng-Shi Chen
Shun-Mao Lin
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Hongfujin Precision Industry Shenzhen Co Ltd
Hon Hai Precision Industry Co Ltd
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Hongfujin Precision Industry Shenzhen Co Ltd
Hon Hai Precision Industry Co Ltd
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Priority claimed from CN201110229894.8A external-priority patent/CN102925952B/en
Application filed by Hongfujin Precision Industry Shenzhen Co Ltd, Hon Hai Precision Industry Co Ltd filed Critical Hongfujin Precision Industry Shenzhen Co Ltd
Priority to US14/208,052 priority Critical patent/US20140193662A1/en
Assigned to HONG FU JIN PRECISION INDUSTRY (SHENZHEN) CO., LTD., HON HAI PRECISION INDUSTRY CO., LTD. reassignment HONG FU JIN PRECISION INDUSTRY (SHENZHEN) CO., LTD. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: CHEN, Cheng-shi, CHIANG, HUANN-WU, LIN, Shun-mao
Publication of US20140193662A1 publication Critical patent/US20140193662A1/en
Abandoned legal-status Critical Current

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
    • B32B15/012—Layered products comprising a layer of metal all layers being exclusively metallic one layer being formed of an iron alloy or steel, another layer being formed of aluminium or an aluminium alloy
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D19/00—Casting in, on, or around objects which form part of the product
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D19/00—Casting in, on, or around objects which form part of the product
    • B22D19/04—Casting in, on, or around objects which form part of the product for joining parts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
    • B32B15/013—Layered products comprising a layer of metal all layers being exclusively metallic one layer being formed of an iron alloy or steel, another layer being formed of a metal other than iron or aluminium
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C1/00—Making non-ferrous alloys
    • C22C1/11—Making amorphous alloys
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C45/00—Amorphous alloys
    • C22C45/001—Amorphous alloys with Cu as the major constituent
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C45/00—Amorphous alloys
    • C22C45/005—Amorphous alloys with Mg as the major constituent
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C45/00—Amorphous alloys
    • C22C45/10—Amorphous alloys with molybdenum, tungsten, niobium, tantalum, titanium, or zirconium or Hf as the major constituent
    • C—CHEMISTRY; METALLURGY
    • C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25F—PROCESSES FOR THE ELECTROLYTIC REMOVAL OF MATERIALS FROM OBJECTS; APPARATUS THEREFOR
    • C25F3/00—Electrolytic etching or polishing
    • C25F3/02—Etching
    • C25F3/06—Etching of iron or steel
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12479—Porous [e.g., foamed, spongy, cracked, etc.]

Definitions

  • the present disclosure generally relates to a composite of stainless steel and amorphous alloy and a method for manufacturing the composite.
  • amorphous alloy may be joined with other metals to be used on electronic devices. Welding and adhesive bonding are two typical joining methods. However, the heat during the welding can produce a crystallization of the amorphous alloy, thus negatively affecting the welding.
  • the adhesive bonding may only achieve a low adhesive strength of about 0.5 MPa between the amorphous alloy and the stainless steel. Moreover, restricted by the chemical durability of the adhesive material, bonded amorphous alloy and stainless steel can be only used within a narrow temperature range of about ⁇ 50° C. to about 100° C., which means they are not suitable in applications where operating or environmental temperatures may fall outside the range.
  • FIG. 1 is a cross-sectional view of an exemplary embodiment of a stainless steel-and-amorphous alloy composite.
  • FIG. 2 is an enlarged schematic view of a circled portion II of FIG. 1 .
  • FIG. 3 is a scanning electron microscopy view of an exemplary embodiment of the electrochemically etched stainless steel part.
  • FIG. 4 is a cross-sectional view of molding the composite shown in FIG. 1 .
  • FIG. 1 shows a stainless steel-and-amorphous alloy composite 100 according to an exemplary embodiment.
  • the stainless steel-and-amorphous alloy composite 100 includes a stainless steel part 11 , and amorphous alloy parts 13 integrally formed on the stainless steel part 11 .
  • the stainless steel part 11 is made of stainless steel, which in the present disclosure refers to known corrosion-resistant ferrous alloys and which include, for instance, Cr stainless steel resulting from adding chromium (Cr) to iron, and Cr—Ni stainless steel comprising combination of nickel (Ni) and chromium (Cr).
  • the stainless steel part 11 defines a plurality of nano-pores 111 in a surface 110 thereof.
  • the nano-pores 111 may be uniformly formed on the surface 110 (see FIG. 3 ).
  • the nano-pores 111 may have an average diameter of about 30 nanometers (nm) to about 60 nm.
  • the amorphous alloy parts 13 may be bonded to the stainless steel part 11 by injection molding, with portions of the amorphous alloy parts 13 penetrating in the nano-pores 111 (see FIG. 2 ).
  • the amorphous alloy parts 13 may be made of an amorphous alloy selected from one of the group consisting of magnesium-based amorphous alloy, zirconium-based amorphous alloy, and copper-based amorphous alloy.
  • the amorphous alloy for the amorphous alloy parts 13 has a super-cooled liquid region ( ⁇ T) larger than 20° C.
  • super-cooled liquid region is defined as the difference (Tx ⁇ Tg) between the onset temperature of glass transition (Tg) and the onset temperature of crystallization (Tx) of an alloy.
  • Tx ⁇ Tg onset temperature of glass transition
  • Tx onset temperature of crystallization
  • the value of ⁇ T is a measure of the amorphous phase-forming ability of the alloy.
  • the onset temperature of crystallization of the amorphous alloy is lower than 500° C.
  • a method for manufacturing the composite 100 may include the following steps:
  • the stainless steel part 11 is provided.
  • the stainless steel part 11 may be formed by punching to obtain a desired shape.
  • the stainless steel part 11 may be degreased.
  • the degreasing process may include the step of dipping the stainless steel part 11 in a degreasing agent for about 5 minutes (min) to about 15 min.
  • the degreasing agent may be a commercial degreaser special for stainless steel or a neutral detergent in common use.
  • the stainless steel part 11 is then rinsed in water.
  • the stainless steel part 11 is electrochemically etched to form the nano-pores 111 .
  • the electrochemical etching process may be carried out in an acid water solution containing about 4 wt %-7 wt % hydrochloric acid, about 10 wt %-12 wt % ferric chloride, and about 1.8 wt %-2.2 wt % ammonium chloride, with the stainless steel part 11 being an anode, and a titanium board being a cathode.
  • An electric current density about 2 ampere per square decimeter (A/dm 2 )-2.5 A/dm 2 is applied between the anode and the cathode.
  • the acid water solution maintains a temperature of about 40° C.-60° C. during the electrochemical etching.
  • Electrochemical etching the stainless steel part 11 may take about 8 min-14 min. Then, the stainless steel part 11 is rinsed in water and then dried.
  • the electrochemically etched stainless steel part 11 is observed using a field emission scanning electronic microscope, such as a JSM-6700F type microscope sold by JEOL Ltd.
  • the observation shows that a plurality of irregular nano-pores 111 are formed on the stainless steel part 11 .
  • the nano-pores 111 have an average diameter of about 30 nm-60 nm.
  • the stainless steel part 11 having the nano-pores 111 is pre-heated to the onset temperature of glass transition (Tg) of the amorphous alloy for the amorphous alloy parts 13 .
  • Tg glass transition
  • the Tg is about 100° C.-200° C.
  • the Tg is about 400° C.-500° C.
  • the pre-heating step may help the amorphous alloy for the amorphous alloy parts 13 easily flow into the nano-pores 111 during the subsequent injection molding step. Also, the pre-heating step may further remove the water remained in the nano-pores 111 , enhancing the bonding between the stainless steel part 11 and the amorphous alloy parts 13 .
  • the pre-heating step may be implemented in an oven.
  • an injection mold 20 is provided.
  • the injection mold 20 includes a core insert 23 and a cavity insert 21 .
  • the core insert 23 defines gates 231 , and first cavities 233 .
  • the cavity insert 21 defines a second cavity 211 for receiving the stainless steel part 11 .
  • the pre-heated stainless steel part 11 is located in the second cavity 211 .
  • Inert gas, such as argon is fed into the injection mold 20 , and molten amorphous alloy is injected through the gates 231 to coat the surface 110 of the stainless steel part 11 and fill the nano-pores 111 , and finally fill the first cavities 233 to form the amorphous alloy parts 13 , as such, the composite 100 is formed.
  • the molten amorphous alloy may be at a temperature of about (Tg+5)° C. to about (Tx ⁇ 10)° C.
  • the injection mold 20 may be at a temperature of about (Tg+5)° C. to about (Tx ⁇ 5)° C.
  • Amorphous alloy at a temperature between the Tg and Tx of the amorphous alloy may be very sensitive to oxidizing atmosphere and oxidized to formed a ceramic film on the surface thereof.
  • inert gas may be fed into to the injection mold 20 as a protecting gas.
  • the onset temperature of crystallization of the magnesium-based amorphous alloy is lower than 500° C., preventing the mechanical property of the stainless steel part 11 from damages.
  • a stainless steel part 11 made of a SUS403 stainless steel is provided.
  • Electrochemically etching the stainless steel part 11 the acid water solution containing 7 wt % hydrochloric acid, 10 wt % ferric chloride, and 2.2 wt % ammonium chloride; the temperature of the acid water solution is maintained at about 40° C.; the electric current density applied is 2 A/dm 2 ; the electrochemical etching takes 8 min.
  • the stainless steel part 11 is pre-heated at a temperature of 157° C.
  • the amorphous alloy is a magnesium-based amorphous alloy containing copper at an atomic percentage of 30%, dysprosium at an atomic percentage of 11.5%, and the remainder magnesium; the magnesium-based amorphous alloy is heated to a temperature of about 170° C. and injection molded to form the amorphous alloy parts 13 .
  • Electrochemically etching the stainless steel part 11 the acid water solution containing 7 wt % hydrochloric acid, 12 wt % ferric chloride, and 2 wt % ammonium chloride; the temperature of the acid water solution is maintained at about 60° C.; the electric current density applied is 2.5 A/dm 2 ; the electrochemical etching takes 14 min.
  • the stainless steel part 11 is pre-heated at a temperature of 412° C.
  • the amorphous alloy is a zirconium-based amorphous alloy containing copper at an atomic percentage of 30%, aluminum at an atomic percentage of 10%, nickel at an atomic percentage of 5%, and the remainder zirconium; the zirconium-based amorphous alloy is heated to a temperature of about 430° C. and injection molded to form the amorphous alloy parts 13 .
  • Electrochemically etching the stainless steel part 11 the acid water solution containing 5 wt % hydrochloric acid, 10 wt % ferric chloride, and 2.1 wt % ammonium chloride; the temperature of the acid water solution is maintained at about 50° C.; the electric current density applied is 2.3 A/dm 2 ; the electrochemical etching takes 12 min.
  • the stainless steel part 11 is pre-heated at a temperature of 433° C.
  • the amorphous alloy is a copper-based amorphous alloy containing zirconium at an atomic percentage of 30%, titanium at an atomic percentage of 10%, and the remainder copper; the copper-based amorphous alloy is heated to a temperature of about 445° C. and injection molded to form the amorphous alloy parts 13 .
  • the shear strength of the composites 100 created by examples 1-3 has been tested.
  • a universal material testing machine sold by INSTRON Ltd may be used. The tests indicate that the shear strength of the composite 100 of example 1 is about 70 MPa.
  • the shear strength of the composite 100 of example 2 is about 110 MPa.
  • the shear strength of the composite 100 of example 3 is about 120 MPa.
  • the composites 100 of examples 1-3 have been subjected to a temperature humidity bias test (72 hours, 85° C., relative humidity: 85%) and a thermal shock test (48 hours, ⁇ 40° C. to 85° C., 4 hours/cycle, 12 cycles total), such testing did not result in decreased tensile or shear strengths of these composites 100 .

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Electrochemistry (AREA)
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Abstract

A stainless steel-and-amorphous alloy composite includes a stainless steel part and an amorphous alloy part. The stainless steel part has nano-pores defined in a surface thereof. The amorphous alloy part is integrally bonded to the surface having the nano-pores. A method for manufacturing the composite is also described.

Description

    CROSS-REFERENCE TO RELATED APPLICATIONS
  • This application is a divisional application of U.S. Ser. No. 13/282,246, filed Oct. 26, 2011 the contents of which are hereby incorporated by reference. The patent application Ser. No. 13/282,246 in turn claims the benefit of priority under 35 USC 119 from Chinese Patent Application 201110229894.8, filed on Aug. 11, 2011. Also, the patent application Ser. No. 13/282,246 is related to U. S. Patent Application (U.S. Ser. No. 13/282,242, Pending), entitled “ALUMINUM-AND-AMORPHOUS ALLOY COMPOSITE AND METHOD FOR MANUFACTURING”, invented by Chang et al. The patent application Ser. No. 13/282,246 has the same assignee as the patent application Ser. No. 13/282,242. The above-indentified applications are incorporated herein by reference.
    • BACKGROUND
  • 1. Technical Field
  • The present disclosure generally relates to a composite of stainless steel and amorphous alloy and a method for manufacturing the composite.
  • 2. Description of Related Art
  • Due to having good properties such as high mechanical strength, high abrasion resistance, and good corrosion resistance, amorphous alloy may be joined with other metals to be used on electronic devices. Welding and adhesive bonding are two typical joining methods. However, the heat during the welding can produce a crystallization of the amorphous alloy, thus negatively affecting the welding. The adhesive bonding may only achieve a low adhesive strength of about 0.5 MPa between the amorphous alloy and the stainless steel. Moreover, restricted by the chemical durability of the adhesive material, bonded amorphous alloy and stainless steel can be only used within a narrow temperature range of about −50° C. to about 100° C., which means they are not suitable in applications where operating or environmental temperatures may fall outside the range.
  • Therefore, there is room for improvement within the art.
    • BRIEF DESCRIPTION OF THE FIGURES
  • Many aspects of the disclosure can be better understood with reference to the following figures. The components in the figures are not necessarily drawn to scale, the emphasis instead being placed upon clearly illustrating the principles of the disclosure. Moreover, in the drawings like reference numerals designate corresponding parts throughout the views.
  • FIG. 1 is a cross-sectional view of an exemplary embodiment of a stainless steel-and-amorphous alloy composite.
  • FIG. 2 is an enlarged schematic view of a circled portion II of FIG. 1.
  • FIG. 3 is a scanning electron microscopy view of an exemplary embodiment of the electrochemically etched stainless steel part.
  • FIG. 4 is a cross-sectional view of molding the composite shown in FIG. 1.
    •  DETAILED DESCRIPTION
  • FIG. 1 shows a stainless steel-and-amorphous alloy composite 100 according to an exemplary embodiment. The stainless steel-and-amorphous alloy composite 100 includes a stainless steel part 11, and amorphous alloy parts 13 integrally formed on the stainless steel part 11.
  • The stainless steel part 11 is made of stainless steel, which in the present disclosure refers to known corrosion-resistant ferrous alloys and which include, for instance, Cr stainless steel resulting from adding chromium (Cr) to iron, and Cr—Ni stainless steel comprising combination of nickel (Ni) and chromium (Cr).
  • Referring to FIG. 2, the stainless steel part 11 defines a plurality of nano-pores 111 in a surface 110 thereof. The nano-pores 111 may be uniformly formed on the surface 110 (see FIG. 3). The nano-pores 111 may have an average diameter of about 30 nanometers (nm) to about 60 nm.
  • The amorphous alloy parts 13 may be bonded to the stainless steel part 11 by injection molding, with portions of the amorphous alloy parts 13 penetrating in the nano-pores 111 (see FIG. 2). The amorphous alloy parts 13 may be made of an amorphous alloy selected from one of the group consisting of magnesium-based amorphous alloy, zirconium-based amorphous alloy, and copper-based amorphous alloy. The amorphous alloy for the amorphous alloy parts 13 has a super-cooled liquid region (ΔT) larger than 20° C. The term “super-cooled liquid region” is defined as the difference (Tx−Tg) between the onset temperature of glass transition (Tg) and the onset temperature of crystallization (Tx) of an alloy. The value of ΔT is a measure of the amorphous phase-forming ability of the alloy. The onset temperature of crystallization of the amorphous alloy is lower than 500° C.
  • A method for manufacturing the composite 100 may include the following steps:
  • The stainless steel part 11 is provided. The stainless steel part 11 may be formed by punching to obtain a desired shape.
  • The stainless steel part 11 may be degreased. The degreasing process may include the step of dipping the stainless steel part 11 in a degreasing agent for about 5 minutes (min) to about 15 min. The degreasing agent may be a commercial degreaser special for stainless steel or a neutral detergent in common use. The stainless steel part 11 is then rinsed in water.
  • The stainless steel part 11 is electrochemically etched to form the nano-pores 111. The electrochemical etching process may be carried out in an acid water solution containing about 4 wt %-7 wt % hydrochloric acid, about 10 wt %-12 wt % ferric chloride, and about 1.8 wt %-2.2 wt % ammonium chloride, with the stainless steel part 11 being an anode, and a titanium board being a cathode. An electric current density about 2 ampere per square decimeter (A/dm2)-2.5 A/dm2 is applied between the anode and the cathode. The acid water solution maintains a temperature of about 40° C.-60° C. during the electrochemical etching. Electrochemical etching the stainless steel part 11 may take about 8 min-14 min. Then, the stainless steel part 11 is rinsed in water and then dried.
  • Referring to FIG. 3, the electrochemically etched stainless steel part 11 is observed using a field emission scanning electronic microscope, such as a JSM-6700F type microscope sold by JEOL Ltd. The observation shows that a plurality of irregular nano-pores 111 are formed on the stainless steel part 11. The nano-pores 111 have an average diameter of about 30 nm-60 nm.
  • The stainless steel part 11 having the nano-pores 111 is pre-heated to the onset temperature of glass transition (Tg) of the amorphous alloy for the amorphous alloy parts 13. In case of magnesium-based amorphous alloy, the Tg is about 100° C.-200° C. In case of zirconium-based amorphous alloy or copper-based amorphous alloy, the Tg is about 400° C.-500° C. The pre-heating step may help the amorphous alloy for the amorphous alloy parts 13 easily flow into the nano-pores 111 during the subsequent injection molding step. Also, the pre-heating step may further remove the water remained in the nano-pores 111, enhancing the bonding between the stainless steel part 11 and the amorphous alloy parts 13. The pre-heating step may be implemented in an oven.
  • Referring to FIG. 4, an injection mold 20 is provided. The injection mold 20 includes a core insert 23 and a cavity insert 21. The core insert 23 defines gates 231, and first cavities 233. The cavity insert 21 defines a second cavity 211 for receiving the stainless steel part 11. The pre-heated stainless steel part 11 is located in the second cavity 211. Inert gas, such as argon is fed into the injection mold 20, and molten amorphous alloy is injected through the gates 231 to coat the surface 110 of the stainless steel part 11 and fill the nano-pores 111, and finally fill the first cavities 233 to form the amorphous alloy parts 13, as such, the composite 100 is formed. The molten amorphous alloy may be at a temperature of about (Tg+5)° C. to about (Tx−10)° C. During the molding process, the injection mold 20 may be at a temperature of about (Tg+5)° C. to about (Tx−5)° C.
  • Amorphous alloy at a temperature between the Tg and Tx of the amorphous alloy may be very sensitive to oxidizing atmosphere and oxidized to formed a ceramic film on the surface thereof. Thus, inert gas may be fed into to the injection mold 20 as a protecting gas. The onset temperature of crystallization of the magnesium-based amorphous alloy is lower than 500° C., preventing the mechanical property of the stainless steel part 11 from damages.
  • Examples of manufacturing the composite 100 are described as follows. The degreasing steps in the specific examples may be substantially the same as described above so it is not described here again.
    • EXAMPLE 1
  • A stainless steel part 11 made of a SUS403 stainless steel is provided.
  • Electrochemically etching the stainless steel part 11: the acid water solution containing 7 wt % hydrochloric acid, 10 wt % ferric chloride, and 2.2 wt % ammonium chloride; the temperature of the acid water solution is maintained at about 40° C.; the electric current density applied is 2 A/dm2; the electrochemical etching takes 8 min.
  • Pre-heating the stainless steel part 11: the stainless steel part 11 is pre-heated at a temperature of 157° C.
  • Injection amorphous alloy to form the amorphous alloy parts 13: the amorphous alloy is a magnesium-based amorphous alloy containing copper at an atomic percentage of 30%, dysprosium at an atomic percentage of 11.5%, and the remainder magnesium; the magnesium-based amorphous alloy is heated to a temperature of about 170° C. and injection molded to form the amorphous alloy parts 13.
    • EXAMPLE 2
  • Providing a stainless steel part 11 made of a SUS405 stainless steel.
  • Electrochemically etching the stainless steel part 11: the acid water solution containing 7 wt % hydrochloric acid, 12 wt % ferric chloride, and 2 wt % ammonium chloride; the temperature of the acid water solution is maintained at about 60° C.; the electric current density applied is 2.5 A/dm2; the electrochemical etching takes 14 min.
  • Pre-heating the stainless steel part 11: the stainless steel part 11 is pre-heated at a temperature of 412° C.
  • Injection amorphous alloy to form the amorphous alloy parts 13: the amorphous alloy is a zirconium-based amorphous alloy containing copper at an atomic percentage of 30%, aluminum at an atomic percentage of 10%, nickel at an atomic percentage of 5%, and the remainder zirconium; the zirconium-based amorphous alloy is heated to a temperature of about 430° C. and injection molded to form the amorphous alloy parts 13.
    • EXAMPLE 3
  • Providing a stainless steel part 11 made of a SUS304 stainless steel.
  • Electrochemically etching the stainless steel part 11: the acid water solution containing 5 wt % hydrochloric acid, 10 wt % ferric chloride, and 2.1 wt % ammonium chloride; the temperature of the acid water solution is maintained at about 50° C.; the electric current density applied is 2.3 A/dm2; the electrochemical etching takes 12 min.
  • Pre-heating the stainless steel part 11: the stainless steel part 11 is pre-heated at a temperature of 433° C.
  • Injection amorphous alloy to form the amorphous alloy parts 13: the amorphous alloy is a copper-based amorphous alloy containing zirconium at an atomic percentage of 30%, titanium at an atomic percentage of 10%, and the remainder copper; the copper-based amorphous alloy is heated to a temperature of about 445° C. and injection molded to form the amorphous alloy parts 13.
    • RESULTS
  • The shear strength of the composites 100 created by examples 1-3 has been tested. A universal material testing machine sold by INSTRON Ltd may be used. The tests indicate that the shear strength of the composite 100 of example 1 is about 70 MPa. The shear strength of the composite 100 of example 2 is about 110 MPa. The shear strength of the composite 100 of example 3 is about 120 MPa.
  • Furthermore, the composites 100 of examples 1-3 have been subjected to a temperature humidity bias test (72 hours, 85° C., relative humidity: 85%) and a thermal shock test (48 hours, −40° C. to 85° C., 4 hours/cycle, 12 cycles total), such testing did not result in decreased tensile or shear strengths of these composites 100.
  • It is believed that the exemplary embodiment and its advantages will be understood from the foregoing description, and it will be apparent that various changes may be made thereto without departing from the spirit and scope of the disclosure or sacrificing all of its advantages, the examples hereinbefore described merely being preferred or exemplary embodiment of the disclosure.

Claims (6)

What is claimed is:
1. A stainless steel-and-amorphous alloy composite, comprising:
a stainless steel part having nano-pores defined in a surface thereof; and
an amorphous alloy part integrally bonded to the surface having the nano-pores.
2. The composite as claimed in claim 1, wherein the nano-pores have an average diameter of about 30 nm-60 nm.
3. The composite as claimed in claim 1, wherein the amorphous alloy part is made of an amorphous alloy selected from the group consisting of magnesium-based amorphous alloy, zirconium-based amorphous alloy, and copper-based amorphous alloy.
4. The composite as claimed in claim 3, wherein the amorphous alloy having a super-cooled liquid region larger than 20° C.
5. The composite as claimed in claim 3, wherein the onset temperature of crystallization of the amorphous alloy is lower than 500° C.
6. The composite as claimed in claim 1, wherein portions of the amorphous alloy part penetrating in the nano-pores.
US14/208,052 2011-08-11 2014-03-13 Stainless steel-and-amorphous alloy composite and method for manufacturing Abandoned US20140193662A1 (en)

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US14/208,052 US20140193662A1 (en) 2011-08-11 2014-03-13 Stainless steel-and-amorphous alloy composite and method for manufacturing

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CN2011102298948 2011-08-11
CN201110229894.8A CN102925952B (en) 2011-08-11 Complex of rustless steel and non-crystaline amorphous metal and preparation method thereof
US13/282,246 US8770262B2 (en) 2011-08-11 2011-10-26 Stainless steel-and-amorphous alloy composite and method for manufacturing
US14/208,052 US20140193662A1 (en) 2011-08-11 2014-03-13 Stainless steel-and-amorphous alloy composite and method for manufacturing

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