Various aspects relate generally to chip arrangements.
Decisions have been made by the European Union to ban environmentally hazardous substances in the near future; such decisions having been made with regard to end-of-life vehicles ELV, indicating that hazardous substances such as lead should be banned. Lead-based products, e.g. lead-based solder materials used for die or semiconductor chip attachment, will be banned and removed from the market in the near future.
Suitable alternative solder materials will in future be selected based on their economic viability. The cost of suitable alternatives would have to be at least comparable to that of current standard solder materials. Suitable alternatives will further have to meet the requirements and have the necessary properties to be used as a connection element, e.g. a solder connection. Such alternatives would have to be compatible for use on various surfaces, e.g. on lead frames or on chip back sides. They would also have to be electrically and thermally conductive, and robust and reliable enough for their application, e.g. being subjected to high temperatures or varying temperature loads.
A further technical requirement is that the solidus temperature of the solder material should lie above 260° C., so that the solder material will not melt and/or soften when subsequent processes are carried out, e.g. when soldering the printer circuit board. Further requirements of alternative solder materials are that they meet the requirements of ductility such that solder wires may be provided from the solder materials.
Up until now, the semiconductor field has not had a lead-free soft solder alternative for the connection of a chip to a lead frame, or from a clip to a bond pad, which may be achieved in mass production. The technical challenge lies in finding a lead-free solder which has a melting temperature over that of the solder material used in printed circuit boards e.g. Sn—Ag—Cu systems, with typical melting temperatures of 260° C. However, the melting temperature should not be too high either, as high mechanical stress would have to be installed in the system to cool down and at the same time, solidify the solder.
A lead-free solder material, apart from the melting temperature requirements, should have good wettability with various metallic surfaces e.g. chip surfaces or lead frames which may be used, to ensure that an optimal connection is provided. The solder material should further possess a certain ductility so that it can be produced and handled in wire form. That is, the solder material in wire form should not be brittle. The solder material has to withstand repetitive melting and solidification conditions, and mechanical and thermomechanical loads which may be applied to the material, without succumbing to degradation.
In some aspects, a chip arrangement including: a chip including a chip back side; a substrate including a surface with a plating; and a zinc-based solder alloy which attaches the chip back side to the plating on the surface of the substrate, the zinc-based solder alloy including, by weight, 1% to 30% aluminum, 0.5% to 20% germanium, and 0.5% to 20% gallium, wherein a balance of the zinc-based solder alloy is zinc.
In some aspects, a chip arrangement including: a chip including a chip back side; a substrate including a surface with a plating, wherein the plating includes at least one of nickel or nickel-phosphorous; and a zinc-based solder alloy which attaches the chip back side to the plating on the surface of the substrate, the zinc-based solder alloy including, by weight, 1% to 20% aluminum, 1% to 20% magnesium, wherein a balance of the zinc-based solder alloy is zinc.
In the drawings, like reference characters generally refer to the same parts throughout the different views. The drawings are not necessarily to scale, emphasis instead generally being placed upon illustrating the principles of the invention. In the following description, various aspects of the invention are described with reference to the following drawings, in which:
The following detailed description refers to the accompanying drawings that show, by way of illustration, specific details and aspects in which the invention may be practiced. The word “exemplary” is used herein to mean “serving as an example, instance, or illustration”. Any aspect or design described herein as “exemplary” is not necessarily to be construed as preferred or advantageous over other aspects or designs.
Various aspects provide a lead-free (Pb-free) multilayer solder connection system for electronic components, including at least one side of a chip, a solder connection, e.g. a solder alloy, a carrier, e.g. a lead frame, and a plating, e.g. a lead frame plating, formed over the carrier.
In comparison to lead-based solders, zinc-based solder systems have better physical characteristics, e.g. better thermal/heat and electrical conductivity. This can be seen from
Solder alloy 810 may be used for joining chip back side 820 to carrier 802, e.g. a lead frame, even if chip 814 is not a silicon-based chip. Chip back side 820 may include a backside metallization 816 system including a multilayer system or part or a variant of a multilayer system. The multilayer system may include individual layers having individual functions.
The multilayer system may include contact layer 816a for contacting to a semiconductor material, e.g. an aluminum contact layer, wherein the aluminum forms a layer having a thickness ranging from 50 nm to 1000 nm.
The multilayer system may include barrier layer 816b, e.g. a titanium (Ti) or titanium-tungsten (TiW) barrier layer, wherein barrier layer 816b may have a thickness ranging from 50 nm to 1000 nm.
The multilayer system may include solder reaction layer 816c, the solder reaction layer 816c including at least one of a group of the following elements and/or alloys thereof: nickel, nickel-vanadium, silver, aluminum, gold, platinum, palladium, nickel, wherein the solder reaction layer 816c may have a thickness ranging from 50 nm to 1000 nm. Solder reaction layer 816c may be a “partner” layer with solder alloy 810 as the thickness of solder reaction layer 816c may be selected so that during the solder process it does not dissolve completely in solder alloy 810.
The multilayer system may include oxidation protection layer 816d to prevent oxidation of the solder reaction layer 816c as solder reaction layers 816c including silver, gold, platinum, palladium or alloys thereof, may be prone to oxidation. Oxidation protection layer 816d may have a thickness ranging from 50 nm to 1000 nm.
Substrate 802 may be formed from one of the following group of materials: copper, nickel, silver or a ceramic. Plating 806 may be formed over substrate 802, e.g. substrate 802 may be a lead frame wherein lead frame plating may be formed over the lead frame. Plating 806 may include at least one from the following group of materials: silver, gold, nickel, platinum, palladium, vanadium, molybdenum, tin, copper, arsenic, antimony, gallium, zinc, aluminum, niobium, tantalum, phosphorus, silver, nickel, nickel phosphorus in elemental form and/or in nitride form and/or in oxide form, the at least one from said group of materials, individually, or in combination. Plating 806 may be configured to be in connection with solder alloy 810.
According to various aspects, substrate 802 may include plating 806 including copper in combination with nickel and/or nickel phosphorus, wherein plating 806 may be a lead frame plating configured to be in connection with the solder alloy. According to various aspects, plating 806 thickness may lie in the range from about 100 nm to about 3 μm.
According to various aspects, chip 814 may include chip back side 820 including at least one from the following group of materials: aluminum, titanium, nickel vanadium, silver, wherein chip back side 820 may be configured to be in connection with solder alloy 810.
Solder alloy 810A according to various aspects may include zinc, aluminum, magnesium and gallium, wherein aluminum constitutes by weight 8% to 20% of alloy 810A, magnesium constitutes by weight 0.5% to 20% of alloy 810A and gallium constitutes by weight 0.5% to 20% of alloy 810A, the rest of alloy 810A including zinc. Solder alloy 810A may be represented by the chemical formula ZnAl4.5Ga1Mg1. Solder alloy 810A may be represented by the chemical formula ZnAl12Ga1Mg1. According to various aspects, solder alloy 810A may be a solder wire. Aluminum may constitute by weight 3% to 12% of alloy 810A. Magnesium may constitute by weight 0.5% to 4% of alloy 810A. Gallium may constitute by weight 0.5% to 4% of alloy 810A.
Solder alloy 810B according to various aspects may include zinc, aluminum, tin and magnesium, wherein aluminum constitutes by weight 1% to 30% of alloy 810B, magnesium constitutes by weight 0.5% to 20% of alloy 810B and tin constitutes by weight 0.5% to 6.5% of alloy 810B, the rest of alloy 810B including zinc. Aluminum may constitute by weight 3% to 8% of alloy 810B. Magnesium may constitute by weight 0.5% to 4% of alloy 810B. Tin may constitute by weight 0.5% to 4% of alloy 810B. Solder alloy 810B may be represented by the chemical formula ZnAl4Sn2Mg1.
Solder alloy 810C according to various aspects may include zinc, aluminum, germanium and gallium, wherein aluminum constitutes by weight 1% to 30% of alloy 810C, germanium constitutes by weight 0.5% to 20% of alloy 810C and gallium constitutes by weight 0.5% to 20% of alloy 810C, the rest of alloy 810C including zinc. Aluminum may constitute by weight 3% to 8% of alloy 810C. Germanium may constitute by weight 0.5% to 4% of alloy 810C. Gallium may constitute by weight 0.5% to 4% of alloy 810C.
Solder alloy 810D according to various aspects may include zinc, aluminum and germanium, wherein aluminum constitutes by weight 1% to 20% of alloy 810D, germanium constitutes by weight 1% to 20% of alloy 810D, the rest of alloy 810D including zinc. Solder alloy 810D may be represented by the chemical formula ZnAl5Ge3. Solder alloy 810D may be represented by the chemical formula ZnAl12Ge3. Solder alloy 810D may be represented by the chemical formula ZnAl6Ge3. Solder alloy may be represented by the chemical formula ZnAl6Ge5. According to various aspects, aluminum may constitute by weight 3% to 8% of alloy 810D. According to various aspects, germanium may constitute by weight 1% to 6% of alloy 810D.
Solder alloy 810E according to various aspects, may include zinc, aluminum and magnesium, wherein aluminum constitutes by weight 1% to 20% of alloy 810E, magnesium constitutes by weight 1% to 20% of alloy 810E, the rest of alloy 810E including zinc. Aluminum may constitute by weight 3% to 8% of alloy 810E. Magnesium may constitute by weight 0.5% to 4% of alloy 810E.
Solder alloy 810F according to various aspects may include zinc and tin, wherein zinc constitutes by weight 10% to 91% of alloy 810F. Solder alloy 810F may be represented by the chemical formula Zn40Sn60. Zinc may constitute by weight 10% to 15% of alloy 810F.
Solder alloy 810G according to various aspects may include zinc and silver, wherein zinc constitutes by weight 26% to 98% of alloy 810G. Zinc may constitute by weight 83% to 99% of alloy 810G.
Solder alloy 810H according to various aspects may include zinc and copper, wherein zinc constitutes by weight 80% to 98% of alloy 810H. Zinc may constitute by weight 88% to 99% of alloy 810H.
According to an aspect, each of solder alloys 810A to 810H may further include at least one from the following group of materials: silver, gold, nickel, platinum, palladium, vanadium, molybdenum, tin, copper, arsenic, antimony, gallium, zinc, aluminum, niobium, tantalum, each and/or in combination including by weight 0.001% to 10% of alloys 810A to 810H.
DSC plot 1236 shows Heat flow (W/g) 1238 versus Temperature (° C.) 1240 with respect to solder alloy 810A having chemical formula ZnAl12Ga1Mg1 according to an aspect. Solder alloy 810A shows exothermic peaks at approximately 273° C., 344° C. Thus, a melting point of approximately 344° C. may be attained in solder alloy 810A having chemical formula ZnAl12Ga1Mg1. The peak representing an enthalpy of 24.4 J/g and peak temperature 272.6° C. reflects a eutectoid reaction between zinc and aluminum. Any further peaks at higher temperatures are created by ternary reactions of Zn—Al with a further alloy element of the alloy, e.g. Ga, Mg.
DSC plot 1436 shows Heat flow (W/g) 1438 versus Temperature (° C.) 1440 with respect to solder alloy 810D having chemical formula ZnAl12Ge3 according to various aspects. Solder alloy 810D shows exothermic peaks at approximately 283° C., 359° C., 368° C. and 412° C. The peak representing an enthalpy of 24.4 J/g and peak temperature 282.8° C. reflects a eutectoid reaction between zinc and aluminum. Any further peaks at higher temperatures are created by ternary reactions of Zn—Al with a further alloy element of the alloy, e.g. Ge.
In various aspects, a solder alloy is provided. The solder alloy may include zinc, aluminum, magnesium and gallium, wherein the aluminum constitutes by weight 8% to 20% of the alloy, the magnesium constitutes by weight 0.5% to 20% of the alloy and the gallium constitutes by weight 0.5% to 20% of the alloy, the rest of the alloy including zinc. In various aspects, the solder alloy may be represented by the chemical formula ZnAl4.5Ga1Mg1. In various aspects, the solder alloy may be represented by the chemical formula ZnAl12Ga1Mg1. In various aspects, the solder alloy may be a solder wire. In various aspects, the aluminum may constitute by weight 3% to 12% of the alloy. In various aspects, the magnesium may constitute by weight 0.5% to 4% of the alloy. In various aspects, the gallium may constitute by weight 0.5% to 4% of the alloy. In various aspects, the alloy may further include at least one from the following group of materials: silver, gold, nickel, platinum, palladium, vanadium, molybdenum, tin, copper, arsenic, antimony, gallium, zinc, aluminum, niobium, tantalum, each and/or in combination including by weight 0.001% to 10% of the alloy.
In various aspects, a solder alloy is provided. The solder alloy may include zinc, aluminum, tin and magnesium, wherein the aluminum constitutes by weight 1% to 30% of the alloy, the magnesium constitutes by weight 0.5% to 20% of the alloy and the tin constitutes by weight 0.5% to 6.5% of the alloy, the rest of the alloy including zinc. In various aspects, the aluminum may constitute by weight 3% to 8% of the alloy. In various aspects, the magnesium may constitute by weight 0.5% to 4% of the alloy. In various aspects, the tin may constitute by weight 0.5% to 4% of the alloy. In various aspects, the solder alloy may be represented by the chemical formula ZnAl4Sn2Mg1. In various aspects, the alloy may further include at least one from the following group of materials: silver, gold, nickel, platinum, palladium, vanadium, molybdenum, tin, copper, arsenic, antimony, gallium, zinc, aluminum, niobium, tantalum, each and/or in combination including by weight 0.001% to 10% of the alloy.
In various aspects, a solder alloy is provided. The solder alloy may include zinc, aluminum, germanium and gallium, wherein the aluminum constitutes by weight 1% to 30% of the alloy, the germanium constitutes by weight 0.5% to 20% of the alloy and the gallium constitutes by weight 0.5% to 20% of the alloy, the rest of the alloy including zinc. In various aspects, the aluminum may constitute by weight 3% to 8% of the alloy. In various aspects, the germanium may constitute by weight 0.5% to 4% of the alloy. In various aspects, the gallium may constitute by weight 0.5% to 4% of the alloy. In various aspects, the alloy may further include at least one from the following group of materials: silver, gold, nickel, platinum, palladium, vanadium, molybdenum, tin, copper, arsenic, antimony, gallium, zinc, aluminum, niobium, tantalum, each and/or in combination including by weight 0.001% to 10% of the alloy.
In various aspects, an arrangement is provided. The arrangement may include a chip; a solder alloy configured to attach the chip to a lead frame; the solder alloy including: zinc, aluminum and germanium, wherein the aluminum constitutes by weight 1% to 20% of the alloy, the germanium constitutes by weight 1% to 20% of the alloy, the rest of the alloy including zinc. In various aspects, the solder alloy may be represented by the chemical formula ZnAl5Ge3. In various aspects, the solder alloy may be represented by the chemical formula ZnAl12Ge3. In various aspects, the solder alloy is represented by the chemical formula ZnAl6Ge3. In various aspects, the solder alloy may be represented by the chemical formula ZnAl6Ge5. In various aspects, the aluminum may constitute by weight 3% to 8% of the alloy. In various aspects, the germanium may constitute by weight 1% to 6% of the alloy. In various aspects, the alloy may further include at least one from the following group of materials: silver, gold, nickel, platinum, palladium, vanadium, molybdenum, tin, copper, arsenic, antimony, gallium, zinc, aluminum, niobium, tantalum, each and/or in combination including by weight 0.001% to 10% of the alloy. In various aspects, the lead frame may include a lead frame plating including at least one from the following group of materials: silver, gold, nickel, platinum, palladium, vanadium, molybdenum, tin, copper, arsenic, antimony, gallium, zinc, aluminum, niobium, tantalum, phosphorus, silver, nickel, nickel phosphorus in elemental form and/or in nitride form and/or in oxide form, the at least one from said group of materials, individually, or in combination including the lead frame plating; wherein the lead frame plating is configured to be in connection with the solder alloy. In various aspects, the lead frame may include a lead frame plating including copper in combination with nickel and/or nickel phosphorus; wherein the lead frame plating is configured to be in connection with the solder alloy. In various aspects, the lead frame plating thickness lies between 100 nm to 3 μm. In various aspects, the chip may include a chip back side including at least one from the following group of materials: aluminum, titanium, nickel vanadium, silver, wherein the chip back side is configured to be in connection with the solder alloy.
In various aspects, an arrangement is provided. The arrangement may include a chip; a solder alloy for attaching the chip to a lead frame; the solder alloy including zinc, aluminum and magnesium, wherein the aluminum constitutes by weight 1% to 20% of the alloy, the magnesium constitutes by weight 1% to 20% of the alloy, the rest of the alloy including zinc. In various aspects, the aluminum may constitute by weight 3% to 8% of the alloy. In various aspects, the magnesium may constitute by weight 0.5% to 4% of the alloy. In various aspects, the alloy may further include at least one from the following group of materials: silver, gold, nickel, platinum, palladium, vanadium, molybdenum, tin, copper, arsenic, antimony, gallium, zinc, aluminum, niobium, tantalum, each and/or in combination including by weight 0.001% to 10% of the alloy. In various aspects, the lead frame may include a lead frame plating including at least one from the following group of materials: silver, gold, nickel, platinum, palladium, vanadium, molybdenum, tin, copper, arsenic, antimony, gallium, zinc, aluminum, niobium, tantalum, phosphorus, silver, nickel, nickel phosphorus in elemental form and/or in nitride form and/or in oxide form, the at least one from said group of materials, individually, or in combination including the lead frame plating; wherein the lead frame plating is configured to be in connection with the solder alloy. In various aspects, the lead frame may include a lead frame plating including copper in combination with nickel and/or nickel phosphorus; wherein the lead frame plating is configured to be in connection with the solder alloy. In various aspects, the lead frame plating thickness lies between 100 nm to 3 μm. In various aspects, the chip may include a chip back side including at least one from the following group of materials: aluminum, titanium, nickel vanadium, silver; wherein the chip back side is configured to be in connection with the solder alloy.
In various aspects, an arrangement is provided. The arrangement may include a chip; a solder alloy configured to attach the chip to a lead frame; the solder alloy including zinc and tin, wherein the zinc constitutes by weight 10% to 91% of the alloy. In various aspects, the solder alloy may be represented by the chemical formula Zn40Sn60. In various aspects, the zinc may constitute by weight 10% to 15% of the alloy. In various aspects, the alloy may further include at least one from the following group of materials: silver, gold, nickel, platinum, palladium, vanadium, molybdenum, tin, copper, arsenic, antimony, gallium, zinc, aluminum, niobium, tantalum, each and/or in combination including by weight 0.001% to 10% of the alloy. In various aspects, the lead frame may include a lead frame plating including at least one from the following group of materials: silver, gold, nickel, platinum, palladium, vanadium, molybdenum, tin, copper, arsenic, antimony, gallium, zinc, aluminum, niobium, tantalum, phosphorus, silver, nickel, nickel phosphorus in elemental form and/or in nitride form and/or in oxide form, the at least one from said group of materials, individually, or in combination including the lead frame plating; wherein the lead frame plating is configured to be in connection with the solder alloy. In various aspects, the lead frame may include a lead frame plating including copper in combination with nickel and/or nickel phosphorus; wherein the lead frame plating is configured to be in connection with the solder alloy. In various aspects, the lead frame plating thickness lies between 100 nm to 3 μm. In various aspects, the chip may include a chip back side including at least one from the following group of materials: aluminum, titanium, nickel vanadium, silver; wherein the chip back side is configured to be in connection with the solder alloy.
In various aspects, an arrangement is provided. The arrangement may include a chip; a solder alloy configured to attach the chip to a lead frame; the solder alloy including zinc and silver, wherein the zinc constitutes by weight 26% to 98% of the alloy. In various aspects, the zinc may constitute by weight 83% to 99% of the alloy. In various aspects, the alloy may further include at least one from the following group of materials: silver, gold, nickel, platinum, palladium, vanadium, molybdenum, tin, copper, arsenic, antimony, gallium, zinc, aluminum, niobium, tantalum, each and/or in combination including by weight 0.001% to 10% of the alloy. In various aspects, the lead frame may include a lead frame plating including at least one from the following group of materials: silver, gold, nickel, platinum, palladium, vanadium, molybdenum, tin, copper, arsenic, antimony, gallium, zinc, aluminum, niobium, tantalum, phosphorus, silver, nickel, nickel phosphorus in elemental form and/or in nitride form and/or in oxide form, the at least one from said group of materials, individually, or in combination including the lead frame plating; wherein the lead frame plating is configured to be in connection with the solder alloy. In various aspects, the lead frame may include a lead frame plating including copper in combination with nickel and/or nickel phosphorus; wherein the lead frame plating is configured to be in connection with the solder alloy. In various aspects, the lead frame plating thickness lies between 100 nm to 3 nm. In various aspects, the chip may include a chip back side including at least one from the following group of materials: aluminum, titanium, nickel vanadium, silver; wherein the chip back side is configured to be in connection with the solder alloy.
In various aspects, an arrangement is provided. The arrangement may include a chip; a solder alloy configured to attach the chip to a lead frame; the solder alloy including zinc and copper, wherein the zinc constitutes by weight 80% to 98% of the alloy. In various aspects, the zinc may constitute by weight 88% to 99% of the alloy. In various aspects, the alloy may further include at least one from the following group of materials: silver, gold, nickel, platinum, palladium, vanadium, molybdenum, tin, copper, arsenic, antimony, gallium, zinc, aluminum, niobium, tantalum, each and/or in combination including by weight 0.001% to 10% of the alloy. In various aspects, the lead frame may include a lead frame plating including at least one from the following group of materials: silver, gold, nickel, platinum, palladium, vanadium, molybdenum, tin, copper, arsenic, antimony, gallium, zinc, aluminum, niobium, tantalum, phosphorus, silver, nickel, nickel phosphorus in elemental form and/or in nitride form and/or in oxide form, the at least one from said group of materials, individually, or in combination including the lead frame plating; wherein the lead frame plating is configured to be in connection with the solder alloy. In various aspects, the lead frame may include a lead frame plating including copper in combination with nickel and/or nickel phosphorus; wherein the lead frame plating is configured to be in connection with the solder alloy. In various aspects, the lead frame plating thickness lies between 100 nm to 3 μm. In various aspects, the chip may include a chip back side including at least one from the following group of materials: aluminum, titanium, nickel vanadium, silver; wherein the chip back side is configured to be in connection with the solder alloy.
While the invention has been particularly shown and described with reference to specific aspects, it should be understood by those skilled in the art that various changes in form and detail may be made therein without departing from the spirit and scope of the invention as defined by the appended claims. The scope of the invention is thus indicated by the appended claims and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced.
This is a continuation of U.S. application Ser. No. 15/659,670 filed on Jul. 26, 2017, which is a continuation of U.S. application Ser. No. 13/154,523 filed on Jun. 7, 2011 (issued as U.S. Pat. No. 9,735,136), the contents of which are all incorporated by reference in their entirety.
Number | Date | Country | |
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Parent | 15659670 | Jul 2017 | US |
Child | 17149741 | US | |
Parent | 13154523 | Jun 2011 | US |
Child | 15659670 | US |