TRANSIENT LIQUID PHASE BONDING COMPOSITIONS AND POWER ELECTRONICS ASSEMBLIES INCORPORATING THE SAME
20210381110 · 2021-12-09
Assignee
Inventors
Cpc classification
H01L2224/48472
ELECTRICITY
H01L2924/00012
ELECTRICITY
B22F2999/00
PERFORMING OPERATIONS; TRANSPORTING
H01L24/00
ELECTRICITY
H01L2924/13091
ELECTRICITY
H01L2224/48139
ELECTRICITY
C22C1/0483
CHEMISTRY; METALLURGY
B22F2999/00
PERFORMING OPERATIONS; TRANSPORTING
B22F2207/17
PERFORMING OPERATIONS; TRANSPORTING
B22F2301/30
PERFORMING OPERATIONS; TRANSPORTING
H01L23/36
ELECTRICITY
H01L2924/00014
ELECTRICITY
B22F1/17
PERFORMING OPERATIONS; TRANSPORTING
H01L2924/00014
ELECTRICITY
H01L2924/00012
ELECTRICITY
H01L2924/10325
ELECTRICITY
B22F2207/11
PERFORMING OPERATIONS; TRANSPORTING
B22F2207/17
PERFORMING OPERATIONS; TRANSPORTING
B22F2207/11
PERFORMING OPERATIONS; TRANSPORTING
B22F7/064
PERFORMING OPERATIONS; TRANSPORTING
B23K35/22
PERFORMING OPERATIONS; TRANSPORTING
H01L24/73
ELECTRICITY
International classification
C23C18/16
CHEMISTRY; METALLURGY
B22F7/06
PERFORMING OPERATIONS; TRANSPORTING
B23K35/22
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A transient liquid phase (TLP) composition includes a plurality of first high melting temperature (HMT) particles, a plurality of second HMT particles, and a plurality of low melting temperature (LMT) particles. Each of the plurality of first HMT particles have a core-shell structure with a core formed from a first high HMT material and a shell formed from a second HMT material that is different than the first HMT material. The plurality of second HMT particles are formed from a third HMT material that is different than the second HMT material and the plurality of LMT particles are formed from a LMT material. The LMT particles have a melting temperature less than a TLP sintering temperature of the TLP composition and the first, second, and third HMT materials have a melting point greater than the TLP sintering temperature.
Claims
1.-24. (canceled)
25. A method, comprising: positioning a TLP bonding layer between a metal substrate and a semiconductor device to form an assembly, the TLP bonding layer comprising first HMT particles, second HMT particles, and LMT particles, wherein: each of the first HMT particles comprise a core-shell structure having a core formed from a first HMT material and a shell formed from a second HMT material, each of the second HMT particles is formed from a third HMT material, and each of the plurality of LMT particles is formed from a LMT material; and heating the assembly to a TLP sintering temperature greater than a melting point of the LMT material to cause the LMT particles to at least partially melt and form a TLP intermetallic layer between the first and second HMT particles, the metal substrate, and the semiconductor device, forming a TLP bond layer between the metal substrate and the semiconductor device having a variation in stiffness of the TLP bond layer.
26. The method of claim 25, wherein, after heating the assembly, the TLP bonding layer has a graded stiffness between the metal substrate and the semiconductor device.
27. The method of claim 25, wherein positioning the TLP bonding layer comprises arranging the first HMT particles within the TLP bonding layer to have a graded average diameter along a thickness of the TLP bonding layer.
28. The method of claim 25, wherein positioning the TLP bonding layer comprises arranging the first HMT particles within the TLP bonding layer to have a graded density along a thickness of the TLP bonding layer.
29. The method of claim 28, wherein positioning the TLP bonding layer further comprises positioning or laying down a plurality of layers of TLP compositions having different quantities of first HMT particles to achieve the graded density along the thickness of the TLP bonding layer.
30. The method of claim 28, wherein positioning the TLP bonding layer to have a graded density further comprises: depositing a first layer comprising a first density of the first HMT particles onto the metal substrate; and depositing a second layer comprising a second density of the first HMT particles onto the first layer.
31. The method of claim 30, wherein a thickness of the first layer is equal to a thickness of the second layer.
32. The method of claim 30, wherein a thickness of the first layer is not equal to a thickness of the second layer.
33. The method of claim 28, wherein positioning the TLP bonding layer to have a graded density further comprises: positioning a first thin foil formed from the LMT material comprising a first density of the first HMT particles and the second HMT particles attached thereto onto the metal substrate; and positioning a second thin foil formed from the LMT material having a second density of first HMT particles and second HMT particles attached thereto onto the first thin foil.
34. The method of claim 33, wherein a thickness of the first thin foil is equal to a thickness of the second thin foil.
35. The method of claim 33, wherein a thickness of the first thin foil is not equal to a thickness of the second thin foil.
36. The method of claim 25, further comprising incorporating the assembly into an inverter circuit.
37. The method of claim 25, wherein: the first HMT material is nickel, silver, copper, aluminum, or an alloy thereof; the second HMT material is nickel, silver, copper, or an alloy thereof; the third HMT material is nickel, silver, copper, aluminum, or an alloy thereof; and the LMT material is tin, indium, or an alloy thereof.
38. A method, comprising: providing a metal substrate; positioning a first thin foil formed from a LMT material comprising a first density of first HMT particles and second HMT particles attached thereto onto the metal substrate, wherein the first HMT particles comprise a core-shell structure having a core formed from a first HMT material and a shell formed from a second HMT material and the second HMT particles are formed from a third HMT material; positioning a second thin foil formed from the LMT material having a second density of first HMT particles and second HMT particles attached thereto onto the first thin foil; placing a semiconductor device over the second thin foil to form an assembly; heating the assembly to a TLP sintering temperature greater than a melting point of the LMT material to cause LMT particles in the LMT material to at least partially melt and form a TLP intermetallic layer between the first and second HMT particles, the metal substrate, and the semiconductor device, thereby forming a TLP bond layer between the metal substrate and the semiconductor device having a variation in stiffness of the TLP bond layer; and incorporating the assembly into an invertor circuit.
39. The method of claim 38, wherein, after heating the assembly, the TLP bonding layer has a graded stiffness between the metal substrate and the semiconductor device.
40. The method of claim 38, wherein positioning the first thin foil and positioning the second thin foil is completed such that the first HMT particles within the TLP bonding layer have a graded average diameter along a thickness of the TLP bond layer resulting therefrom.
41. The method of claim 38, wherein a thickness of the first thin foil is equal to a thickness of the second thin foil.
42. The method of claim 38, wherein a thickness of the first thin foil is not equal to a thickness of the second thin foil.
43. A method, comprising: positioning a TLP bonding layer comprising a first layer having a first density of first HMT particles and a second layer having a second density of the first HMT particles between a metal substrate and a semiconductor device to form an assembly, the TLP bonding layer further comprising second HMT particles and LMT particles, wherein: each of the first HMT particles comprise a core-shell structure having a core formed from a first HMT material and a shell formed from a second HMT material, each of the second HMT particles is formed from a third HMT material, and each of the plurality of LMT particles is formed from a LMT material; heating the assembly to a TLP sintering temperature greater than a melting point of the LMT material to cause the LMT particles to at least partially melt and form a TLP intermetallic layer between the first and second HMT particles, the metal substrate, and the semiconductor device, forming a TLP bond layer between the metal substrate and the semiconductor device having a variation in stiffness of the TLP bond layer; and incorporating the assembly into an invertor circuit.
44. The method of claim 43, wherein, after heating the assembly, the TLP bonding layer has a graded stiffness between the metal substrate and the semiconductor device.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0008] The embodiments set forth in the drawings are illustrative and exemplary in nature and not intended to limit the subject matter defined by the claims. The following detailed description of the illustrative embodiments can be understood when read in conjunction with the following drawings, where like structure is indicated with like reference numerals and in which:
[0009]
[0010]
[0011]
[0012]
[0013]
[0014]
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[0017]
DETAILED DESCRIPTION
[0018]
[0019] Referring initially to
[0020] The thicknesses of the metal substrate 110 and the semiconductor devices 120 may depend on the intended use of the power electronics assembly 100. In one embodiment, the metal substrate 110 has a thickness within the range of about 2.0 mm to about 4.0 mm, and the semiconductor device 120 has a thickness within the range of about 0.1 mm to about 0.3 mm. For example and without limitation, the metal substrate may have a thickness of about 3.0 mm and the semiconductor device 120 may have a thickness of about 0.2 mm. It should be understood that other thicknesses may be utilized.
[0021] The metal substrate 110 may be formed from a thermally conductive material such that heat from the semiconductor devices 120 is transferred to the cooling structure 140. The metal substrate may be formed copper (Cu), e.g., oxygen free Cu, aluminum (Al), Cu alloys, Al alloys, and the like. The semiconductor devices 120 may be formed from a wide band gap semiconductor material suitable for the manufacture or production of power semiconductor devices such as power insulated-gate bipolar transistors (IGBTs), power metal-oxide-semiconductor field-effect transistors (MOSFETs), power transistors, and the like. In embodiments, the semiconductor devices 120 may be formed from wide band gap semiconductor materials including without limitation silicon carbide (SiC), silicon dioxide (SiO.sub.2), aluminum nitride (AlN), gallium nitride (GaN), boron nitride (BN), diamond, and the like. In embodiments, the metal substrate 110 and the semiconductor devices 120 may comprise a coating, e.g., nickel (Ni) plating, to assist in the TLP sintering of the semiconductor devices 120 to the metal substrate 110.
[0022] As depicted in
[0023] The metal substrate 110 is thermally coupled to the cooling structure 140 via a bond layer 138. In one embodiment, the cooling structure 140 comprises an air-cooled heat sink. In an alternative embodiment, the cooling structure 140 comprises a liquid-cooled heat sink, such as a jet impingement or channel-based heat sink device. The metal substrate 110 of the illustrated embodiment is directly bonded to a first surface 142 of the cooling structure 140 via the bond layer 138 without any additional interface layers (e.g., additional metal base plates). The metal substrate 110 may be bonded to the cooling structure 140 using a variety of bonding techniques, such as by TLP sintering, solder, brazing, or diffusion bonding, for example. However, in an alternative embodiment, one or more thermally conductive interface layers may be positioned between the metal substrate 110 and the cooling structure 140.
[0024] Still referring to
[0025] Within the power electronics assembly 100 may be a first electrical contact 104a and a second electrical contact 104b to provide electrical power connections to the semiconductor devices 120. The first electrical contact 104a may correspond to a first voltage potential and the second electrical contact 104b may correspond to a second voltage potential. In the illustrated embodiment, the first electrical contact 104a is electrically coupled to a first surface of the semiconductor devices 120 via a first electrical wire 121a, and the second electrical contact 104b is electrically coupled to a second surface of the semiconductor devices 120 via a second electrical wire 121b and the metal substrate 110. It should be understood that other electrical and mechanical configurations are possible, and that embodiments are not limited by the arrangement of the components illustrated in the figures.
[0026] Referring now to
[0027] The LMT material of the LMT particles 136 has a melting temperature that is lower than that of the first and second HMT materials of the core 132c and shell 132s, respectively, of the first HMT particles 132, and the second HMT particles 134. Accordingly, the embodiment depicted in
[0028] The example TLP composition 130 illustrated in
[0029] In embodiments, the plurality of first HMT particles 132, plurality of second HMT particles 134, and plurality of LMT particles 136 may be configured as loose particles in the form of a powder. In other embodiments, the plurality of first HMT particles 132, plurality of second HMT particles 134, and plurality of LMT particles 136 may be configured as a paste disposed in a binder 139 (
[0030] Example first HMT materials for the core 132c include of the first HMT particles 132, but are not limited to, nickel (Ni), silver (Ag), Cu, aluminum (Al), and alloys thereof. As used herein, the term “alloys thereof” refers to alloys not limited to the elements listed unless otherwise stated. For example, a Ni alloy as disclosed herein may include an alloy formed from Ni and elements other than Ag, Cu, and Al. In the alternative, a Ni alloy as disclosed herein may include an alloy formed from Ni with Ag, Cu, Cu and/or Al, plus additional elements. In another alternative, a Ni alloy as disclosed herein may include an alloy formed from only Ni and Ag, Cu and/or Al plus any incidental impurities present from manufacturing of the Ni alloy. Example second HMT materials for the shell 132s of the first HMT particles 132 include, but are not limited to, Ni, Ag, and alloys thereof. Example HMT materials for the second HMT particles 134 include, but are not limited to, Ni, Ag, Cu, and alloys thereof. It should be understood that the same material should not be chosen for both the core 132c and the shell 132s of the first HMT particles 132. Also, the second HMT particles 134 may be formed from a different HMT material than the shell 132s of the first HMT particles 132. Example LMT materials for the LMT particles 136 include, but are not limited to tin (Sn), indium (In), and alloys thereof
[0031] Any known or yet-to-be-developed technique may be utilized to fabricate the first HMT particles 132 described herein. As non-limiting examples, the first HMT particles 132 described herein may be fabricated from electroplating, electroless plating, and other water-based processes.
[0032] The material for the core 132c of the first HMT particles 132 may be chosen to achieve desirable mechanical properties of the resulting TLP bond layer 130′ following the initial melting of the TLP composition 130. For example, the material for the core 132c may be chosen to reduce the stiffness of the resulting TLP bond layer 130′. As used herein, the term “stiffness” refers to the elastic modulus (also known as Young's modulus) of a material, i.e., a measure of a material's resistance to being deformed elastically when a force is applied to the material. In the alternative, or in addition to, the material for the core 132c may be chosen to increase the ductility of the resulting TLP bond layer 130′ thereby resulting in a less brittle bond between the metal substrate 110 and the semiconductor devices 120. As used herein, the term “ductility” refers to the plastic deformation of a material prior to failure, i.e., a measure of the material's ability to deform plastically without failing when a force is applied to the material. The second HMT particles 134 may be chosen to reduce a thermal expansion of the TLP bond layer 130′ during operation of the power electronics assembly 100 and/or reduce a TLP sintering time for forming the TLP bond layer 130′. For example, the presence of Ni in the Cu—Sn system stabilizes the Cu intermetallic Cu.sub.6Sn.sub.5 as (Cu,Ni).sub.6Sn.sub.5. Particularly, the binary intermetallic Cu.sub.6Sn.sub.5 exhibits an allotropic transformation from a monoclinic crystal structure to a hexagonal crystal structure with an approximate 2% volume expansion at about 186° C., whereas the ternary intermetallic (Cu,Ni).sub.6Sn.sub.5 has a hexagonal crystal structure down to room temperature. Accordingly, there is no volume expansion associated with a change in crystal structure for the ternary intermetallic (Cu, Ni).sub.6Sn.sub.5 when heated to elevated temperatures. Also, the presence of Ni increases the growth kinetics of the TLP intermetallic bonding layer thereby reducing the time for TLP sintering to form the TLP bond layer 130′ that bonds the semiconductor devices 120 to the metal substrate 110. Particularly, diffusion within the ternary (Cu, Ni).sub.6Sn.sub.5 intermetallic (diffusion rate=202.5×10.sup.−19 m.sup.2/s at 150° C.) is about 11 times faster than within the binary Cu.sub.6Sn.sub.5 intermetallic (diffusion rate=17.69×10.sup.−19 m.sup.2/s at 150° C.). Accordingly, the growth kinetics, and thus the TLP sintering time, for the TLP bond layer 130′ may be significantly faster for a TLP bonding layer 131 that includes the second HMT particles 134.
[0033] The TLP compositions 130 described herein may be useful in power electronics applications (e.g., to bond a power semiconductor device to a cooling assembly in an inverter circuit of a hybrid or electric vehicles) because they have a high operating temperature (e.g., greater than 450° C.) and have a ductility (i.e., softness) comparable to traditional tin-based solder. Also, the TLP compositions 130 described herein may reduce the time at a TLP sintering temperature required to form the TLP bond layer 130′ thereby reducing the time the semiconductor devices 120 are exposed to the TLP sintering temperature.
[0034] In one non-limiting example, the first HMT particles 132 comprise a core 132c formed from Al and a shell 132s formed from Ni, the second HMT particles 134 are formed from Cu, and the LMT particles 136 are formed from Sn. In another non-limiting example, the first HMT particles 132 comprise a core 132c formed from Cu a shell 132s formed from Ni, the second HMT particles are formed from Cu, and the LMT particles 136 are formed from Sn. In yet another non-limiting example, the first HMT particles 132 comprise a core 132c formed from Al and a shell 132s formed from Cu, the second HMT particles 134 are formed from Ni, and the LMT particles 136 are formed from Sn.
[0035] The concentration of the LMT particles 136 in the TLP composition 130 may be chosen to achieve a TLP bond layer 130′ with desired mechanical properties as well as a desired re-melting temperature of the intermetallic compound after the initial melting process. The desired concentration of the LMT particles 136 may be achieved by selecting the diameter and thickness of the core 132c and shell 132s, respectively, of the first HMT particles 132, the diameter of the second HMT particles 134, and/or the diameter of the LMT particles 136. Particularly, and referring to
[0036] Referring now to
[0037] The core 132c of the first HMT particles 132 may have an average diameter d1 between about 5 micrometers (m) and about 400 μm. For example, the core 132c may have an average diameter d1 greater than 5 μm, greater than 10 μm, greater than 15 μm, greater than 20 μm, greater than 25 μm, greater than 35 μm, greater than 50 μm, greater than 75 μm, greater than 100 μm, or greater than 150 μm, and less than 400 μm, less than 300 μm, less than 250 μm, less than 200 μm, less than 150 μm, or less than 100 μm. In embodiments, the core 132c has an average diameter d1 between about 10 μm and about 150 μm. For example, the core 132c may have an average diameter d1 between about 10 μm and about 100 μm. In some embodiments, the core 132c may have an average diameter d1 between about 10 μm and 50 μm. The thickness t of the shell 132s may be between about 0.2 μm and about 20 μm. For example, the thickness t of the shell 132s may be greater than 0.2 μm, greater than 0.5 μm, greater than 1.0 μm, greater than 2.5 μm, greater than 5.0 μm, greater than 10 μm, or greater than 15 μm, and less than 20 μm, less than 17.5 μm, less than 15 μm, less than 10 μm, or less than 7.5 μm. In embodiments, the thickness t of the shell 132s is between about 0.5 μm and 20 μm. In such embodiments, the thickness t of the shell 132s may be between about 0.5 μm and 15 μm.
[0038] The average diameter d2 of the second HMT particles 134 may be between about 5 μm and about 400 μm. For example, the average diameter d2 may be greater than 5 μm, greater than 10 μm, greater than 15 μm, greater than 20 μm, greater than 25 μm, greater than 35 μm, greater than 50 μm, greater than 75 μm, greater than 100 μm, or greater than 150 μm, and less than 400 μm, less than 300 μm, less than 250 μm, less than 200 μm, less than 150 μm, or less than 100 μm. In embodiments, the second HMT particles 134 have an average diameter d2 between about 5 μm and about 150 μm. For example, the second HMT particles 134 may have an average diameter d2 between about 5 μm and 100 μm. In some embodiments, the second HMT particles 134 may have an average diameter d2 between about 5 μm and 50 μm.
[0039] The average diameter d3 of the LMT particles 136 may be between about 5 μm and about 200 μm. For example, the average diameter d3 may be greater than 5 μm, greater than 10 μm, greater than 15 μm, greater than 20 μm, greater than 25 μm, greater than 50 μm, greater than 75 μm, greater than 100 μm, or greater than 150 μm, and less than 200 μm, less than 150 μm, less than 100 μm, or less than 75 μm. In embodiments, the LMT particles 136 have an average diameter d3 between about 10 μm and 150 μm. For example, the LMT particles 136 may have an average diameter d3 between about 15 μm and 100 μm. In some embodiments, these LMT particles 136 may have an average diameter d3 between about 25 μm and 75 μm.
[0040] The TLP sintering temperature and for the TLP bonding layer 131 may be between about 200° C. and about 400° C. As a non-limiting example, the TLP sintering temperature is between about 280° C. and about 350° C. and the LMT particles 136 have a melting point less than about 280° C. and the core 132c and shell 132s of the first HMT particles 132, and the second HMT particles 134, have melting points greater than 350° C. For example, the LMT particles 134 may be formed from Sn with a melting point of about 232° C., whereas the core 132c and shell 132s of the first HMT particles 132, and the second HMT particles 134, may be formed from materials such as Cu, Al, silver (Ag), zinc (Zn) and magnesium (Mg) with a melting point of about 1085° C., 660° C., 962° C., 420° C. and 650° C., respectively. Accordingly, the LMT particles 136 at least partially melt and the core 132c and shell 132s of the first HMT particles 132, and the second HMT particles 134, do not melt during TLP sintering of the TLP bonding layer 131.
[0041] Particularly, and referring now to
[0042] While
[0043] Referring now to
[0044] Still referring to
[0045] The TLP bonding layer 131 with first HMT particles 132 having graded average diameters along the thickness of the TLP bonding layer 131 may be formed using known or yet-to-be developed techniques that position or lay down multiple layers of TLP compositions having first HMT particles 132 with different average diameters. One non-limiting example includes additive manufacturing (3D printing), i.e., a first layer 131A containing the first HMT particles 132A is deposited (3D printed) onto the metal substrate 110, a second layer 131B containing the first HMT particles 132B is deposited onto the first layer 131A, and then a third layer 131C containing the first HMT particles 132C is deposited onto the second layer 131B. Another non-limiting example includes positioning a first thin foil formed from the LMT material (not shown) with the first HMT particles 132A and second HMT particles 134 attached thereto onto the metal substrate 110, then positioning a second thin foil formed from the LMT material (not shown) with the first HMT particles 132B and second HMT particles 134 attached thereto onto the first thin foil, and then positioning a third thin foil formed from the LMT material (not shown) with the first HMT particles 132C and second HMT particles 134 attached thereto onto the second thin foil. It should be understood that the arrangement of the first layer 131A, the second layer 131B and the third layer 131C may be different than as depicted in
[0046] Referring now to
[0047] Referring to
[0048] Still referring to
[0049] The TLP bonding layer 131 with a graded density of the first HMT particles 132 along the thickness of the TLP bonding layer 131 may be formed using known or yet-to-be developed techniques that position or lay down multiple layers of TLP compositions having different quantities of first HMT particles 132. One non-limiting example includes additive manufacturing (3D printing), i.e., a first layer 131HD containing a first density of first HMT particles 132 is deposited onto the metal substrate 110 and then a second layer 131LD containing a second density of first HMT particles 132 is deposited onto the first layer 131HD. Another non-limiting example includes positioning a first thin foil formed from the LMT material (not shown) with the first density of first HMT particles 132 and second HMT particles 134 attached thereto onto the metal substrate 110, then positioning a second thin foil formed from the LMT material (not shown) with the second density of first HMT particles 132 and second HMT particles 134 attached thereto onto the first thin foil. It should be understood that the TLP bonding layer 131 may include more than two layers. And the arrangement of the first layer 131HD and second layer 131LD may be different than as depicted in
[0050] The TLP bond layers 130′ described herein compensate for thermally-induced stresses, e.g., thermal cooling stresses, resulting from fabrication (e.g., TLP sintering) and operational conditions (e.g., transient electric loads causing high changes in temperature). Because the metal substrate 110 and semiconductor devices 120 of the power electronics assembly 100 are made of differing materials, differences in the CTE for each material may cause large thermally-induced stresses within the metal substrate 110, semiconductor devices 120 and TLP bond layer 130′. It should be understood that the large thermally-induced stresses may result in failure of the power electronics assembly 100 due to fracturing of the metal substrate 110 or failure of a traditional TLP bonding material (e.g., delamination) between the metal substrate 110 and one or both of the semiconductor devices 120.
[0051] The use of the TLP bond layer 130′ to TLP bond the metal substrate 110 to the semiconductor devices 120 alleviates or mitigates such stresses. That is, the TLP bond layer 130′ described herein compensates for the thermal expansion and contraction experienced by the metal substrate 110 and semiconductor devices 120. In some embodiments, the TLP bond layer 130′ described herein compensates for the thermal expansion and contraction experienced by the metal substrate 110 and semiconductor devices 120 with the plurality of first HMT particles 132 providing localized variation in stiffness and/or ductility between the metal substrate 110 and semiconductor devices 120. In other embodiments, the TLP bond layer 130′ described herein compensates for the thermal expansion and contraction experienced by the metal substrate 110 and semiconductor devices 120 with the TLP bond layer 130′ having a graded stiffness and/or ductility provided by a graded average diameter of the first HMT particles 132 along the thickness (Y-direction) of the TLP bond layer 130′. In still other embodiments, the TLP bond layer 130′ described herein compensates for the thermal expansion and contraction experienced by the metal substrate 110 and semiconductor devices 120 with the TLP bond layer 130′ having a graded stiffness and/or ductility provided by a graded density of the first HMT particles 132 along the thickness of the TLP bond layer 130′. The TLP bond layer 130′, with the variation in localized stiffness and/or ductility or the graded stiffness and/or ductility across its thickness, allows the TLP bond layer 130′ to plastically deform and not delaminate due to the CTE mismatch between the metal substrate 110 and semiconductor devices 120. Also, the TLP bond layer 130′ provides sufficient stiffness such that the semiconductor devices 120 are adequately secured to the metal substrate 110 for subsequent manufacturing steps performed on the semiconductor devices 120. The TLP bond layer 130′ also provides sufficient high temperature bonding strength between the metal substrate 110 and semiconductor devices 120 during operating temperatures approaching and possibly exceeding 200° C.
[0052] Generally, the TLP bond layer 130′ comprises a flat thin layer date. As non-limiting examples, the thickness of the TLP bond layer 130′ may be between about 25 micrometers (μm) and about 200 μm. In embodiments, the TLP bond layer 130′ has a thickness between about 50 μm and about 150 μm. In other embodiments, the TLP bond layer 130′ has a thickness between about 75 μm and 125 μm, for example a thickness of 100 μm.
[0053] As stated above, the metal substrates and power electronics assemblies described herein may be incorporated into an inverter circuit or system that converts direct current electrical power into alternating current electrical power and vice versa depending on the particular application. For example, in a hybrid electric vehicle application as illustrated in
[0054] Power semiconductor devices utilized in such vehicular applications may generate a significant amount of heat during operation, which require bonds between the semiconductor devices and metal substrates that can withstand higher temperatures and thermally-induced stresses due to CTE mismatch. The thermal stress compensation layers described and illustrated herein may compensate for the thermally-induced stresses generated during thermal bonding of the semiconductor devices to the metal substrate and/or operation of the power semiconductor devices with a constant or graded stiffness across the thickness of the thermal stress compensation layers while also providing a compact package design.
[0055] It should now be understood that the multilayer composites incorporated into the power electronics assemblies and vehicles described herein may be utilized to compensate thermally-induced stresses due to CTE mismatch without the need for additional interface layers, thereby providing for a more compact package design with reduced thermal resistance.
[0056] It is noted that the terms “about” and “generally” may be utilized herein to represent the inherent degree of uncertainty that may be attributed to any quantitative comparison, value, measurement, or other representation. This term is also utilized herein to represent the degree by which a quantitative representation may vary from a stated reference without resulting in a change in the basic function of the subject matter at issue.
[0057] While particular embodiments have been illustrated and described herein, it should be understood that various other changes and modifications may be made without departing from the spirit and scope of the claimed subject matter. Moreover, although various aspects of the claimed subject matter have been described herein, such aspects need not be utilized in combination. It is therefore intended that the appended claims cover all such changes and modifications that are within the scope of the claimed subject matter.