TRANSIENT LIQUID PHASE BONDING COMPOSITIONS AND POWER ELECTRONICS ASSEMBLIES INCORPORATING THE SAME
20190078212 ยท 2019-03-14
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
H01L23/373
ELECTRICITY
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. A transient liquid phase (TLP) composition comprising: a plurality of first high melting temperature (HMT) particles, wherein each of the plurality of first HMT particles comprise a core-shell structure with a core formed from a first HMT material and a shell formed from a second HMT material; a plurality of second HMT particles, wherein each of the plurality of second HMT particles are formed from a third HMT material; a plurality of low melting temperature (LMT) particles, wherein each of the plurality of LMT particles are formed from a LMT material; wherein the first HMT material, the second HMT material, and the third HMT material have a melting point greater than a TLP sintering temperature of the TLP composition and the plurality of LMT particles have a melting point less than the TLP sintering temperature.
2. The TLP composition of claim 1, wherein the first HMT material is nickel, silver, copper, aluminum, or an alloy thereof.
3. The TLP composition of claim 1, wherein the second HMT material is nickel, silver copper or an alloy thereof.
4. The TLP composition of claim 1, wherein the third HMT material is nickel, silver, copper, aluminum, or an alloy thereof.
5. The TLP composition of claim 1, wherein the LMT material is tin, indium, or an alloy thereof.
6. The TLP composition of claim 1, wherein a concentration of the LMT material in the TLP composition is between about 25 weight % and about 75 weight %.
7. The TLP composition of claim 1, wherein the core of the plurality of first HMT particles comprise a graded average diameter along a thickness of a TLP bonding layer formed from the TLP composition.
8. A power electronics assembly comprising: a semiconductor device extending across a metal substrate; and a transient liquid phase (TLP) bond layer disposed between the semiconductor device and the metal substrate, the TLP bond layer comprising a plurality of first high melting temperature (HMT) particles, a plurality of second HMT particles, and a TLP intermetallic layer positioned between and TLP bonding together the plurality of first HMT particles, the plurality of second HMT particles, the semiconductor device and the metal substrate, wherein: each of the plurality of first HMT particles comprise a core formed from a first HMT material and a shell formed from a second HMT material; each of the plurality of second HMT particles is formed from a third HMT material; the first HMT material, the second HMT material, the third HMT material and the TLP intermetallic layer have a melting point greater than a TLP sintering temperature for the TLP bond layer.
9. The power electronics assembly of claim 8, wherein the TLP bond layer has a graded stiffness along a thickness of the TLP bond layer.
10. The power electronics assembly of claim 8, further comprising localized stiffness variations at locations where the plurality of first HMT particles are positioned within the TLP bond layer.
11. The power electronics assembly of claim 8, wherein the plurality of first HMT particles within the TLP bond layer have a graded average diameter along a thickness of the TLP bond layer.
12. The power electronics assembly of claim 8, wherein the TLP bond layer has a graded density of the plurality of first HMT particles along a thickness of the TLP bond layer.
13. The power electronics assembly of claim 8, wherein the first HMT material is nickel, silver, copper, aluminum, or an alloy thereof.
14. The power electronics assembly of claim 8, wherein the second HMT material is nickel, copper, silver or an alloy thereof.
15. The power electronics assembly of claim 8, wherein the third HMT material is nickel, silver, copper, aluminum, or an alloy thereof.
16. The power electronics assembly of claim 8, wherein the TLP intermetallic layer comprises tin.
17. The power electronics assembly of claim 8, wherein an average diameter of the core of the plurality of first HMT particles is between about 10.0 m and about 50.0 m, an average thickness of the shell of the plurality of first HMT particles is between about 0.5 m and about 15 m, and an average diameter of the plurality of second HMT particles is between about 5m and 50 m.
18. A process for manufacturing a power electronics assembly comprising: positioning a transient liquid phase (TLP) bonding layer between a metal substrate and a semiconductor device to provide a metal substrate/semiconductor device assembly, the TLP bonding layer comprising a plurality of first high melting temperature (HMT) particles, a plurality of second HMT particles, and a plurality of low melting temperature (LMT) particles, wherein: each of the plurality of first HMT particles comprise a core-shell structure with a core formed from a first HMT material and a shell formed from a second HMT material; each of the plurality of second HMT particles is formed from a third HMT material; each of the plurality of LMT particles is formed from a LMT material; heating the metal substrate/semiconductor device assembly to a TLP sintering temperature and forming a TLP bond layer between the metal substrate and the semiconductor device, wherein: the first HMT material, the second HMT material and the third HMT material have a melting point above the TLP sintering temperature; and the LMT material has a melting point below the TLP sintering temperature such that the plurality of LMT particles at least partially melt and form a TLP intermetallic layer between the plurality of first HMT particles, the plurality of second HMT particles, the metal substrate, and the semiconductor device.
19. The process of claim 18, wherein the TLP bond layer comprises a graded stiffness between the metal substrate and the semiconductor device.
20. The process of claim 18, wherein the plurality of first HMT particles within the TLP bond layer have a graded average diameter along a thickness of the TLP bond layer.
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]
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[0014]
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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=202.510.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=17.6910.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 m. For example, the core 132c may have an average diameter dl greater than 5 m, greater than 10 m, greater than 15 m, greater than 20 m, greater than 25 m, greater than 35 m, greater than 50 m, greater than 75 m, greater than 100 m, or greater than 150 m, and less than 400 m, less than 300 m, less than 250 m, less than 200 m, less than 150 m, or less than 100 m. In embodiments, the core 132c has an average diameter dl between about 10 m and about 150 m. For example, the core 132c may have an average diameter dl between about 10 m and about 100 m. In some embodiments, the core 132c may have an average diameter d1 between about 10 m and 50 m. The thickness t of the shell 132s may be between about 0.2 m and about 20 m. For example, the thickness t of the shell 132s may be greater than 0.2 m, greater than 0.5 m, greater than 1.0 m, greater than 2.5 m, greater than 5.0 m, greater than 10 m, or greater than 15 m, and less than 20 m, less than 17.5 m, less than 15 m, less than 10 m, or less than 7.5 m. In embodiments, the thickness t of the shell 132s is between about 0.5 m and 20 m. In such embodiments, the thickness t of the shell 132s may be between about 0.5 m and 15 m.
[0038] The average diameter d2 of the second HMT particles 134 may be between about 5 m and about 400 m. For example, the average diameter d2 may be greater than 5 m, greater than 10 m, greater than 15 m, greater than 20 m, greater than 25 m, greater than 35 m, greater than 50 m, greater than 75 m, greater than 100 m, or greater than 150 m, and less than 400 m, less than 300 m, less than 250 m, less than 200 m, less than 150 m, or less than 100 m. In embodiments, the second HMT particles 134 have an average diameter d2 between about 5 m and about 150 m. For example, the second HMT particles 134 may have an average diameter d2 between about 5 m and 100 m. In some embodiments, the second HMT particles 134 may have an average diameter d2 between about 5 m and 50 m.
[0039] The average diameter d3 of the LMT particles 136 may be between about 5 m and about 200 m. For example, the average diameter d3 may be greater than 5 m, greater than 10 m, greater than 15 m, greater than 20 m, greater than 25 m, greater than 50 m, greater than 75 m, greater than 100 m, or greater than 150 m, and less than 200 m, less than 150 m, less than 100 m, or less than 75 m. In embodiments, the LMT particles 136 have an average diameter d3 between about 10 m and 150 m. For example, the LMT particles 136 may have an average diameter d3 between about 15 m and 100 m. In some embodiments, these LMT particles 136 may have an average diameter d3 between about 25 m and 75 m.
[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 (m) and about 200 m. In embodiments, the TLP bond layer 130 has a thickness between about 50 m and about 150 m. In other embodiments, the TLP bond layer 130 has a thickness between about 75 m and 125 m, for example a thickness of 100 m.
[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.