Proceedings of IPACK2005 Proceedings of IPACK2005 ASME InterPACK ‘05 ASME InterPACK '05 July 17-22, San Francisco, California, USA July 17-22, San Francisco, California, USA IPACK2005-73018 InterPack2005-73018 REDESIGNS OF HSOP PACKAGE FOR HIGH POWER CONSUMPTION BASED ON THE NUMERICAL THERMAL SIMULATION ANALYSIS Jinfa Chen Department of Technology Management Kao Yuan Institute of Technology Kaohsiung, Taiwan John Chia Department of Technology Management Kao Yuan Institute of Technology Kaohsiung, Taiwan Keywords: FEM, Thermal Analysis, Multilayer Design, HSOP, DOE ABSTRACT A Heat Slug Outline Package (HSOP) with different design concepts to improve its thermal performance is investigated. The thermal performance of the standard designs of TSSOP usually could not pass the requirements for greater functional integration in wireless frquency and reduction in power consumption, e.g. for a radio frequency (RF) front-end IC’s in silicon its power consumption can be increased about twice when the design frequency increases from 2.0 GHz to 3.5 GHz. The configuration of HSOP28 proposed here is redesigned based on the Thin Shrink Small Outline Package (TSSOP) that is a plastic encapsulated semiconductor device complied with a standard Surface Mount Technology (SMT). In order to accommodate a chip with the same size but double it power consumption, various types of lead frame design for HSOP packages are studies. It is therefore an object of the present study to investigate what will be the maximum thermal improvement of HSOP package compared to the corresponding same size of TSSOP package, which is also related to further reliability issue of this type of IC package, i.e. the thermal fatigue life calculation. Studies presented here are also taken into account the thermal performance of HSOP package associated with different multi-layers PCB designs and the thermal conductivity variations, where the package internal heat conduction as function of board thermal conductivity can be made. INTRODUCTION The configuration of thin shrink small outline package (TSSOP) is a plastic encapsulated semiconductor device. It comprises a die pad, die pad support pins suspending the die pad, and an IC chip mounted on the die pad. Thin metal wire is then utilized for connecting the electrode of the IC chip to leads. A sealing resin is used for sealing the whole components, in which the perimeter of leads are trimmed and formed, and can be soldered directly to the PCB to provide the direct electrical and heat paths (Lau and Lee, 1999). The TSSOP package is usually used in many low lead-count applications involving surface mount packages for RFIC. The thermal performance of TSSOP packages has required to increase it power consumption, but not allowable junction temperatures. This offers significant challenges to package designers in thermal reliability concerns with a newer package structure and smaller geometry in complying with the current SMT (Barcohen, Watwe and Seetharamu, 2001). Thermal resistance analysis of TSSOP package is a quick way and is most often used to determine package thermal characterization in an attempt to account for end-use environments. In addition to laboratory measurement, the thermal resistance of TSSOP package involves geometry, material and IC power variations, all of which are calculated differently and current can be estimated accurately by dedicated finite element analysis (FEA). In this study, the thermal resistance of HSOP28 compared to TSSOP42 package with different lead-frame designs follow instructions specified in MIL-STD-833 Method 1012.1, EIA/JESD 51-3, and EIA/JESD 51-7 and are examined by different thickness of multi-layers PCB designs with thermal conductivity variations. The thermal performance of HSOP packages in high precision power applications is required to maximize it power consumption while decreasing the package size, but the increase of junction temperatures is not allowable. The thermal performance of the standard designs of TSSOP usually couldn't pass the common industrial requirement for high power dissipation, especially, for applications such as higher frequencies of RF devices. This offers significant challenges to package designers in thermal reliability concerns with a newer package structure and smaller geometry (Kamath and Tummala, 2001). Here thermal analysis of HSOP package and the Junction-to-Ambient θJA is used as a quick way to determine package thermal characterization in an attempt to account for the end-user environments. REDESIGN OF PACKAGE CONFIGURATION In order to accommodate higher power chip and increase the package heat dissipation without much change in current 1 Copyright © 2005 by ASME TSSOP package configuration that complies with a standard Surface Mount Technology (SMT), there are 7 dummy leads were welded together with the die pad to form a wing at the sides which function as a heat slug. The variations of width of the die pad wing welded with the lead section are given in a range of 2.6~4.4 mm. Figure 1 shows the details outline drawings of lead frame illustration for TSSOP42 and two HSOP28 package designs. The finite element models of TSSOP42 and HSOP28 are then created based on the package outline specifications for the thermal analysis. 0.350 0.350 0.800 0.800 8.000 8.000 7.500 7.500 2.800 2.800 4.388 6X0.8+0.35=5.150 18.500 18.500 0.350 0.800 7.500 8.000 2.800 2.575 Unless Otherwise Specified Unit International Semiconductor Technology LTD. Scale mm 15 : 1 Package Code HSOP42(2.8X8.0) Material C194 FH Tolerance Drawn Checked Approved Copper foil Proj 飛信半導體股份有限公司 General Roughness Drawing No MULTI-LAYERS OF PCB DESIGN ALTERNATIVES It is known that not only the geometry of package but also the design of printed circuit board (PCB) will greatly influence how much the heat is transferred to the PCB and away from the chip (Romm and Purdom, 1999; Chia and Yang, 2003). Here we provide a series of package thermal data based on different test-board PCB profiles and designs, the package heat flow path as a function of board thermal conductivity is included in the numerical model. Therefore, meaningful comparisons of package thermal data between suppliers can be made by our thermal analysis. The drawings shown in Figure 2 represent one of three types of multi-layer PCB designs in our Design of Experiment (DOE) simulations. The build-up thickness for these three types of multi-layer PCB is proposed by 1.6mm, 1.0 mm and 0.6 mm; respectively. The copper mass per unit area range is specified in the JEDC and IEC publications. Here, for external layers a copper foil with a mass of 152 g/m2 (thickness 18 µm) thickness, whereas 35 µm thickness for internal layers is adopted in our analysis. The area percentage of copper trace layout design in density is assumed to be a range of 20% ~ 50%. 18 um .25 mm 35 um Rev 6x0.8+0.35=5.150 Dimension ± 0.025 By Jemi Wu Date 09-06-00' 1 18.500 Angle ± 30' Sheet 1 of 1 Size A4 18 um 0.15 mm Figure 1 TSSOP42 (upper right) and HSOP28 Package Outline Drawings 35 um 1.0 mm 18 um 0.15 mm 35 um 0.6 mm THERMAL PROPERTIES OF MATERIAL ASSEMBLIES The materials involved a thermal computation, which are the package assembly composition and an EIA standard PCB, have different thermal properties. At present study, through the collection and analysis of historical data, only the properties are sensitive to thermal resistance computation is listed in Table 1. It is well known that silicon thermal conductivity can be highly temperature dependent. However, for simplicity, a temperature dependence of chip thermal conductivity was not included in current study. Table 1 Material Properties of HSOP/TSSOP Package Assembly Conductivity Material (W/ mm oC) Chip 1.48x10-1 Glue 1.10x10-3 Leadframe 1.70x10-1 Molding 5.86x10-4 Solder 5.06x10-2 Copper Foil 3.89x10-1 FR4 3.50x10 -4 0.2 mm 35 um 35 um .25 mm 0.15 mm 35 um 0.15 mm 18 um 18 um 0.6 mm 1.0 mm 1.6 mm 18 um Figure 2 Four Layers of PCB Build-up Designs (t=1.6mm, 1.0mm and 0.6mm) TAGUCHI ORTHOGONAL ARRAY FOR SIMULATIONS Parameters effecting on the thermal performance of package concerned here are the widths of the die pad wing fused with lead section, the number of PCB layers and thickness, the copper mass per unit area, and die size. Each parameter is given three levels of design alternatives. The width of the die pad wing fused with lead section is given 2.6, 3.5 and 4.4 mm. Levels for number of PCB layers are 2, 4 and 6 layers. Levels for the percentage of Cu mass per unit are 20%, 30% and 50%. The three levels of PCB thickness are 1.6 mm, 1.0 mm and 0.6 mm. Table 2 shows 3 different sizes of accommodable IC and their thermal requirements. Table 2 Thermal Resistance Value (θJA) Requirements for HSOP28 θJA Unit: (0C/W) Size of IC θJA for θJA for Chip package Power Tj=125oC Tj=150oC (mmxmm) (W) Requirement Requirement A B C 2 2.76 x 3.33 2.69 x 1.98 3.57 x3.76 2.2 1.7 1.7 34.1 44.1 44.1 45.5 58.8 58.5 Copyright © 2005 by ASME A series of statistical numerical simulations based on the Taguchi’ experimental designs is conducted. There are five parameters with three levels were selected in our design of experiment of numerical simulations. The above conditions necessitate an eighteen trials, i.e. L18 orthogonal array is required to cover all necessary factor variations. However, the variations of the die pad wing fused with lead section given 2.6 ~4.4 mm in width are neglectable compared to other factors, such as the dimension of PCB. Here only four parameters with 3 levels of variation were adopted in our study. A detailed design matrix is reduced to be L9 array and shown in Table 3 (Krottmaier, 1994), which are total eighteen simulations are needed to perform for both HSOP and TSSOP packages. The number of trial is then less required simulations. With these number of parameter combinations, numerical results will not neglect one of the main effects from our concerns. Table 3 Simulation Sequence from Layout of Orthogonal Array, L9 Table 4. Heat Transfer Coefficients on BC surfaces Item Position W/mm2 oC Upper surface 2.98x10-6 PCB Test Board Lower surface 5.96x10-6 Vertical surface 1.93x10-6 Mold Compound Upper surface -5 1.03x10 Vertical surface 3.54x10-5 Typical thermal simulations of a TSSOP package that is direct soldered to PCB are performed as the first trial, where Figure 3(a), (b) and (c) illustrates the temperature distribution of package after computation, can be used for the thermal resistance calculation. A series of thermal resistance values (θJA) of HSOP and TSSOP package are then obtained from numerical simulations. Parameter A B C D Test No. PCB PCB/ Cu Die size /number of thickness Percentage layer 1 1 1 1 1 2 1 2 2 2 3 1 3 3 3 4 2 1 2 3 5 2 2 3 1 6 2 3 1 2 7 3 1 3 2 8 3 2 1 3 9 3 3 2 1 SIMULATION AND RESULT INTERPRETATIONS A steady-state thermal analysis is performed by the commercial code ANSYS. A quarter of TSSOP42 and HSOP28 packages soldered on different PCB designs are modeled and simulated by the analysis. Based the homing-in methods, the chip power consumption and its size given by the IC providers shown in the fifth column of Table 2 are considered to be the last concerning factor. The temperature boundary conditions applied on the surfaces of package and PCB, on which the surfaces adjoining air Tambient, are assumed to be 50 oC. The corresponding temperature B.C. shown in Table 4 is calculated based on natural convection on isothermal heated vertical/ horizontal plate, which is given by (Holman, 1990; Chia and Yang, 2003). (for vertical ) (1) h = Nu ∗ k / H h = N u ∗ k /((W ∗ L) /( 2W + 2 L)) (for face down or up) (2) where N u is the Nusselt Number that is a function of Reynolds Number, Re and the Prandtl number, Pr . k is the conductivity, W and L are the width and length of PCB, respectively. Figure 3 (a) Temperature Distribution of PCB with TSSOP42 (1/4 model) Figure 3 (b) Temperature Distribution of TSSOP42 (1/4 model) 3 Copyright © 2005 by ASME Figure 3 (c) Temperature Distribution of TSSOP42 Leadframe (1/4 model) Figure 4 (a) Temperature Distribution of PCB with HSOP28 (1/4 model) It is our first concern on the PCB designs that can alter the thermal performance of an IC package in use. In our studies, the number of layers of PCB illustrated in Figure 1 was altered from 2 to 6 layers, the copper trace density changed from 20% to 50%, and its thickness was altered from 1.6 mm, 1.0 mm to be 0.6 mm, respectively. It was found that the thermal resistance, θJA is decreased while increasing number of layers of PCB or trace density of PCB. To address the issues of PCB thickness h, and copper trace density d, numerical simulations were performed again by altering the thickness of PCB. Numerical results depict the thinner PCB with a higher copper foil density yields higher thermal effective by a lower thermal resistance value. In order to investigate the thermal improvement of TSSOP, an alternative lead-frame design as HSOP, with respect to same material properties and boundary conditions, in comparison with TSSOP is analyzed under conditions stated above. Figure 4(a) shows a typical temperature distribution of the HSOP package by ANSYS where HSOP is direct soldered to PCB. To look into the temperature distribution of HSOP package and lead frame inside as shown in Figure 4(b) and 4(c) illustrates the redesign of HSOP package can yield better thermal performance than TSSOP, however, simple redesign TSSOP package structure may not fulfill the requirements of thermal value θJA decrease in half. It was found that the thermal performance of package could be significantly changed by the number of layers and thickness of PCB designs. To fulfill such a requirement, an optimum of thermal value θJA for a given package structure that is a function of thickness h, copper trace density d, and number of layers, N was taken into account. Figure 4 (b) Temperature Distribution of HSOP28 (1/4 model) Figure 4 (c) Temperature Distribution of HSOP28 Leadframe (1/4 model) Numerical results computed θJA values of HSOP42 and HSOP28 attached on a multi-layers of PCB from the simulations are typical listed on Tables 5 and 6, where only the 4 Copyright © 2005 by ASME values (θJA) for PCB thickness = 1.6 mm with a range of 20% ~50% copper trace density are given. It can be expected the thinner PCB and higher percentage of copper density will provide the better heat dissipation path in which the lower thermal resistance can be obtained. Table 7 is the summary of simulation results based on the sequences shown on Table 3. The results show that HSOP yields better thermal performance than TSSOP. The parameter D shown in Table 8, the chip size significantly influences the thermal performance of package compared to other parameters in our calculations, where D3 is the smallest die size in design.. Finally, the locations of socket for package mounted on the PCB affecting on thermal performance were considered in our analysis too. Figures 5 (a) and (b) show the results from the socket located on the edge of PCB. It was found that a package at the center of PCB yields the best thermal performance since the PCB can provide the best thermal dissipation path. In our case as shown in Tables 5 and 6, for 30% of copper trace of density the thermal resistance values (θJA) can be decreased from 73.18 to 50.07 for a TSSOP while decreasing from 56.03 to 29.52 for a HSOP if the location of socket is designed from the edge of PCB moving to center of PCB. Table 8 Effects of Individual parameters of DOE simulation Parameter Total Result, θJA Average, θJA TSSOP HSOP TSSOP HSOP PCB layer A1 162.4 90.2 54.1 30.1 A2 142.8 69.7 47.6 23.2 A3 133.9 61.2 44.6 20.4 PCB B1 155.4 84.1 51.8 28.0 thickness B2 150.9 76.2 50.3 25.4 B3 132.7 60.9 44.2 20.3 Cu C1 151.4 80.2 50.5 26.7 percentage C2 148.3 75.7 49.4 25.2 C3 139.3 65.2 46.4 21.7 Die size D1 130.6 67.8 43.5 22.6 D2 220.0 110.8 73.3 36.7 D3 88.4 43.2 29.5 14.4 Table 5 Thermal Resistance Values (θJA) of TSSOP42 (1.6 mm PCB thickness) θJA Unit: (0C/W) Copper Foils 20% 30% 50% 2 lyrs PCB 53.58 50.07/73.18 46.65 4 lyrs PCB 47.68 45.60/67.24 43.72 Table 6 Thermal Resistance Values (θJA) of HSOP28 (1.6 mm PCB thickness) θJA Unit: (0C/W) Copper Foils 20% 30% 50% 2 lyrs PCB 33.70 29.52/56.03 25.40 4 lyrs PCB 27.15 24.59/51.76 22.15 Table 7 Results of Thermal Resistance Values (θJA) based on L9 Orthogonal Array Test No. Parameter, (θJA) of TSSOP42 (θJA) of HSOP28 ABCD 1 1111 53.58 33.70 2 1222 80.86 43.66 3 1333 27.92 12.80 4 2123 31.92 17.21 5 2231 41.53 19.27 6 2312 69.30 33.23 7 3132 69.86 33.14 8 3213 28.54 13.23 9 3321 35.48 14.87 Figure 5 (a) Temperature Distribution of PCB and HSOP with a Socket located at Edge Figure 5 (b) Temperature Distribution of Leadframe with a Socket located at Edge CONCLUSIONS This study based on thermal computation has described thermal improvement of HSOP package design compared to TSSOP that encourage the modification of package design for 5 Copyright © 2005 by ASME higher power IC in complying with standard SMT processing while yielding much cost effective. About 30% ~ 40% reduction in the thermal resistance values of HSOP28 package lower than TSSOP42 with a same size and similar package structure can be obtained. The further improvement of thermal resistance values of HSOP28 package can be obtained when it is soldered on more layers and higher percentage of copper foil area but less thickness of PCB design. The thermal data of HSOP28 package presented here give simple representative thermal performance of the package in use. It significantly depends on the end-user PCB designs and chip size for checking the maximum power dissipation of IC package in field. ACKNOWLEDGMENTS The author gratefully thanks people from Package Development Center, International Semiconductor Tech. for their helps and comments. This paper is based on a research conducted at the IST Package Development Center. REFERENCES Bar-Cohen, A.., A. Watwe and K. 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H., Purdom, “Thermal Characteristics of Linear and Logic Packages using JEDEC PCB Designs,” report SZZA017A, Texas Instruments, 1999. EIA/JESD 51-3, "Low Effective Thermal Conductivity Test Board for Leaded Surface Mount Packages, "1996. EIA/JESD 51-7, "High Effective Thermal Conductivity Test Board for Leaded Surface Mount Packages," 1999. "Plastic Encapsulated Semiconductor Device and Method of Manufacturing the Same," US patent 5,942,794, Aug. 24, 1999. 6 Copyright © 2005 by ASME