J Mater Sci: Mater Electron (2014) 25:627–634 DOI 10.1007/s10854-013-1478-6 Advanced characterization of mechanical properties of multilayer ceramic capacitors Kun-Yen Chen • Chang-Wei Huang Marklaw Wu • Wen-Cheng J. Wei • Chun-Hway Hsueh • Received: 16 January 2013 / Accepted: 29 August 2013 / Published online: 11 September 2013 Ó Springer Science+Business Media New York 2013 Abstract Characterization of the mechanical properties of small components is a significant issue. For the multilayer ceramic capacitor (MLCC), direct loading by conventional facilities is not suitable because of its small size. To date, the standard method used to determine MLCC’s mechanical properties is board flex test; i.e., mounting the capacitor onto a printed circuit board (PCB) and applying bending to the entire system. Failure is defined as cracking or capacitance loss of the MLCC when the mounted PCB is subjected to a specified deflection, and the measurements are usually performed after the test. In this case, characterization of the mechanical properties of MLCCs is qualitative. The purpose of the present study was to quantitatively characterize the mechanical properties of MLCCs. Specifically, the acoustic emission was used to detect cracking of MLCCs during the board flex test. To confirm cracking-induced acoustic emission, telemicroscope was used to perform the in situ observation of cracking. Finite element analyses were also performed to analyze the stress field resulting from the test to compare with the observed cracking path. In addition, nanoindentation was used to explore the mechanical properties of the constituents of MLCCs in the nanoscale. Our work not only K.-Y. Chen W.-C. J. Wei C.-H. Hsueh (&) Department of Materials Science and Engineering, National Taiwan University, Taipei, Taiwan e-mail: hsuehc@ntu.edu.tw C.-W. Huang Department of Civil Engineering, Chung Yuan Christian University, Taoyuan, Taiwan M. Wu MLCC Specialty R&D Division, Yageo Corporation, Kaohsiung, Taiwan allows identification and understanding of the fracture origin, but also provides guidelines in the material design. 1 Introduction With the miniaturization of commercial electronic products and devices, the sizes of electronic components have become much smaller than ever. Multilayer ceramic capacitor (MLCC) is now an indispensable electronic component because of its characteristics of small volume and high capacitance density [1, 2]. The system consists of alternate layers of dielectric ceramics and metal electrodes sandwiched between two ceramic cover layers and cosintered at high temperatures. After sintering, the component is cooled to room temperature and the end termination electrodes are formed on both sides of the component. The MLCCs are then mounted to the printed circuit board (PCB) by the soldering process. A photo of half of the mounted MLCC is shown in Fig. 1. This surface mounted electronic component must withstand severe environment with vibration and high temperatures [3, 4]. Based on the analysis of Center for Advanced Life Cycle Engineering (CALCE), the capacitors are more responsible for the failure of the system than other components [5]. Therefore, other than the investigation to increase MLCC’s capacitance density, the mechanical properties-related issues of reliability and durability are of great concern [6, 7]. However, characterization of the mechanical properties of small component is a daunting challenge. Because of its small size, direct loading on MLCCs by conventional facilities is infeasible. Because failure of surface mounted MLCCs results mainly from bending of the PCB during the handling and assembly process such as solder reflow, or by the vibration 123 628 Fig. 1 A photo of half of the surface mounted MLCC and shocking in the function environment, the mechanical strength of MLCC to survive a certain deflection that it might experience under manufacturing and functioning is Fig. 2 The schematic diagrams of a board flex test under AECQ200-005 [9] and b four-point bending test under IPC/JEDEC9702 [22] 123 J Mater Sci: Mater Electron (2014) 25:627–634 necessary [5]. The method used to date to determine MLCCs’ mechanical properties is board flex test [8, 9]; i.e., mounting the capacitor onto a PCB that is subjected to bending, and the failure criterion is defined as cracking or the capacitance loss of the MLCC when the board is under a specified deflection. A schematic drawing of the board flex test is shown in Fig. 2a. The observation of flex cracking is a non-trivial problem. Unless the MLCC is sectioned and polished, the crack may not be apparent on the external surface of the MLCC [10]. Also, it has been reported that while cracking causes separation along its path and disconnection of one or more of the electrode plates, the separation may be eliminated and allow the disconnected electrodes to return and connect again upon load removal [8, 11]. Because of this return, it is difficult to test a cracked MLCC for capacitance and insulation resistance after removal of the flex force. To resolve this problem, the purpose of the present study was J Mater Sci: Mater Electron (2014) 25:627–634 629 to perform the in situ detection of flex cracking. Specifically, the telemicroscope and acoustic emission [12–14] were used to perform in situ inspection of cracking when the MLCC was subjected to the board flex test. The crack initiation site was identified and compared to the stress field obtained from the finite element analysis (FEA), and the observed cracking event was correlated to the acoustic emission signal. Furthermore, with the identification of the cracking-induced acoustic emission, cracking of MLCC can be readily detected without in situ observation of cracking for which cutting and polishing of the specimen are required prior to testing. In addition, nanoindentation [15, 16] was performed to explore the mechanical properties of the constituents of MLCCs in the nanoscale. Our work not only allows identification and understanding of the fracture origin in MLCCs, but also provides guidelines in the material design. 1,140 GPa and mi is 0.07. With the Poisson’s ratio of material obtained from the literature, Young’s modulus of the test material can be calculated from Eq. (1) and is listed in Table 1. Young’s moduli obtained elsewhere [17–19] are also listed for comparison. It is worth noting that the PCB is FR4 material, which is a glass fiber-reinforced epoxy composite. As a result, Young’s modulus of PCB obtained from nanoindentation is the surface property; i.e., the property of epoxy matrix. To obtain Young’s modulus of the PCB, three-point bending was performed and Young’s modulus can be calculated from the following equation [20] E¼ I¼ The MLCCs were provided by YAGEO with X7R dielectric type and 1210 size that have a length of 0.12 inch and a width of 0.10 inch. Hysitron TI 950 TriboIndenter Nanomechanical Test Instrument was used to perform nanoindentation in order to obtain the mechanical properties of each constituent of MLCC. Specifically, ten indentations each were performed on the MLCC’s dielectric, inner electrode, end termination, solder, and copper pad, respectively. From the slope of the curve upon unloading, the reduced Young’s modulus, Er, could be obtained. This reduced Young’s modulus is related to Young’s modulus of the test specimen by the following equation 1 1 m2i 1 m2s ¼ þ Er Ei Es ð1Þ where E and v are Young’s modulus and Poisson ratio, and the subscripts i and s denote the indenter tip and the specimen, respectively. For a diamond indenter tip, Ei is Table 1 Material properties of MLCC mounted on PCB ð2Þ where P is the applied force during bending, l is the loading span, d is the bending deflection, and I is the moment of inertia of the cross-sectional area which is given by the following equation [21] 2 Experimental procedure 2.1 Material properties and nanoindentation Pl3 48dI bh3 12 ð3Þ where b and h are, respectively, the width and the height of the rectangular cross section of the PCB. 2.2 Acoustic emission and telemicroscope A lead-free solder, Sn95.5Ag3.8Cu0.7, was used to mount the MLCC at the center of PCB. After assembling, the PCB was subjected to deflection based on IPC/JEDEC standard 9702 by four-point bending [22] and MTS Criterion tabletop test system was used to perform this test. The inner load span was 4 cm and the outer support span was 9 cm. The loading condition used in this study was displacement control with the crosshead moving to a specified displacement at the speed of 0.1 mm/s, holding at the specified displacement for 5 s, and then unloading to origin at the same speed. A schematic drawing of this four-point bending is shown in Fig. 2b. The acoustic emission detector was attached to the PCB during the test. The acoustic emission analog filter frequency was set between Young’s modulus (GPa) This study Franken et al. [17] Park et al. [18] Poisson ratio [17, 19] X7R dielectric 200 91 175 0.25 Internal electrode 167 110 208 0.33 Termination 105 207 128 0.33 Solder 45.3 (Sn95.5Ag3.8Cu0.7) 26.5 (Sn63Pb37) 26.5 (Sn62Pb36Ag2) 0.36 Copper pad 100 131 128 0.33 PCB 17.2 23 – 0.25 123 630 20 kHz and 1 MHz, and the threshold was set at different levels. The contact between the bending fixture and the PCB was lubricated to minimize the frictional stress. Optem Zoom 125 telemicroscope, which has a working distance of 10 cm, was used to perform the in situ observation of cracking of MLCC during the test. A photograph of the experimental setup for in situ cracking observation is shown in Fig. 3. In order to facilitate the observation, the mounted PCB was cut and polished (see Fig. 1 as an example) prior to the test. The observed cracking event was then synchronized with the acoustic emission signals to identify the cracking-induced acoustic emission. To eliminate the acoustic noises from PCB itself during the test, four-point bending was also performed on the PCB without the MLCC. 3 Finite element analysis A simple analytical model has been developed previously to analyze the thermal stress in the MLCC [23]. The stress development in the MLCC during the board flex test has been simulated using the FEA elsewhere [18, 24–28]. Also, a recent finite element study showed that the thermal stress was much smaller than the flexural stress during the board flex test [29]. For simplicity, a two-dimensional planestress FEA model of MLCC was used in the present study and the deformation behavior of the mounted PCB system was assumed to be elastic to study the essential trend of the distribution of the flexural stress resulting from the board flex test. Only half of the system was modeled because of J Mater Sci: Mater Electron (2014) 25:627–634 the symmetric geometry. The material properties listed in Table 1 were adopted in the simulation. Because the nickel electrode is thin compared with other constituents in the MLCC, it is difficult to construct a model with many thin layer electrodes within the dielectric ceramic. Therefore, the rule-of-mixtures was used to calculate the effective elastic properties of the dielectric ceramic/electrode composite, such that [18, 30] E ¼ fd Ed þ fe Ee ð4aÞ m ¼ fd md þ fe me ð4bÞ where f is the volume fraction and the subscripts d and e denote the dielectric ceramic and the electrode, respectively. It should be noted that the dimension of PCB (length 10 cm 9 width 4 cm 9 height 1.6 mm) is much larger than MLCC (0.3048 cm 9 0.254 cm 9 1.085 mm) and it is impractical to simulate the entire system to obtain the accurate stress distribution in the MLCC. Hence, the following methodology was used in the present simulation. First, the twodimensional simulation was performed within the inner loading span that is subjected to a constant moment and has a dimension of 4 cm 9 2.685 mm. In this case, the simulated result in the MLCC is expected to be not sufficiently accurate because of the coarse mesh-size. In the absence of MLCC, the analytical solution for the stress distribution within the inner span of PCB can be obtained, such that rx ¼ My I ð5Þ where rx is the normal stress along the beam length direction, M is the applied bending moment, and y is the distance from the neutral axis. The stress distribution, rx, through the thickness of PCB is linear. In the presence of MLCC, the stress field within PCB is expected to be perturbed in the region surrounding MLCC and, hence, deviates from linearity. Then, a section encompassing the perturbed area was selected and the stress distribution described by Eq. (5) was defined as the loading condition at the edges of the selected section. In this case, the area in simulation is much smaller than the entire system and more accurate simulation result can be obtained for the MLCC. The first principal stress in MLCC obtained from FEA during the board flex test is then compared with the observed cracking. 4 Results and discussion 4.1 Acoustic emission Fig. 3 A photo of the experimental setup for in situ cracking observation 123 With the aid of telemicroscope to perform in situ observation, the crack initiation and its propagation can be inspected. It provides a means to correlate the acoustic J Mater Sci: Mater Electron (2014) 25:627–634 signal to cracking. First, the board flex test was performed on PCB only, the acoustic threshold was set at 28 db, and the acoustic signals were detected. These signals are induced by bending of PCB. The characteristic acoustic waveform of PCB bending is shown in Fig. 4a. The amplitude of the corresponding acoustic signal wave decays in a relatively short time (about 100 microseconds), and its initial amplitude was up to *6 mV. Then, the sample of MLCC mounted on PCB was cut and polished to facilitate the in situ observation of cracking using telemicroscope. The acoustic threshold was set at 28 db initially. In this case, several hits were detected during the test, and the waveforms could be categorized into three kinds. The first has the characteristic acoustic waveform pattern of PCB bending (Fig. 4a). The second is the cracking-induced acoustic signal, which could be identified by the moment of cracking observed by telemicroscope. This cracking-induced acoustic wave has a relatively large amplitude (*10000 mV) as shown in Fig. 4b. The third kind of acoustic wave has an amplitude of *2 mV that is smaller than the previous two, and the associated pattern of the waveform is also very different and is shown in Fig. 4c. The source of this acoustic wave is currently unknown; however, it might result from the deformation and void growth in the solder during bending. Since only the acoustic signal resulting from cracking of MLCC is of significance, other signals could be treated as background noises and should be removed for better characterization of cracking. Therefore, the acoustic threshold was raised to 45 db, and all of the solder-contributed acoustic signals were removed; however, most of the PCB bending-contributed acoustic signals still existed. Therefore, the threshold was then raised to 60 db, and nearly all of the noises were removed. After raising the threshold to 70 db, only the acoustic emission resulting from cracking of MLCC was detected. In order to identify the moment of cracking and to correlate the acoustic signal to cracking, the MLCC samples used for in situ cracking observation using the telemicroscope were all cut and polished. However, for the board flex test in the industrial application, cutting and polishing the sample represent extra steps. Therefore, it would be fruitful if cracking of MLCC during the board flex test could be characterized without cutting and polishing of the specimen. Hence, the board flex test was performed on the pristine MLCC specimen mounted on PCB, the maximum deflection of PCB was set at 4 mm, and the acoustic threshold was set at 70 db. When a hit was detected, the corresponding acoustic waveform was found to have the characteristics of Fig. 4b. The MLCC specimen was then cut and polished and the crack was observed (as shown in Fig. 5 where the crack initiation site is indicated by an arrow). On the other hand, when no acoustic signal 631 Fig. 4 The characteristic acoustic waveform resulting from a PCB bending with a fast decay, b cracking in MLCC with a large amplitude, and c the deformation and void growth in the solder with a small amplitude 123 632 was detected, no crack was observed after cutting and polishing of the MLCC specimen. This confirms that cracking of MLCC during the board flex test could be identified by acoustic emission without cutting and polishing of the specimen. J Mater Sci: Mater Electron (2014) 25:627–634 which the stress field is perturbed in the presence of MLCC can be identified readily. For example, Fig. 6b shows that the stress field in the PCB is unperturbed when its position is 4 mm away from the symmetric axis which is denoted by an arrow. The FEA was then re-run by setting the simulation domain much smaller than the entire system but larger than the 4.2 Finite element analysis The stress fields, rx, of PCB without and with MLCC mounting subjected to a constant bending moment of 3.5 N per unit width are showed, respectively, in Fig. 6a, b. It should be noted that a thin layer (*40 lm) of copper pad is present on the top surface of the PCB which, in turn, results in the redistribution of the stresses at the left edge. The region in Fig. 5 The crack pattern in MLCC subjected to board flex test and the crack initiation site is indicated by an arrow Fig. 6 The stress field, rx, of bending of PCB a in the absence and b in the presence of MLCC mounting 123 Fig. 7 The simulation results for a rx in MLCC/PCB subjected to the board flex test, b detailed principal stress field in MLCC, and c the orientation of the principal stress in MLCC J Mater Sci: Mater Electron (2014) 25:627–634 633 confirmed by the in situ cracking observation using a telemicroscope. Nanoindentation is used to obtain the mechanical properties of MLCC in the nanoscale. Using the FEA, the location of the simulated maximum principal stress agrees with the crack initiation site and the orientation of the first principal stress is also consistent with the observed crack path in MLCC during the board flex test. Also, it was found that reduced stiffness of the PCB shifted the location of the maximum principal stress in MLCC and decreased the magnitude of the maximum principal stress at a fixed deflection of PCB in the test. Acknowledgments This work was supported by National Science Council, Taiwan under Contract No. NSC100-2221-E-002-129 and Yageo Corporation under Contract No. 99-S-A74. Fig. 8 The simulated principal stress contour in MLCC/PCB subjected to the board flex test with underestimated Young’s modulus for the PCB perturbed region to improve the efficiency and accuracy of the simulation results. Adopting the new simulation domain and finer mesh, the simulated rx is shown in Fig. 7a with the details of the first principal stress in the MLCC shown in Fig. 7b when cracking occurs at the deflection of 2.99 mm. The maximum principal stress in the MLCC shown in Fig. 7b is 128 MPa that agrees with Park et al.’s [18] result of *130 MPa. The location of the maximum principal stress in MLCC agrees with the crack initiation site, which is located in the dielectric ceramics at the bottom end of the termination (see Fig. 5) and is indicated by an arrow in Fig. 7b. The orientation of the principal stress is also consistent with the observed crack path as shown in Fig. 7c. It is worth mentioning that Young’s modulus of PCB obtained from nanoindentation is 3.95 GPa, which is much smaller than that obtained from three-point bending, 17.2 GPa. This is because of the glass fiber-reinforced epoxy structure of the PCB and the surface property (i.e., the epoxy matrix) is measured by nanoindentation. Using this underestimated Young’s modulus for PCB in the simulation, the simulated first principal stress is shown in Fig. 8. The maximum first principal stress location is no longer at the bottom end of the termination. Instead, it is located at the side face of MLCC and its magnitude is also smaller (115 MPa in Fig. 8 vs. 128 MPa in Fig. 7b). The effects of other parameters (e.g., electrode number/thickness, solder material/geometry, and lateral margin length, etc.) on the stress distribution in the MLCC during board flex test can also be examined using FEA. 5 Conclusions The acoustic emission system is a powerful tool to detect cracking of MLCC during the board flex test. This is References 1. C.A. Randall, J. Ceram. Soc. Jpn. 109, S2 (2001) 2. H. Kishi, Y. Mizuno, H. Chazono, Jpn. J. Appl. Phys. Part 1 42, 1 (2003) 3. H.A. Post, P. Letullier, T. Briolat, R. Humke, R. Schuhmann, K. Saarinen, W. Werner, Y. Ousten, G. Lekens, A. Dehbi, W. Wondrak, Microelectron. Reliab. 45, 1626 (2005) 4. S.J. Yang, J.W. Kim, D.S. Ryu, M.S. Kim, J.S. Jang, Int. J. Mod. Phys. B 17, 1318 (2003) 5. M. Keimasi, M.H. Azarian, M.G. Pecht, IEEE Trans. Device Mater. Rel. 8, 182 (2008) 6. C.R. Koripella, IEEE Trans. Compon. Hybrids Manuf. Technol. 14, 4 (1991) 7. R. Al-Saffar, R. Freer, I. Tribick, P. Ward, Br. Ceram. Trans. 98, 241 (1999) 8. J. Bergenthal, J.D. Prymak, Capacitance monitoring while flex testing, KEMET Electronics Corporation, F-2110, Aug (1997) 9. Method-005, passive component surface mounted ceramic capacitors board flex test, AEC-Q200-005, Automotive electronics council, Component Technical Committee, 1 June 2010 10. TDK MLCC Application Notes, Common cracking modes in surface mount multilayer ceramic capacitors, Apr 2000 11. J. Prymak, M. Prevallet, P. Blais, B. Long, New improvements in flex capabilities for MLC chip capacitors, in CARTS conference, Orlando, FL, April 3–6, Components Technology Institute, Inc. Huntsville, AL 2006 pp. 1–11 12. I.G. Palmer, P.T. Heald, Mater. Sci. Eng. 11, 181 (1973) 13. H.L. Dunegan, D.O. Harris, C.A. Tatro, Eng. Fracture Mech. 1, 105 (1968) 14. A.G. Evans, M. Linzer, L.R. Russell, Mater. Sci. Eng. 15, 253 (1974) 15. J. Mencik, D. Munz, E. Quandt, E.R. Weppelmann, M.V. Swain, J. Mater. Res. 12, 2475 (1997) 16. S.S. Ryu, H.T. Kim, H.J. Kim, S. Kim, J. Ceram. Soc. Jpn. 117, 811 (2009) 17. K. Franken, H.R. Maier, K. Prume, R. Waser, J. Am. Ceram. Soc. 83, 1433 (2000) 18. J.W. Park, J.H. Chae, I.H. Park, H.J. Youn, Y.H. Moon, J. Am. Ceram. Soc. 90, 2151 (2007) 19. A.S.M. International, Metals Handbook, 2nd edn. (ASM International, Materials Park, OH, 1998), p. 118 20. R.J. Roark, Formulas for Stress and Strain (McGraw-Hill, New York, 1965), p. 112 21. R.C. Hibbeler, Statics and Mechanics of Materials (Prentice Hall, Singapore, 2004), p. 293 123 634 22. IPC/JEDEC-9702, Monotonic Bend Characterization of Board Level Interconnect, June. 2004 23. C.H. Hsueh, M.K. Ferber, Compos. A 33, 1115 (2002) 24. N. Blattau, D. Barker, C. Hillman, Design guidelines for preventing flex cracking failures in ceramic capacitors, CARTS 2003: 23rd Capacitor and resistor technology symposium, pp. 150–162 (2003). 31 March–3 April 2003 25. D. Lau, M. Tsang, S. W. R. Lee, J. Lo, L. Fu, J. Jin, and S. Liu, Experimental testing and computational stress analysis of printed circuit board for the failure prediction of passive components under the depaneling load condition, Electronic 123 J Mater Sci: Mater Electron (2014) 25:627–634 26. 27. 28. 29. 30. Components and Technology Conference 2005 proceedings, pp. 1783–1791 (2005) K. Prume, K. Franken, U. Bottger, R. Waser, H.R. Maier, J. Eur. Ceram. Soc. 22, 1285 (2002) M. Keimasi, M. Azarian, M. Pecht, Microelectron. Reliab. 47, 2215 (2007) G. Sharon, D. Barker, J. Fail. Anal. Prev. 11, 1546 (2011) C.W. Huang, B.T. Chen, K.Y. Chen, C.H. Hsueh, W.C. Wei, C.T. Lee, Inter. J. Appl. Ceram. Technol. (in press) S. Timoshenko, Strength of Materials, 3rd edn. (Krieger, Huntington, NY, 1976), p. 88