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Degradation Mechanism of CuPd Wire in High Temperature Hermetically Sealed Electronics

机译:高温气密密封电子杯丝的降解机理

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There is a big push in the aerospace industry toward more electric aircraft (MEA)[1-2]. The progress is necessary to improve the overall power efficiency and reliability of the aircraft. Aircraft engine health monitoring (EHM) system is one the major effort from aircraft manufacturer toward MEA. This system employs arrays of strategically placed sensors that need to maintain high reliability and robustness under high temperature condition (i.e. 250°C). One key aspect of attaining robust EHM under harsh environment is having high temperature endurable electrical connection using wire bond couple with suitable barrier metallization. Gold (Au) and Aluminum (Al) wire are popular among high temperature electronics packaging solution and development [3-4]. Others employ conformal coating to shield Copper Palladium (CuPd) wires against oxidation from oxygen rich environment at extreme high temperature [5-6]. These are proven solutions for 225 to 250°C high temperature endurable electronics. CuPd wire has made many inroads for IC assembly packaging and this study was initiated to assess whether it could replace Au wire in 250°C high temperature endurable hermetic packages. An approach of using a hermetic (sealing in nitrogen) system in package design with alumina (Al_2O_3) substrate and Au thick film conductor technology and packaged with CuPd wire bond as interconnects has been investigated. The wires were bonded to the test chip using thermosonic wire bonding technology. The reliability test evaluation included Thermal Cycling (TC, -55°C to 225°C, 1000 cycles) and High Temperature Storage (HTS, 250°C, 2000 hours). Hermetic condition did not prevent CuPd wire pull strength from decreasing significantly after 500 hours of HTS and substantial wire resistance increase was observed. Hence, the work indicated that CuPd wire is not suitable as an alternative to Au or Al wire in high temperature hermetic environments due to the oxidative reaction even with low levels of oxygen.
机译:航空航天工业迈向更多电气飞机(MEA)[1-2]。需要提高飞机的总功率效率和可靠性所必需的进展。飞机发动机健康监测(EHM)系统是飞机制造商对MEA的主要努力。该系统采用战略放置的传感器阵列,该传感器需要在高温条件下保持高可靠性和鲁棒性(即250°C)。在恶劣环境下获得稳健EHM的一个关键方面具有使用具有合适阻挡金属化的线键合耦合的高温耐久的电连接。金(AU)和铝(AL)电线在高温电子包装解决方案和开发中受欢迎[3-4]。其他人采用全成形涂层以在极高的高温下屏蔽铜钯(CUPD)电线免受富氧环境的氧化[5-6]。这些方法是225至250°C高温耐久性电子产品的解决方案。 Cupd Wire使IC组装包装的许多进度造成了许多进度,并开始该研究以评估它是否可以在250°C高温耐久的气密包装中取代Au线。已经研究了使用氧化铝(AL_2O_3)衬底和Au厚膜导体技术的包装设计中使用密封(氮气)系统的方法,并用CUPD膜键合作为互连。使用热循环键合技术将电线粘合到测试芯片上。可靠性测试评估包括热循环(Tc,-55°C至225°C,1000个循环)和高温储存(HTS,250°C,2000小时)。在500小时的HTS和大量导线电阻增加后,密封条件并未防止杯子线拉伸强度显着降低。因此,该工作表明,由于氧化反应即使具有低水平的氧气,Cupd Wire不适合于高温气密环境中的Au或Al导线。

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