• DocumentCode
    2072079
  • Title

    Prognostication of latent damage and residual life in leadfree electronics subjected to multiple thermal-environments

  • Author

    Lall, Pradeep ; More, Vikrant ; Vaidya, Rahul ; Goebel, Kai

  • Author_Institution
    Dept. of Mech. Eng., Auburn Univ., Auburn, AL
  • fYear
    2009
  • fDate
    26-29 May 2009
  • Firstpage
    1381
  • Lastpage
    1392
  • Abstract
    Electronic assemblies deployed in harsh environments may be subjected to multiple thermal environments during the use-life of the equipment. Often the equipment may not have any macro-indicators of damage such as cracks or delamination. Quantification of thermal environments during use-life is often not feasible because of the data-capture and storage requirements, and the overhead on core-system functionality. There is need for tools and techniques to quantify damage in deployed systems in absence of macro-indicators of damage without knowledge of prior stress history. The presented PHM framework is targeted towards high reliability applications such as avionic and space systems. In this paper, Sn3.0Ag0.5Cu alloy packages have been subjected to multiple thermal cycling environments including -55 to 125C and 0 to 100C. Assemblies investigated include area-array packages soldered on FR4 printed circuit cards. The methodology involves the use of condition monitoring devices, for gathering data on damage pre-cursors at periodic intervals. Damage-state interrogation technique has been developed based on the Levenberg-Marquardt Algorithm in conjunction with the micro structural damage evolution proxies. The presented technique is applicable to electronic assemblies which have been deployed on one thermal environment, then withdrawn from service and targeted for redeployment in a different thermal environment. Test cases have been presented to demonstrate the viability of the technique for assessment of prior damage, operational readiness and residual life for assemblies exposed to multiple thermo-mechanical environments. Prognosticated prior damage and the residual life show good correlation with experimental data, demonstrating the validity of the presented technique for multiple thermo-mechanical environments.
  • Keywords
    RoHS compliance; avionics; copper alloys; life testing; reliability; silver alloys; soldering; thermal stress cracking; tin alloys; FR4 printed circuit card; Levenberg-Marquardt algorithm; PHM framework; SnAgCu; electronic assemblies; harsh environments; latent damage; leadfree electronics; residual life; temperature 218.15 K to 398.15 K; thermal cycling; thermo mechanical environment; Aerospace electronics; Assembly; Delamination; Electronic packaging thermal management; History; Lead; Printed circuits; Prognostics and health management; Thermal stresses; Thermomechanical processes;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Electronic Components and Technology Conference, 2009. ECTC 2009. 59th
  • Conference_Location
    San Diego, CA
  • ISSN
    0569-5503
  • Print_ISBN
    978-1-4244-4475-5
  • Electronic_ISBN
    0569-5503
  • Type

    conf

  • DOI
    10.1109/ECTC.2009.5074193
  • Filename
    5074193