Effects of basal-plane thermal conductivity and interface thermal conductance on the hot spot temperature in graphene electronic devices

Author:

Choi David1ORCID,Poudel Nirakar2,Cronin Stephen B.2,Shi Li13ORCID

Affiliation:

1. The University of Texas at Austin 1 Department of Mechanical Engineering, , Austin, Texas 78712, USA

2. University of Southern California 2 Department of Electrical Engineering, , Los Angeles, California 90089, USA

3. The University of Texas at Austin 3 Texas Materials Institute, , Austin, Texas 78712, USA

Abstract

Electrostatic force microscopy and scanning thermal microscopy are employed to investigate the electric transport and localized heating around defects introduced during transfer of graphene grown by chemical vapor deposition to an oxidized Si substrate. Numerical and analytical models are developed to explain the results based on the reported basal-plane thermal conductivity, κ, and interfacial thermal conductance, G, of graphene and to investigate their effects on the peak temperature. Irrespective of the κ values, increasing G beyond 4 × 107 W m−2 K−1 can reduce the peak temperature effectively for graphene devices made on sub-10 nm thick gate dielectric, but not for the measured device made on 300-nm-thick oxide dielectric, which yields a cross-plane thermal conductance (Gox) much smaller than the typical G of graphene. In contrast, for typical G values reported for graphene, increasing κ from 300 W m−1 K−1 toward 3000 W m−1 K−1 is effective in reducing the hot spot temperature for the 300-nm-thick oxide devices but not for the sub-10 nm gate dielectric case, because the heat spreading length (l) can be appreciably increased relative to the micron-scale localized heat generation spot size (r0) only when the oxide layer is sufficiently thick. As such, enhancement of κ increases the vertical heat transfer area above the gate dielectric only for the thick oxide case. In all cases considered, the hot spot temperature is sensitive to varying G and κ only when the G/Gox ratio and r0/l ratio are below about 5, respectively.

Funder

National Science Foundation

U.S. Department of Energy

Publisher

AIP Publishing

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