Hostname: page-component-74656f9884-rdgjk Total loading time: 0 Render date: 2026-11-08T10:47:49.908Z Has data issue: false hasContentIssue false

Observing and measuring strain in nanostructures and devices with transmission electron microscopy

Published online by Cambridge University Press:  12 February 2014

Martin J. Hÿtch
Affiliation:
CEMES-CNRS, Toulouse; martin.hytch@cemes.fr
Andrew M. Minor
Affiliation:
University of California, Berkeley; aminor@berkeley.edu

Abstract

The evolution of elastic strain engineering in nanostructures and devices requires characterization tools that can be used to not only observe but also quantify the actual strain in a sample, whether this strain is intrinsic or applied. Strain contrast in crystalline samples has always been one of the primary contrast mechanisms used for imaging the microstructure of a material in a transmission electron microscope (TEM). In this regard, TEM is a particularly powerful tool due to its ability to spatially resolve strain information with high precision and spatial resolution. This article reviews the techniques currently available for directly measuring strain in the TEM. Examples are given for measuring strain in semiconductor devices using imaging, diffraction, and holographic techniques. For strain measurement during in situ mechanical testing, two general methods are presented: the conversion of displacement from an actuation device or the direct measurement of strain using image features during deformation.

Information

Type
Research Article
Copyright
Copyright © Materials Research Society 2014 
Figure 0

Table I. Comparison of transmission electron microscopy strain measurement techniques.

Figure 1

Figure 1. Strain mapping with convergent-beam electron diffraction (CBED). (a) Conventional TEM image of a shallow trench isolation (STI) structure, probe positions marked; (b) interpolated map of εxx horizontal strain component in silicon; strain units are ×10–4. Reprinted with permission from Reference 4. © 2003 American Institute of Physics. (c) On-axis high-angle annular dark-field scanning TEM image of a STI structure; (d) tilted zone-axis used for CBED analysis makes the interfaces blurred. Reprinted with permission from Reference 17. © 2005 American Institute of Physics.

Figure 2

Figure 2. Large-angle convergent-beam electron diffraction pattern of a strained-silicon transistor. (a) Bending of the black 4$$\overline 4 $$0 diffraction line in the channel is indicative of strain; (b) corresponding shear component, units of ×10–3. Reprinted with permission from Reference 25. © 2008 Elsevier.

Figure 3

Figure 3. Nano-beam electron diffraction (NBED) experiment: (a) acquisition area; (b) high-angle annular dark-field scanning TEM (HAADF-STEM) and electron diffraction patterns acquired simultaneously during the scan; (c) HAADF-STEM intensity map of the specimen to identify where NBED patterns were acquired; (d) NBED patterns; and (e) resulting strain tensor point by point across the acquisition area. Reprinted with permission from Reference 6. © 2011 Elsevier.

Figure 4

Figure 4. Strain mapping by geometric phase analysis of high-resolution transmission electron microscope (HRTEM) images: (a) HRTEM image of strained-silicon test device, enlarged to show the lattice contrast; (b) strain maps compared with finite element method (FEM) modeling of the thin-film sample; (c) horizontal strain, εxx, as a function of distance from the gate, z, and modeled thin-film and bulk strain. Reprinted with permission from Reference 33. © 2008 American Physical Society. (d) Strain profiles of εxx from a similar type of structure obtained by geometric phase analysis (GPA) of HAADF-STEM images (blue) and extrapolated profile from convergent-beam electron diffraction (CBED) (orange). Reprinted with permission from Reference 36. © 2010 Wiley.

Figure 5

Figure 5. Dark-field electron holography. (a) A diffracted beam from an unstrained region of crystal (in blue) is interfered with the same diffracted beam emanating from the region of interest (in yellow) with the aid of a bi-prism wire (red). Provided the crystal is of uniform thickness, the non-geometric phase terms cancel, or only produce a uniform phase change to a good first approximation, thus yielding the geometric phase component. (b) Typical transistor geometry with reference zone in substrate and active region at the surface. Reprinted with permission from Reference 11. © 2011 Elsevier.

Figure 6

Figure 6. The problem of the scale of strain measurements. (a) Strain map obtained by high-resolution transmission electron microscopy (in color) superimposed on a bright-field image of the full structure (G, gate electrode); (b) strain map obtained by dark-field electron holography (DFEH) of a similar device. Reprinted with permission from Reference 45. © 2013 Wiley. (c) Strain tensor maps obtained by DFEH: experimental strain components (left column) and simulated strain components from finite element method (right column). Reprinted with permission from Reference 10. © 2008 Nature Publishing Group.

Figure 7

Figure 7. Comparison of in situ nanocompression and nanotensile tests of pure Ti. (a) Image of a Ti nanopillar before testing. The pillar is tapered, hence the deformation is inhomogeneous and localized at the top of the pillar, as shown in (b). (c) Gauge section of a nanotensile test before testing. (d) After the nanotensile test. (e) Quantitative data for the two tests, where the nanocompression test is plotted as engineering stress versus displacement and the nanotensile test is plotted as engineering stress versus engineering strain. Courtesy of Q. Yu.

Figure 8

Figure 8. In situ tensile test of a Mo-alloy nanofiber demonstrating the application of digital image correlation to calculate local stress and strain in the deforming volume. (a) TEM micrograph of an 8-µ-long Mo-alloy nanofiber before deformation. (b) Local true stress-strain curve generated using digital image correlation, with a time-series of the local area being analyzed shown along the curve. From left to right: Initial dislocation structure; at 1.56 GPa, a spiral arm source begins to activate and emit dislocations; dislocation structure after load drop; final necked region at 3 GPa after the spiral arm source deactivates. Reprinted with permission from Reference 58. © 2012 Elsevier.