Η δονητική φασματοσκοπία και οι μηχανικές μετρήσεις στη νανοτεχνολογία

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1 Η δονητική φασματοσκοπία και οι μηχανικές μετρήσεις στη νανοτεχνολογία Δρ Ι. Παρθένιος Κύριος Ε. Λ. Ε., ITE/IEXMH CNT

2 From macro to nano 25 cm (a) (b) (c) (d) Human Skin Human Cell on Si House Curtains Bilayer Graphene 1μm 25 cm 1 μm (t ~ 0.7 nm) Vandeparre H., et al. PRL, 106, (2011) 0D 1D 2D 3D

3 Various forms of carbon-based nanomaterials P. Ehrenfreund and B. H. Foing, Science 329, 1159 (2010)

4 Mechanical characterization of nanomaterials MWCNT Force = kd ~ nn Strain = δl/l Hard k (soft) Fracture strength: GPa Strain at break: ~12% Young s Modulus: 274 to 954 GPa Yu MF, Lourie O, Dyer MJ, Moloni K, Kelly TF, and Ruoff RS, Strength and breaking mechanism of multiwalled carbon nanotubes under tensile load, Science, 287, (2000).

5 Mechanical characterization of nanomaterials Graphene AFM nanoindentation of graphene membrane Max deflection δ ~ 100 nm The elastic properties and intrinsic breaking strength of defect-free monolayer Breaking strength ~ 42 N/m Young s modulus ~1.0 Tpa Tensile Strength ~ 130 GPa Lee, et al., Science, 321, (2008),

6 Force to break a covalent bond in graphene 1 F Breaking strength deformation 42 Nm nm 6 nn bond It is assumed that the deformation for bond breaking of the C-C bond in graphene is ~ nm Force ~ 65 pn 1N optical tweezers Need: Precise force measurement Stretching DNA* *Gross, P. et al. Quantifying how DNA stretches, melts and changes twist under tension. Nature Physics 7, (2011).

7 Tensile strength and stiffnes of materials A comparison ~100 GPa ~1000 GPa

8 Raman spectroscopy in Nanomechanics

9 Raman scattering Energy conservation: s i f Momentum conservation: k ki k f

10 Experimental set-ups I. II m 0.60 m Renishaw invia 2000 spectrometer system III. Jobin Yvon microscope/spex Triplemate 0.6m Remote Raman System

11 Raman spectra of graphitic materials - 2D Raman shift (cm -1 )

12 Raman Spectrum of SWCNT 1D

13 CF Structure Development and the corresponding Raman spectra of carbon fibres -3D High Modulus Low Modulus Carbon fibres (microscale) (Source: A. R. Bunsell, Fibre Reinforcements for Composite Materials, Amsterdam, The Netherlands: Elsevier Science Publishers B.V., 1988, p. 120.)

14 G-band of graphene under Strain in Tension & Compression

15 Axial Experiments in Graphene (tension & compression combined with Raman measurements)

16 Experimental Set-up for Application of Uniaxial Strain Simply-supported flake F1 Embedded flake or S1805 (785 nm) (514.5 nm) Materials & Geometry SU8 photo resist epoxy-based polymer PMMA beam substrate (2.9x12.0x70) mm 3 x = 10.4 mm and L = 70 mm Mechanical strain at the top of the beam x 2 3t 1 2L x L δ: deflection of the beam neutral axis L: span of the beam t : beam thickness Operating limits: L>> 10δ max -1.5% < ε < 1.5% 16

17 G-band under Strain in Tension & Compression F1

18 G-band vs. Strain (no residual strain) 0.0% 1.0% / 36.0 cm G 1 /% G / 17.5 cm 1 /% Mohiudin et al, PRB, 2009 Frank et al, ACS-Nano, 2010

19 Raman Intensity (a.u.) Raman 2D-peak splitting in single-layer graphene λ=514.5 nm Tension λ=785 nm 1.30% 0.90% 0.61% 0.41% 0.00% Raman shift (cm -1 ) Measurements of the 2D band alone, for excitation energies lower than 2.41 ev (514.5 nm), may lead to errors with regards to the detailed determination state of stress/strain in the specimen. Frank et al., ACS-Nano, 5, 2321 (2011)

20 Pos(2D) (cm -1 ) ω2d/ε (cm -1 /%) A simply-supported ( bare ) flake can be loaded! λ exc =514.5nm ω = ε 27.8ε ω = ε 17.3ε Graphene flake PMMA Compression Tension Strain (%) -80 Tsoukleri et al. Small 2009, 5, 2397]

21 Pos(2D) (cm -1 ) ω 2D /ε (cm -1 /%) D Band for embedded flake λ exc =514.5nm ω = ε 55.1ε 2 PMMA PMMA 495 SU8 Compression ω = ε 13.7ε 2 Tension Strain (%) Tsoukleri et al. Small 2009, 5, 2397

22 Tensile testsin graphene Current status Lee et al, Science (2008) Theory *

23 Graphene: a powerful stress/ strain sensor Phonon stress (σ) or strain (ε) sensitivities: G T 1 1 ~ 27.0 (cm % ) G T 1 1 ~ 2.7 (cm GPa ) For small(??) strains E, E 1TPa [Lee et al, Science (2008)] (2 D) T ~ 60.0 cm (cm % ) (2 D) T 1 1 ~ 6.0 (cm GPa ) Knowing the wavenumber shift we can resolve the inverse problem i.e. to obtain the values of axial σ and/or ε in graphene-based materials through the above relations. Frank, O. et al. Development of a universal stress sensor for graphene and carbon fibres. Nat Commun 2, 255 (2011).

24 Mechanical characterization of single layer graphene Ti strip AFM nanoindentation C. Lee, et al., Science 321, 385 (2008) E =1.0 TPa, Fracture strength = 130 GPa Bending of the substrate (PDMS) & Raman PDMS M. Huang, et al., Proc. Nat. Acad. Sci. 106, 7304 (2009) 1 ω ε 12.5 cm % G 1 ω ε 5.6 cm % G 1 ω2d ε 21.0 cm % 4-point bending of the substrate (PMMA) & Raman T. M. G. Mohiuddin, et al., Phys. Rev. B 79, (2009) Graphene under pressure & Raman J. Nicolle, et al., Nano Lett. 11, 3564 (2011) Bulge test & Raman (Biaxial deformation) J.-U. Lee, et al., Nano Lett. 12, 4444 (2012) Controlled creation of periodic ripples in suspended graphene sheets using thermally generated strains W. Bao, et al., Nat Nano 4, 562 (2009) Imaging of a vibrating graphene beam using SPM Garcia-Sanchez, et al., Nano Lett., 8, 1399 (2008) Graphene resonator with local buckling E = 2.4 TPa!!!

25 Axial Experiments in CNT yarns (tension combined with Raman measurements)

26 Draw-Twist process for CNT yarn production Ribbon Spindle Motor MWNT forest Twisted Yarn Si substrate Spinning machine CNT forest CNT yarn M. Zhang, et al. Multifunctional Carbon Nanotube Yarns by Downsizing an Ancient Tecnology, Science, 36, p. 1358, 2004

27 Yarn model geometry (Ideal helical structure) r k R Yarn segment concentric packing of l layers (R is the radius of the outer layer of the yarn and r k is the radius of layer k ) layer helix angles (h is the height along the yarn axis of one turn of twist) Outer layer helix angle Inner layer k helix angle a a s s 2 R arctan h r tan a k s arctan R

28 Twist (turns/m) of yarns tan a 1 s h D a s a s 2 R arctan h 1 ~ m 1 h where α s = 26 o and D = 10.5 μm were measured by SEM pictures

29 Stress / MPa 1000 CNT yarn mechanical performance CNT yarn (θ = 26 0, D = 10.5 μm) 0.01 min -1 Shell Sliding Experiment in MWCNT min min min min -1 strain rate: min min min min min Strain / % CNT yarns behave like a viscoelastic Material Strain-to-failure increases with strain rate CNT yarn strength is 620 MPa and is independent from strain rate (friction forces are independent from the rate of the relative movement between CNT bundles) Qian D. eta al. Appl Mech Rev vol 55, no 6, November 2002 Yu, M.-F., et al.,. J. Phys. Chem. B 104, (2000).

30 CNT yarn fracture surface (i) grab-like pike-like (ii) A bundle of MWCNTs located at the yarn centre is clearly unveiled (ii) showing that the bundle is subjected to higher strains when an external tensile load is applied to the yarn. This is consistent with ideal helix yarn models where when an ideal helical structure is under an external tensile load, the fiber strains are largest along the yarn axis and smallest in the outermost layer.

31 Stress transfer in CNT yarns Raman Spectroscopy D G CNT yarn surface indicative spectrum 2D 2D peak position decreases slightly (~4cm -1 ) with strain 2D FWHM decreases showing a min value which reflects the decreasing of helix angle and consequently the spread of strain values Raman shift (cm -1 ) Raman shift (cm -1 ) These results indicate that the fiber strains are largest along the yarn axis and smallest in the outermost layer. 2D peak position and FWHM as a function of uniaxial tensile strain 2D peak position 2D FWHM

32 Breaking the diffraction limit with TERS (Tip Enhanced Raman Spectrocopy) AFM + Raman microscopy Graphene G Stadler, J., et al., Nano Lett. 10, (2010). 2D The AFM nano-antenna can locally enhance the electromagnetic field intensity near the tip apex and become a localized nano-source of light. P. Dorozhkin et al, Microscopy Today, doi: /s (2010)

33 Thank you very much for your kind attention!

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