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S-1 Supporting Information Ultra-high Thermally Conductive and Rapid Heat Responsive Poly(benzobisoxazole) Nanocomposites with Self-aligned Graphene Weifeng Zhao 1,2 , Jie Kong 1 *, Hu Liu, 3 Qiang Zhuang 1 , Junwei Gu 1 and Zhanhu Guo 3 * 1 MOE Key Laboratory of Space Applied Physics and Chemistry, Shaanxi Key Laboratory of Macromolecular Science and Technology, School of Science, Northwestern Polytechnical University, Xi’an, 710072, P. R. China 2 School of Materials and Chemical Engineering, Xi’an Technological University, Xi’an 710021, P. R. China 3 Integrated Composites Laboratory (ICL), Department of Chemical & Biomolecular Engineering, University of Tennessee, Knoxville, TN 37996 USA *Corresponding Authors: E-mail Address: [email protected] (J. K.); [email protected] (Z.G.) Electronic Supplementary Material (ESI) for Nanoscale. This journal is © The Royal Society of Chemistry 2016

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Page 1: Self-aligned Graphene Supporting Information Responsive ... · PDF fileResponsive Poly(benzobisoxazole) Nanocomposites with ... Table S1 List of the atomic composition of GO and TRG

S-1

Supporting Information

Ultra-high Thermally Conductive and Rapid Heat

Responsive Poly(benzobisoxazole) Nanocomposites with

Self-aligned Graphene

Weifeng Zhao1,2, Jie Kong1*, Hu Liu,3 Qiang Zhuang1, Junwei Gu1 and Zhanhu

Guo3*

1MOE Key Laboratory of Space Applied Physics and Chemistry, Shaanxi Key

Laboratory of Macromolecular Science and Technology, School of Science,

Northwestern Polytechnical University, Xi’an, 710072, P. R. China 2School of Materials and Chemical Engineering, Xi’an Technological University, Xi’an

710021, P. R. China3Integrated Composites Laboratory (ICL), Department of Chemical & Biomolecular

Engineering, University of Tennessee, Knoxville, TN 37996 USA

*Corresponding Authors: E-mail Address: [email protected] (J. K.);

[email protected] (Z.G.)

Electronic Supplementary Material (ESI) for Nanoscale.This journal is © The Royal Society of Chemistry 2016

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S-2

Synthesis and Characterization of PBO Precursor (TBS-prePBO)

O

N

O

Nn

Figure S1 Chemical structure of PBO.

OH

H2N

HO

NH2

2HClSi Cl

TEA DMF

HN

O

HN

O

Si

Si

Si

Si

C ClOO

Cl C

NMP

m

HN

O

HN

HO Si

COO

C

n

HN

O

HN

OSi Si

COO

C

TBS-prePBO

TBS-DARDAR

Figure S2 Synthesis of soluble PBO precursor (TBS-prePBO) via reaction of tert-

butyldimethylsilyl group-functionalized 4, 6-diaminoresoisinol (TBS-DAR) and

terephthaloyl chlorid.

As illustrated in Figures S1-2, the 4, 6-diaminoresorcinol dihydrochloride (DAR) is the

main monomer for the synthesis of PBO. However, it has poor solubility in common

solvents and is easily oxidized in air atmosphere, leading to the difficulty in the design

and synthesis of the PBO precursor. To overcome this defect, tert-butyldimethylsilyl

(TBS) was chosen as the functional unit of DAR to improve its solubility and stability.

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S-3

8 7 6 5 4 3 2 1 0

Chemical shift (ppm)

CDCl3 ec,d

b

a

ec

dba

O SiSi O

NH

NH SiSi

(a)

TMS

14 13 12 11 10 9 8 7 6 5 4 3 2 1 0 -1

g

gO SiHO

NH

NH

COC

O

n

Chemical shift (ppm)

a bd

c

fe

TMS

a

b

ef

c

d

H2O

DMSO

(b)

Figure S3 1H NMR spectrum of (a)TBS-DAR and (b)TBS-prePBO.

As shown in Figure S3a, the strong signals ascribed to the protons of TBS groups (Ha at

0.22–0.24 ppm, Hb at 0.97–1.02 ppm) are observed from the 1H NMR spectrum of the

prepared TBS-functionalized DAR (TBS-DAR). Especially, the Ha,b in the TBS group

and the Hc,d (6.27-6.30 ppm) in the aromatic groups were determined to be TBS:

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S-4

aromatic=60.3:2, which gave an evidence that all the hydroxyl and amine groups of DAR

have been fully protected by the TBS groups.

As shown in Figure S3b, two resonance peaks attributed to the proton Hf of terephthaloyl

chloride and the proton He of the secondary amine N-H (-C=O) were observed, which

clearly suggested the progress of polycondension reaction. Moreover, compared with

Figure S3a, the resonance peaks of Hc and He moved to a much higher chemical shift due

to the presence of terephthaloyl groups, providing an obvious evidence for the

condensation reaction. The integration ratio of methyl and aromatic protons was

(Ha+Hb):(Hc+Hd+Hf), i.e. 22.3:6, which was in correspondence with the TBS content

around 75% in molar ratio on the main chain. It is lower than the expected value 30:6 for

the TBS-prePBO with hydroxyl groups fully protected. It suggests that a partial

weakening of the TBS has occurred during the polymerization process. As a result, the

proton in the phenolic hydroxyl group (Hg, 5.29 ppm) was also detected as shown in

Figure S3b.

The good solubility of TBS-DAR greatly facilitates the synthesis of PBO precursors by a

benign condensation polymerization of TBS-DAR with terephthaloyl chloride in N-

methyl-2-pyrrolidone solution. During the synthesis, an increase of the solution’s

viscosity is observed, giving a direct indication that there is a dramatic increase in the

molecular weight as expected according to the general mechanism of the condensation

polymerization. After precipitation in methanol and purification with water, a yellowish

powder was obtained with a yield of 85%. The intrinsic viscosity of the obtained TBS-

prePBO polymer was 0.36 dL g-1 in DMF at 30 °C.

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4000 3000 2000 1000 065

70

75

80

85

90

95

100 TBS-prePBO

1650

Tra

nsm

ittan

ce(%

)

Wavenumbers(cm-1)

1730

TRG@TBS-prePBO

Figure S4 FT-IR spectrum of TBS-prePBO and the extracted TRG@TBS-prePBO hybrid.

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S-7

292 290 288 286 284 282 280Binding energy (ev)

O=C-O289.1ev

C=O287.8ev

C-O286.4ev

C-C284.2ev

(a)

292 290 288 286 284 282 280Binding energy (ev)

O-C=O288.5ev

C=O286.8ev

C-O285.7ev

C-C284.3ev

(b)

Figure S5 XPS spectra of (a) GO and (b) TRG reduced at 350 oC.

Table S1 List of the atomic composition of GO and TRG reduced at 350 oC measured by XPS.

Sample C(atomic%) O(atomic%) N(atomic%) S(atomic%) Si(atomic%) C/O ratio

GO 65.2 30.4 1.8 1.4 1.2 2.14TRG@350oC 76.8 16.5 2.8 2.6 1.3 4.65

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100 200 300 400 500 600 700 800 900 100020

30

40

50

60

70

80

90

100

TRG@350oC GO

Mas

s (%

)

Temperature (oC)

Figure S6 TGA curves of GO and TRG heated at 350 oC

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S-9

Figure S7 SEM images of the fracture surface of TRG/PBO nanocomposite film, the red cycle indicate a well-ordered parallel stacking of graphene sheets with their sheet plane

parallel to the composite film surface

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Figure S8 (a) Principle of operation of laser flash apparatus; and (b) sample carriers used

for the through-thickness and in-plain thermal diffusivity test.

In the laser flash test, the samples were coated with graphite aerosol and then placed

on a carrier as shown in Figure S8(b). In carrying out a measurement, the lower surface

of the sample (Figure S8(a)) is irradiated by a short energy pulse. The pulse energy is

absorbed and converted into a confined heat source on the lower surface. The heat waves

diffuse through the sample and lead to a temperature rise on the upper surface of the

sample. An infrared detector is directed to the upper surface and generates a highly

sensitive signal on a response to the temperature change of the sample. The obtained

Test Sample

Temperature Signal versus

Time

Laser Pulse

Heating

Trough-thickness In-plain

(a)

(b)

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S-11

typical course of the normalized signals versus time is presented in Figure5 (A). Using

the half time (t1/2, time value at half signal height) and sample thickness (δ), the thermal

diffusivity (D) can be given by means of the Parker formula[S1].

2 2

21 1

2 2

1.37 0.1388Dt t

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-500 0 500 1000 1500 2000 2500

0.0

0.2

0.4

0.6

0.8

1.0 Stage2 TRG1.4vol% TRG1.05vol% PBO

Norm

alize

d Te

mpe

ratu

re S

igna

l

Time/ms

(a)

Stage1

-10 0 10 20 30 40

0.0

0.2

0.4

0.6

0.8

1.0(b)

Norm

alize

d Te

mpe

ratu

re S

igna

l

Time/ms

Figure S9 (a)In-plane direction temperature evolution of nanocomposite film surface at

different time after pulsed laser heating; (b) the curve of temperature evolution typically

measured for the stage1 incensement shown in (a) for the composite with 1.05vol% TRG

loading

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Table S2 Comparison of the thermal conductivity enhancement of polymer composites with various graphene-based materials.

Polymer matrix Filler type Filler

fraction

Thermal conductivity

(W/(m·K))Method Reference

PP Graphene nanoplatelets 25 vol% 1.2 DSC S2

PPS Graphene nanoplatelets 40 wt% 4.4 Hot plate

method S3

LCP Graphene nanoplatelets 30 wt% 2.5 ASTM

E1225-04 S4

Epoxy GO 20 wt% 5.8 Laser flash S5

Epoxy Graphene nanoplatelets 25 wt% 2.67 Hot plate

method S6

Epoxy TRG 4 phr 1.9 Hot plate method S7

Epoxy Non-oxidized graphene 10 wt% 1.53 Laser flash S8

Epoxy Multilayer graphene 10 vol% 5.1 Laser flash S9

Epoxy Few layer graphene 25vol% 6.4 Laser flash S10

Epoxy Multilayer graphene 11.8wt% 33.5 ASTM

D5470-06 S11

PBO TRG 4.2vol% 50 Laser flash This work

References:

[S1]WJ Parker, R J Jenkins, C P Butler and G L Abbott.J.Appl. Phys.,1961:1679

[S2] K Kalaitzidou , H Fukushima, L T Drzal. Carbon, 2007, 45, 1446–1452.

[S3] JW Gu, J. Du, J Dang, W.C Geng, SH Hu and QY Zhang. RSC Adv., 2014, 4, 22101

[S4] SN Leung, MO Khan, H Nagui and F. Dawson. Appl. Phys. Lett. 2014, 104, 081904

[S5] S Ganguli, A K Roy, D P Anderson , Carbon 2008,46,806 .

[S6] WM Guo, GH Chen. J. Appl. Polym. Sci. 2014, 131, 40565

[S7] C C Teng , C C M Ma, C H Lu, SY Yang and et al. Carbon, 2011,49, 5107.

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[S8] S H Song , K H Park , B H Kim and et al. Adv. Mater. 2013, 25, 732.

[S9] K M F Shahil, A A Balandin. Nano Lett. 2012, 12, 861.

[S10] A Yu , P Ramesh , M E. Itkis, E Bekyarova and R. C. Haddon. J. Phys. Chem. C, 2007, 111, 7565.

[S11] Q Li, Y F Guo, W Li, SQ Qiu and et al. Chem. Mater. 2014, 26, 4459.