**Postsynthesis Treatment Influence on Hydrogen Sorption Properties of Carbon Nanotubes**

Michail Obolensky, Andrew Basteev, Vladimir Beletsky, Andrew Kravchenko, Yuri Petrusenko, Valeriy Borysenko, Sergey Lavrynenko, Oleg Kravchenko, Irina Suvorova, Vladimir Golovanevskiy and Leonid Bazyma

Additional information is available at the end of the chapter

http://dx.doi.org/10.5772/50151

## **1. Introduction**

It has been shown in the previous investigations (Pradhan et al., 2002; Obolensky et al., 2011a, 2011b) that the postsynthesis treatment (e.g. chemical, heat treatment, milling, irradiation etc.) of single-walled carbon nanotubes (SWCNT) can essentially change their sorption properties. Methods of SWCNT synthesis and features of the postsynthesis treatment of the SWCNT show in numerous experiments a wide range of gas (e.g. hydrogen etc.) mass contents in SWCNT ranging from extremely low (less than 0.1 wt%) to significantly high (more than 6 wt%) values. Unfortunately, none of the claims of hydrogen storage exceeding the DOE limit have been confirmed. For recent review of effect of synthesis method and post-treatment of CNTs, see Ref. (Chang & Hui-Ming, 2005).

So, it is well established that hydrogen storage capacity of CNTs depends on many parameters including their pretreatment, types and structural modifications etc. One of the ways seems to be highly influential and it is the generation of appreciable structural defects in the tube walls. However, the increase in defects in graphitized layers of CNTs should be limited otherwise their structure would be destroyed which might lead to lowering of interaction or potential energy between the hydrogen molecules and carbon atoms. For instance, non-optimized electron irradiations severely destroy the graphitic network of CNTs (Banhart et al., 2002) which is not desirable for application purposes.

It has been reported that postsynthesis treatment can easily induce defects in the wall of SWCNT (Pradhan et al., 2002; Banhart et al., 2002; Hashimoto et al., 2004). The possibility of molecular hydrogen adsorption by the defect sites can also be considered. The experimental investigations of above mentioned factors as well as the result of irradiation on to SWCNT sorption capability are reported in this study.

## **2. Experimental**

## **2.1. Materials**

The arc-derived as-prepared (AP) SWNT material used in the present studies was obtained from Carbon Solutions, Inc.. All data reported here are collected using materials from the same batch of SWNT material.

Postsynthesis Treatment Influence on Hydrogen Sorption Properties of Carbon Nanotubes 169

Parameters Values

Energy of accelerated electrons 0.5- 3.0 MeV Beam current (without scanning) 0.5-150 μА Max beam current (with scanning): up to 500 μА Electron beam disperse 10-4 radian

Vacuum in electron beam line 1x10-7 mbar Power consumption 20 кW

studied on the mass spectrometer MX7203. The schematics of the experimental facility used

Diameter of electron beam without focusing 1,0 сm

Diameter of electron beam with focusing, for 90% capacity <1 mm

**Figure 1.** Experimental facility schematics (Obolensky et al., 2011b). Vc – total accurate including manometer and supply pipelines; V1 – vessel with pure gas; V0 – ampoule with carbon nanotubes

some samples at the Physics Institute of the Penn State University.

Raman spectra studies at ambient conditions with 514 nm laser line were carried out for

with both measurement methods is shown in Figure 1.

**Table 1.** Parameters of ELIAS accelerator

sample; H2 – non-purified hydrogen source

The impurities in AP-SWNTs may be divided into two categories: carbonaceous (amorphous carbon and graphitic nanoparticles) and metallic (typically transition-metal catalysts). Thermogravimetric analysis (TGA) can be used to analyze the amount of metallic components quantitatively whereas Raman spectroscopy can be used to estimate qualitatively the carbonaceous impurities in AP and purified-SWNTs.

The AP SWNT (Carbon Solutions, Inc.) material has 21 to 31 percent of impurities which is consistent with the previously reported (Itkis et al., 2003) 34.5 ±1.8 percent impurities range. For purification of SWNTs the following technique has been used (Pradhan et al., 2002; Obolensky et al., 2011b). The SWNT (Carbon Solutions, approximately 1g amount) was oxidized in open air at 3500C temperature for 30 minutes and then heated in 2.6 M HNO3 for 20 hours. After above procedure the treated CNTs were flushed in methanol and then in water until the neutral reaction was achieved, dried in air and then were annealed in deep vacuum (10-8 bar) for 20 hours at 800оС temperature. Identification of the gases allocated in an act of warming of a sample at 850оС was carried by mass-spectrometry (МХ-7203). Working pressure in the chamber of the mass-spectrometer was 10-4 Па. Approbation of nanotubes purify technology was carried out and 700 milligrams of the purified nanotubes were obtained (metal 6-9 at. %).

After chemical treatment, CNTs were milled at liquid nitrogen temperature in a stainless steel ball mill. Milling duration was 60 minutes with interruption after each 5 minutes for CNT samples' microscopic control. After the milling procedure finishing the "ball mill" was heated up to the room temperature and CNT samples were sieved through a 63 μm sieve (Obolensky et al., 2011b).

## **2.2. Experimental facility**

The method for SWNT electron bombardment irradiation was elaborated. In contrast to (Obolensky et al., 2011a) where the exposure of γ – quantum 105 Rad was used (this dose is equal to regime of electron bombardment ~3\*1012 e- /cm2) the fluence in the work reported here was 1013-2\*1015e- /cm2. The electron bombardment procedure was carried out at room temperature on the ELIAS linear accelerator (National Science Center "Kharkov Institute of Physics and Technology"). The electron energy was 2.3 MeV and beam intensity was 0.2 μA/cm2. The main parameters of ELIAS accelerator are specified in Table 1.

Study of sorption/desorption process was carried out using the standard volumetric method (Obolensky et al., 2011a, 2011b). Hydrogen desorption out from SWNT was also studied on the mass spectrometer MX7203. The schematics of the experimental facility used with both measurement methods is shown in Figure 1.


**Table 1.** Parameters of ELIAS accelerator

168 Hydrogen Storage

**2. Experimental** 

same batch of SWNT material.

were obtained (metal 6-9 at. %).

(Obolensky et al., 2011b).

here was 1013-2\*1015e-

**2.2. Experimental facility** 

equal to regime of electron bombardment ~3\*1012 e-

The arc-derived as-prepared (AP) SWNT material used in the present studies was obtained from Carbon Solutions, Inc.. All data reported here are collected using materials from the

The impurities in AP-SWNTs may be divided into two categories: carbonaceous (amorphous carbon and graphitic nanoparticles) and metallic (typically transition-metal catalysts). Thermogravimetric analysis (TGA) can be used to analyze the amount of metallic components quantitatively whereas Raman spectroscopy can be used to estimate

The AP SWNT (Carbon Solutions, Inc.) material has 21 to 31 percent of impurities which is consistent with the previously reported (Itkis et al., 2003) 34.5 ±1.8 percent impurities range. For purification of SWNTs the following technique has been used (Pradhan et al., 2002; Obolensky et al., 2011b). The SWNT (Carbon Solutions, approximately 1g amount) was oxidized in open air at 3500C temperature for 30 minutes and then heated in 2.6 M HNO3 for 20 hours. After above procedure the treated CNTs were flushed in methanol and then in water until the neutral reaction was achieved, dried in air and then were annealed in deep vacuum (10-8 bar) for 20 hours at 800оС temperature. Identification of the gases allocated in an act of warming of a sample at 850оС was carried by mass-spectrometry (МХ-7203). Working pressure in the chamber of the mass-spectrometer was 10-4 Па. Approbation of nanotubes purify technology was carried out and 700 milligrams of the purified nanotubes

After chemical treatment, CNTs were milled at liquid nitrogen temperature in a stainless steel ball mill. Milling duration was 60 minutes with interruption after each 5 minutes for CNT samples' microscopic control. After the milling procedure finishing the "ball mill" was heated up to the room temperature and CNT samples were sieved through a 63 μm sieve

The method for SWNT electron bombardment irradiation was elaborated. In contrast to (Obolensky et al., 2011a) where the exposure of γ – quantum 105 Rad was used (this dose is

temperature on the ELIAS linear accelerator (National Science Center "Kharkov Institute of Physics and Technology"). The electron energy was 2.3 MeV and beam intensity was 0.2

Study of sorption/desorption process was carried out using the standard volumetric method (Obolensky et al., 2011a, 2011b). Hydrogen desorption out from SWNT was also

μA/cm2. The main parameters of ELIAS accelerator are specified in Table 1.

/cm2. The electron bombardment procedure was carried out at room

/cm2) the fluence in the work reported

qualitatively the carbonaceous impurities in AP and purified-SWNTs.

**2.1. Materials** 

**Figure 1.** Experimental facility schematics (Obolensky et al., 2011b). Vc – total accurate including manometer and supply pipelines; V1 – vessel with pure gas; V0 – ampoule with carbon nanotubes sample; H2 – non-purified hydrogen source

Raman spectra studies at ambient conditions with 514 nm laser line were carried out for some samples at the Physics Institute of the Penn State University.

## **3. Results**

#### **3.1. Adsorption studies of non-irradiated samples**

Study of sorption/desorption process was carried out using the standard volumetric method on a custom designed and manufactured manufactured vacuum stainless steel facility which included the known good unit volume VE and measuring vessel with volume VМ. Part of measuring vessel V78 was cooled down to liquid nitrogen vaporisation temperature of ~ 78 K. Before measurements the facility was calibrated. The good unit with volume VE was inflated by gaseous helium or hydrogen with pressure РI ~ 10 bar at room temperature which has been measured with ± 0.5 К precision. The pressure was controlled by electronic manometer GE Druck 104 with 1 mbar resolution. After the total facility volume V = VE + VМ was filled up, the pressure dropped to the value of PF = VEPI(VE + VМ - VA). This circumstance allowed exact determination of the volumes relation, taking into account the ampoule volume VA without sample. Above relation for hydrogen and helium was found equal with approximately ~ 0.01 percent accuracy and therefore the hydrogen sorption by vacuum system elements could be excluded from consideration. After this procedure, the container with ampoule was cooled to temperature 78 K and relation РW/РF was determined, where РW is the pressure in the system after cooling.

Postsynthesis Treatment Influence on Hydrogen Sorption Properties of Carbon Nanotubes 171

In Figure 2, one can see three sections with different sorption dynamics. On the base of comparison of this pressure drop dynamics with pressure drop dynamics for calibration stroke the following can be noted. The pressure drop relative to the empty container was observed already at room temperature during the letting-to-hydrogen and this pressure was noted at a ~ 20 mbar level. The additional pressure decrease was observed during further container cooling to 78 K temperature and at different cooling cycles this value was 10 – 15

The pressure in the system during whole system heating was less than the pressure before the beginning of cooling by 10 – 12 mbar. Apparently this fact could be explained by any amount of hydrogen staying in binding state at room temperature after desorption. We

Figure 3 illustrates the correlation of pressure and temperature in the system for two evacuating regimes: fast (3 min) and gradual (15 min). Apparently already at 78 K temperature the increase of the duration of evacuation causes significant desorption and consequently elimination of part of hydrogen out from the system even before the beginning of heating. The duration of container heating for both regimes was approximately 25 – 30 min.

**Figure 3.** The dependence of pressure in the container with non-irradiated CNT samples upon temperature during container heating for different evacuation rates (Obolensky et al., 2011b)

chemosorption regime with higher characteristic temperatures.

located in non-irradiated SWNT was equal to 0.12 ±0.2 mass percent.

The temperature dependences of hydrogen density in volume situated at heating regime (V78) and in the rest facility volume at ambient temperature are shown in Figure 4. It could be seen that the main hydrogen mass is exuded at temperature T< 160 K that is caused by relatively low value of physical absorption activation energy. Pressure difference occurring at container heating without evacuating and initial pressure РF as noted earlier is caused by other mechanism with higher values of desorption energies and it can be related to

Our estimations show that at different sorption/desorption cycles the amount of hydrogen

didn't register this phenomenon on repeat of the heating-cooling cycles.

mbar.

The measurement of physically absorbed hydrogen was conducted in accordance with the following procedure. Firstly, after cooling down the container to temperature 78 K the system was evacuated to pressure ~ 0.1mbar for gaseous hydrogen elimination. The next step was pressure increase registration in the system during container heating, caused by hydrogen desorption process.

The samples of SWNT with mass of 80 – 300 mg (estimated bulk density ~ 1000 kg/m3) were used for the experiments on the volumetric facility. The pressure drop character dynamics during container with non-irradiated samples cooling are shown in Figure 2.

**Figure 2.** The dependence of pressure drop in the container with non-irradiated CNT samples upon time during container with samples cooling (PF = 5035 mbar) (Obolensky et al., 2011b)

In Figure 2, one can see three sections with different sorption dynamics. On the base of comparison of this pressure drop dynamics with pressure drop dynamics for calibration stroke the following can be noted. The pressure drop relative to the empty container was observed already at room temperature during the letting-to-hydrogen and this pressure was noted at a ~ 20 mbar level. The additional pressure decrease was observed during further container cooling to 78 K temperature and at different cooling cycles this value was 10 – 15 mbar.

170 Hydrogen Storage

**3. Results** 

**3.1. Adsorption studies of non-irradiated samples** 

where РW is the pressure in the system after cooling.

hydrogen desorption process.

Study of sorption/desorption process was carried out using the standard volumetric method on a custom designed and manufactured manufactured vacuum stainless steel facility which included the known good unit volume VE and measuring vessel with volume VМ. Part of measuring vessel V78 was cooled down to liquid nitrogen vaporisation temperature of ~ 78 K. Before measurements the facility was calibrated. The good unit with volume VE was inflated by gaseous helium or hydrogen with pressure РI ~ 10 bar at room temperature which has been measured with ± 0.5 К precision. The pressure was controlled by electronic manometer GE Druck 104 with 1 mbar resolution. After the total facility volume V = VE + VМ was filled up, the pressure dropped to the value of PF = VEPI(VE + VМ - VA). This circumstance allowed exact determination of the volumes relation, taking into account the ampoule volume VA without sample. Above relation for hydrogen and helium was found equal with approximately ~ 0.01 percent accuracy and therefore the hydrogen sorption by vacuum system elements could be excluded from consideration. After this procedure, the container with ampoule was cooled to temperature 78 K and relation РW/РF was determined,

The measurement of physically absorbed hydrogen was conducted in accordance with the following procedure. Firstly, after cooling down the container to temperature 78 K the system was evacuated to pressure ~ 0.1mbar for gaseous hydrogen elimination. The next step was pressure increase registration in the system during container heating, caused by

The samples of SWNT with mass of 80 – 300 mg (estimated bulk density ~ 1000 kg/m3) were used for the experiments on the volumetric facility. The pressure drop character dynamics

**Figure 2.** The dependence of pressure drop in the container with non-irradiated CNT samples upon

time during container with samples cooling (PF = 5035 mbar) (Obolensky et al., 2011b)

during container with non-irradiated samples cooling are shown in Figure 2.

The pressure in the system during whole system heating was less than the pressure before the beginning of cooling by 10 – 12 mbar. Apparently this fact could be explained by any amount of hydrogen staying in binding state at room temperature after desorption. We didn't register this phenomenon on repeat of the heating-cooling cycles.

Figure 3 illustrates the correlation of pressure and temperature in the system for two evacuating regimes: fast (3 min) and gradual (15 min). Apparently already at 78 K temperature the increase of the duration of evacuation causes significant desorption and consequently elimination of part of hydrogen out from the system even before the beginning of heating. The duration of container heating for both regimes was approximately 25 – 30 min.

**Figure 3.** The dependence of pressure in the container with non-irradiated CNT samples upon temperature during container heating for different evacuation rates (Obolensky et al., 2011b)

The temperature dependences of hydrogen density in volume situated at heating regime (V78) and in the rest facility volume at ambient temperature are shown in Figure 4. It could be seen that the main hydrogen mass is exuded at temperature T< 160 K that is caused by relatively low value of physical absorption activation energy. Pressure difference occurring at container heating without evacuating and initial pressure РF as noted earlier is caused by other mechanism with higher values of desorption energies and it can be related to chemosorption regime with higher characteristic temperatures.

Our estimations show that at different sorption/desorption cycles the amount of hydrogen located in non-irradiated SWNT was equal to 0.12 ±0.2 mass percent.

Postsynthesis Treatment Influence on Hydrogen Sorption Properties of Carbon Nanotubes 173

sorption sites appearing as the result of irradiation and can be characterized by various activation energies. It should be noted that over a long period of time of samples staying in air between irradiation procedures and hydrogen saturation, complete saturation generated by irradiation sites filling by the molecules of other gases has not been detected. The data in Figure 5 can be presented in another form (Figure 6) i.e. as additional amount of hydrogen desorbed from irradiated sample (Δ - the difference between the irradiated and not

**Figure 5.** The dependencies of amount of hydrogen (arbitrary units) exuded from non-irradiated (a)

hydrogen adsorption property of SWNTs without mechanical milling.

In order to control the structural transformations of CNTs, it is important to clearly understand the defect generation mechanism and to realize the extent of defects and their influence on sorption properties of CNTs. Acid or alkali treatment does not routinely improve the hydrogen storage capacity of CNT samples. A suitable ball-milling treatment and activation process can open the caps of CNTs and produce more structural defects, and therefore may be beneficial in improving their hydrogen storage properties (Chang & Hui-Ming, 2005). In this connection we investigated the effect of electron irradiation on the

Five AP samples (cf., Table 2) have been annealed in vacuum during 10 hours at 8000C temperature. The first sample (#1) was retained as the control sample. Sample #2 has remained for control and three samples (#3-5) were irradiated with various fluence (5\*1014,

/cm2). After that, four samples (#2-5) were saturated at 10 bar pressure for 3

/сm2 (b) samples upon temperature (Obolensky et al., 2011b)

irradiated samples).

and irradiated up to fluence 1014 e-

1015 and 2\*1015e-

hours at 78 K temperature..

**Figure 4.** The dependence of hydrogen density in container with non-irradiated CNT samples upon temperature during container heating for different evacuation rates (Obolensky et al., 2011b)

#### **3.2. Adsorption studies of irradiated samples**

Hydrogen storage was studied with 2.5-90 mg samples. Saturation was carried out at liquid nitrogen temperatures (~78 K), and 300 K and at pressures between 3 and 10 bar. The measurement of physically absorbed hydrogen was conducted in accordance with the following procedure.

First, after cooling the container down to 78 K temperature the system was evacuated to ~ 0.1 mbar of pressure for gaseous hydrogen elimination. Next, pressure in the system during container heating up to room temperature caused by hydrogen desorption process was registered. Hydrogen desorption out from SWNT was also studied in the 0-900 C temperature range by mass-spectrometry method on the MX 7203 mass spectrometer.

Our estimations (Obolensky et al., 2011b) show that at different sorption/desorption cycles the amount of hydrogen located in non-irradiated SWNT was equal to 0.12 ±0.2 mass percent. Hydrogen desorption from treated and exposed to physical sorption/desorption procedure material at pressures ~3000 mbar as it is described above has been studied with the use of mass-spectrometry method within the 0 – 900 °C temperature interval on the MX 7203 mass spectrometer. The dependencies of the amount of hydrogen extracted from nonirradiated (a) and irradiated up to the fluence of 1014 e-/сm2 (b) SWNT samples upon temperature are shown in arbitrary units in Figure 5.

As can be seen from Figure 5 the amount of hydrogen desorbed from irradiated material is approximately 2.5 times higher compared with that desorbed from the non-irradiated material. We have to draw attention to the fact that all procedures of the sorption/desorption processes were carried out at the 78 – 300 К temperature interval but at the same time significant amount of hydrogen is desorbed at temperatures higher than 300 K. There are additional peaks on the desorption curve which apparently correspond with different sorption sites appearing as the result of irradiation and can be characterized by various activation energies. It should be noted that over a long period of time of samples staying in air between irradiation procedures and hydrogen saturation, complete saturation generated by irradiation sites filling by the molecules of other gases has not been detected. The data in Figure 5 can be presented in another form (Figure 6) i.e. as additional amount of hydrogen desorbed from irradiated sample (Δ - the difference between the irradiated and not irradiated samples).

172 Hydrogen Storage

**Figure 4.** The dependence of hydrogen density in container with non-irradiated CNT samples upon

Hydrogen storage was studied with 2.5-90 mg samples. Saturation was carried out at liquid nitrogen temperatures (~78 K), and 300 K and at pressures between 3 and 10 bar. The measurement of physically absorbed hydrogen was conducted in accordance with the

First, after cooling the container down to 78 K temperature the system was evacuated to ~ 0.1 mbar of pressure for gaseous hydrogen elimination. Next, pressure in the system during container heating up to room temperature caused by hydrogen desorption process was registered. Hydrogen desorption out from SWNT was also studied in the 0-900 C

Our estimations (Obolensky et al., 2011b) show that at different sorption/desorption cycles the amount of hydrogen located in non-irradiated SWNT was equal to 0.12 ±0.2 mass percent. Hydrogen desorption from treated and exposed to physical sorption/desorption procedure material at pressures ~3000 mbar as it is described above has been studied with the use of mass-spectrometry method within the 0 – 900 °C temperature interval on the MX 7203 mass spectrometer. The dependencies of the amount of hydrogen extracted from nonirradiated (a) and irradiated up to the fluence of 1014 e-/сm2 (b) SWNT samples upon

As can be seen from Figure 5 the amount of hydrogen desorbed from irradiated material is approximately 2.5 times higher compared with that desorbed from the non-irradiated material. We have to draw attention to the fact that all procedures of the sorption/desorption processes were carried out at the 78 – 300 К temperature interval but at the same time significant amount of hydrogen is desorbed at temperatures higher than 300 K. There are additional peaks on the desorption curve which apparently correspond with different

temperature range by mass-spectrometry method on the MX 7203 mass spectrometer.

temperature during container heating for different evacuation rates (Obolensky et al., 2011b)

**3.2. Adsorption studies of irradiated samples** 

temperature are shown in arbitrary units in Figure 5.

following procedure.

**Figure 5.** The dependencies of amount of hydrogen (arbitrary units) exuded from non-irradiated (a) and irradiated up to fluence 1014 e- /сm2 (b) samples upon temperature (Obolensky et al., 2011b)

In order to control the structural transformations of CNTs, it is important to clearly understand the defect generation mechanism and to realize the extent of defects and their influence on sorption properties of CNTs. Acid or alkali treatment does not routinely improve the hydrogen storage capacity of CNT samples. A suitable ball-milling treatment and activation process can open the caps of CNTs and produce more structural defects, and therefore may be beneficial in improving their hydrogen storage properties (Chang & Hui-Ming, 2005). In this connection we investigated the effect of electron irradiation on the hydrogen adsorption property of SWNTs without mechanical milling.

Five AP samples (cf., Table 2) have been annealed in vacuum during 10 hours at 8000C temperature. The first sample (#1) was retained as the control sample. Sample #2 has remained for control and three samples (#3-5) were irradiated with various fluence (5\*1014, 1015 and 2\*1015e- /cm2). After that, four samples (#2-5) were saturated at 10 bar pressure for 3 hours at 78 K temperature..

Postsynthesis Treatment Influence on Hydrogen Sorption Properties of Carbon Nanotubes 175

**Figure 7.** The dependencies of the amount of hydrogen (arbitrary units) exuded from samples (Table 1)

**Figure 8.** The dependence of the additional amount of hydrogen (the difference between saturated and

**Figure 9.** The dependencies of the additional amount of hydrogen (the difference between saturated non-irradiated sample and saturated irradiated samples; arbitrary units) for irradiated samples (Table

non-saturated samples; arbitrary units) exuded from non-irradiated samples (Table 2) upon

upon temperature

temperature

2) upon temperature

**Figure 6.** The dependence of additional amount of hydrogen (arbitrary units) desorbed from irradiated up to fluence 1014 e- /сm2 sample upon temperature (Obolensky et al., 2011b)


Note: For sample #2 Δ H2 - the difference between irradiated and non-irradiated samples. For samples #3-5, ΔH2 thedifference between saturated and non-saturated samples.

**Table 2.** Sample history for adsorption studies

The dependencies of the amount of hydrogen extracted from the samples upon temperature are shown in arbitrary units in Figure 7. As can be seen from this Figure, the desorption curves were displaced in comparison with those for the samples exposed to all stages of treatment (i.e. oxidation, chemical treatment, annealing and milling shown in Figure 5..

For not irradiated samples the curves have remained similar, with some displacement of the maximum peak in the area of lower temperatures for the non-chemically treated and nonmilled sample (2, Table 2). At the same time, the character of the curves for the irradiated samples (3-5, Table 2) essentially differs from the Ref. (Obolensky et al., 2011b). Characteristic peaks in the vicinity of 400 K and 650 K temperatures for the Ref. (Obolensky et al., 2011b) practically do not become visible for samples 3-5 (Table 2). With increase in fluence, the amount of hydrogen desorbed from irradiated samples is reduced for the given range of temperatures (Figure 8 and Figure 9).

As the temperature of samples at irradiation did not exceed 400C (Figure 10), most likely the temperature factor could not affect decrease in the amount of hydrogen desorbed from the irradiated samples in comparison with the non-irradiated samples. This feature needs additional study.

up to fluence 1014 e-

Sample Vacuum anneal

*T* (°C)/time (h)

thedifference between saturated and non-saturated samples. **Table 2.** Sample history for adsorption studies

range of temperatures (Figure 8 and Figure 9).

additional study.

**Figure 6.** The dependence of additional amount of hydrogen (arbitrary units) desorbed from irradiated

Electron irradiation fluence

/cm2)/time (sec)

1 800/10 - - - 2 800/10 - ~78/10 0.13 3 800/10 5\*1014/327 ~78/10 0.12 4 800/10 1015/706 ~78/10 0.16 5 800/10 2\*1015/1340 ~78/10 0.22

Note: For sample #2 Δ H2 - the difference between irradiated and non-irradiated samples. For samples #3-5, ΔH2 -

The dependencies of the amount of hydrogen extracted from the samples upon temperature are shown in arbitrary units in Figure 7. As can be seen from this Figure, the desorption curves were displaced in comparison with those for the samples exposed to all stages of treatment (i.e. oxidation, chemical treatment, annealing and milling shown in Figure 5..

For not irradiated samples the curves have remained similar, with some displacement of the maximum peak in the area of lower temperatures for the non-chemically treated and nonmilled sample (2, Table 2). At the same time, the character of the curves for the irradiated samples (3-5, Table 2) essentially differs from the Ref. (Obolensky et al., 2011b). Characteristic peaks in the vicinity of 400 K and 650 K temperatures for the Ref. (Obolensky et al., 2011b) practically do not become visible for samples 3-5 (Table 2). With increase in fluence, the amount of hydrogen desorbed from irradiated samples is reduced for the given

As the temperature of samples at irradiation did not exceed 400C (Figure 10), most likely the temperature factor could not affect decrease in the amount of hydrogen desorbed from the irradiated samples in comparison with the non-irradiated samples. This feature needs

Hydrogen sorption *T* (K)/P (bar)

ΔH2 (wt%)

/сm2 sample upon temperature (Obolensky et al., 2011b)

(e-

**Figure 7.** The dependencies of the amount of hydrogen (arbitrary units) exuded from samples (Table 1) upon temperature

**Figure 8.** The dependence of the additional amount of hydrogen (the difference between saturated and non-saturated samples; arbitrary units) exuded from non-irradiated samples (Table 2) upon temperature

**Figure 9.** The dependencies of the additional amount of hydrogen (the difference between saturated non-irradiated sample and saturated irradiated samples; arbitrary units) for irradiated samples (Table 2) upon temperature

Postsynthesis Treatment Influence on Hydrogen Sorption Properties of Carbon Nanotubes 177

**Figure 11.** Room-temperature Raman spectra of bundles of arc-derived carbon nanotubes at various

From the analysis of Raman spectra, it follows that the RBM frequency, ωR, is inversely proportional to the tube diameter, d, while its value is up-shifted owing to the intertube interaction within a SWNT bundle (Pradhan et al., 2002). One of the empirical relations between d and ωR, applicable for bundled SWNT is (Pradhan et al., 2002) is d (nm) = [224 cm-1 nm]/ [ω<sup>R</sup> (cm-1) - 12 cm-1]. According to this equation, the main RBM peaks (Figure 12) at 163-166 cm-1 correspond to SWNT with a diameter of ~1.46 nm, whereas the shoulder at

stages of post synthesis (Table 3). The Raman spectra were taken using 514-nm excitation

~150 cm-1 is related to SWNT with a diameter of ~1.62 nm.

**Figure 12.** Raman spectra (RBM) at 514nm laser excitation energy (Table 3)

#### **3.3. Raman scattering studies**

Raman scattering is a sensitive probing of the structure and bonding in carbon materials, particularly carbon nanotubes. Raman scattering spectra for seven sets of samples (cf., Table 2) taken at room temperature in the range 100 to 3200 cm-1 are given in Figures 11-15..

The dominant spectral features include the low-frequency radial breathing modes (RBM) in the range approximately 150 to 200 cm-1 and the higher frequency modes in the range 1300 to 2700 cm-1 (Figure 11).

The SWNT tangential displacement modes observed near approximately 1600 cm-1 (G band) are related to the high frequency vibrational modes of a flat graphene sheet. The band (at 1300 cm-1), commonly called the D band, has been observed in many *sp*2-bonded carbon materials and is associated with disorder in the hexagonal carbon network.


a) AP-SWNT "Carbon Solution"

b) Electron irradiation – 1013 e- /cm2 (time – 375 sec)

c) Sorption – 78 K and 10 bar

d) Heated in 2.6 M HNO3 during 20 hours

e) Electron irradiation – 2\*1013 e- /cm2 (time – 625 sec)

**Table 3.** Sample history for adsorption studies

**3.3. Raman scattering studies** 

to 2700 cm-1 (Figure 11).

a) AP-SWNT "Carbon Solution" b) Electron irradiation – 1013 e-

d) Heated in 2.6 M HNO3 during 20 hours e) Electron irradiation – 2\*1013 e-

**Table 3.** Sample history for adsorption studies

c) Sorption – 78 K and 10 bar

**Figure 10.** The dependence of samples temperature on the irradiation time (fluence 1015e-

Raman scattering is a sensitive probing of the structure and bonding in carbon materials, particularly carbon nanotubes. Raman scattering spectra for seven sets of samples (cf., Table

The dominant spectral features include the low-frequency radial breathing modes (RBM) in the range approximately 150 to 200 cm-1 and the higher frequency modes in the range 1300

The SWNT tangential displacement modes observed near approximately 1600 cm-1 (G band) are related to the high frequency vibrational modes of a flat graphene sheet. The band (at 1300 cm-1), commonly called the D band, has been observed in many *sp*2-bonded carbon

1 AP SWNTs a), irradiation b) - 21-31 2 AP SWNTs a) irradiation b), sorption c) - 21-31 3 AP SWNTs a), sorption c) 1000/20 21-31 4 Treated d), milling, sorption c) 1000/20 6-9 5 Treated d), milling, irradiation b) - 6-9 6 Treated d), milling, irradiation b), sorption c) - 6-9 7 Treated d), milling, irradiation e), sorption c) 1000/20 6-9

*T* (°C)/time (h)

2) taken at room temperature in the range 100 to 3200 cm-1 are given in Figures 11-15..

materials and is associated with disorder in the hexagonal carbon network.

Sample Sample history Vacuum anneal

/cm2 (time – 375 sec)

/cm2 (time – 625 sec)

/cm2)

Metal (at. %)

**Figure 11.** Room-temperature Raman spectra of bundles of arc-derived carbon nanotubes at various stages of post synthesis (Table 3). The Raman spectra were taken using 514-nm excitation

From the analysis of Raman spectra, it follows that the RBM frequency, ωR, is inversely proportional to the tube diameter, d, while its value is up-shifted owing to the intertube interaction within a SWNT bundle (Pradhan et al., 2002). One of the empirical relations between d and ωR, applicable for bundled SWNT is (Pradhan et al., 2002) is d (nm) = [224 cm-1 nm]/ [ω<sup>R</sup> (cm-1) - 12 cm-1]. According to this equation, the main RBM peaks (Figure 12) at 163-166 cm-1 correspond to SWNT with a diameter of ~1.46 nm, whereas the shoulder at ~150 cm-1 is related to SWNT with a diameter of ~1.62 nm.

**Figure 12.** Raman spectra (RBM) at 514nm laser excitation energy (Table 3)

The intense Raman G-band at a higher energy corresponds to the C–C stretching vibrations in tangential and axial directions of the SWNT that splits to G- (tangential) and G+ (axial) bands located at 1566-1571 cm-1 and 1588-1602 cm-1, respectively. The shape of the G- -band is sensitive to the electronic properties (strongly related to chirality) of SWNT.

Postsynthesis Treatment Influence on Hydrogen Sorption Properties of Carbon Nanotubes 179

Intensity of peak D for sample #6 which differed from sample #5 only on stages of hydrogen sorption is a little bit lower (0.275; I(D)/I(G)= 1.389, fig.14), but considerably exceeds intensity of peak D for samples #1-3. Apparently, during hydrogen sorption there was

Addition to the above-stated procedures of high-temperature heating in vacuum (samples #7 and #4) leads to essential decrease in intensity of peak D (0.062 and 0.107; I(D)/I(G)= 0.185 and 0.239, Figure 14). Most likely, at once two factors here dominate: treatment due to

Range G' (2672-2686 cm-1, Figure 15) which characterizes presence of "positive" or "negative" defects in SWCNT is submitted in spectra and has the obvious tendency: hydrogen sorption lowers intensity of this peak and leads to displacement of peak "to the left" in short-wave

The amount of hydrogen desorbed from non-irradiated samples was 0.12 ±0.2 mass percent. The significant increase (more than two times) of hydrogen mass absorbed in irradiated

irradiated with fluences more than 1014 e-/сm2 the decrease of hydrogen desorption was

/сm2) relative to non-irradiated ones has been proved. For samples

"treatment" of defects due to introduction of hydrogen in vacant sites of SWCNT.

heating and treatment due to formation of С-Н bond.

**Figure 15.** Raman spectra (G' band) at 514nm laser excitation energy (Table 3)

*National Aerospace University "Kharkov Aviation Institute", Ukraine* 

Michail Obolensky, Andrew Kravchenko and Vladimir Beletsky

area of a spectrum.

**4. Conclusion** 

**Author details** 

observed.

SWCNT samples (1014 e-

Andrew Basteev and Leonid Bazyma

*V.N. Karazin Kharkiv National University, Ukraine* 

**Figure 13.** Raman spectra (D band) at 514nm laser excitation energy (Table 3)

D band (1341-1352 sm-1, Figure 13) testifies to presence in samples of amorphous carbon and defects in structure of SWCNT. The ratio of peak intensity D band to peak intensity G band allows to judge as a level of crystallization and quantity of defects. It is possible to see that for samples which were not exposed to chemical treating and cryogenic milling (#1-3), intensity of peak D is minimal (0.03-0.036; I(D)/I(G)= 0.333-0.793, fig.14) and quantity of defects in structure of SWCNT was small.

Intensity of peak D band culminates for sample #5 (0.498; I(D)/I(G)= 2.129, Figure 14) which was exposed to chemical treating and cryogenic milling, but was not exposed to hightemperature heating in vacuum, to an irradiation and to hydrogen saturation.

**Figure 14.** Distribution of the intensity ratio I(D)/I(G) for samples (Table 3)

Intensity of peak D for sample #6 which differed from sample #5 only on stages of hydrogen sorption is a little bit lower (0.275; I(D)/I(G)= 1.389, fig.14), but considerably exceeds intensity of peak D for samples #1-3. Apparently, during hydrogen sorption there was "treatment" of defects due to introduction of hydrogen in vacant sites of SWCNT.

Addition to the above-stated procedures of high-temperature heating in vacuum (samples #7 and #4) leads to essential decrease in intensity of peak D (0.062 and 0.107; I(D)/I(G)= 0.185 and 0.239, Figure 14). Most likely, at once two factors here dominate: treatment due to heating and treatment due to formation of С-Н bond.

Range G' (2672-2686 cm-1, Figure 15) which characterizes presence of "positive" or "negative" defects in SWCNT is submitted in spectra and has the obvious tendency: hydrogen sorption lowers intensity of this peak and leads to displacement of peak "to the left" in short-wave area of a spectrum.

**Figure 15.** Raman spectra (G' band) at 514nm laser excitation energy (Table 3)

## **4. Conclusion**

178 Hydrogen Storage

The intense Raman G-band at a higher energy corresponds to the C–C stretching vibrations

D band (1341-1352 sm-1, Figure 13) testifies to presence in samples of amorphous carbon and defects in structure of SWCNT. The ratio of peak intensity D band to peak intensity G band allows to judge as a level of crystallization and quantity of defects. It is possible to see that for samples which were not exposed to chemical treating and cryogenic milling (#1-3), intensity of peak D is minimal (0.03-0.036; I(D)/I(G)= 0.333-0.793, fig.14) and quantity of

Intensity of peak D band culminates for sample #5 (0.498; I(D)/I(G)= 2.129, Figure 14) which was exposed to chemical treating and cryogenic milling, but was not exposed to high-

temperature heating in vacuum, to an irradiation and to hydrogen saturation.

**Figure 14.** Distribution of the intensity ratio I(D)/I(G) for samples (Table 3)

bands located at 1566-1571 cm-1 and 1588-1602 cm-1, respectively. The shape of the G-

sensitive to the electronic properties (strongly related to chirality) of SWNT.

(tangential) and G+ (axial)


in tangential and axial directions of the SWNT that splits to G-

**Figure 13.** Raman spectra (D band) at 514nm laser excitation energy (Table 3)

defects in structure of SWCNT was small.

The amount of hydrogen desorbed from non-irradiated samples was 0.12 ±0.2 mass percent. The significant increase (more than two times) of hydrogen mass absorbed in irradiated SWCNT samples (1014 e- /сm2) relative to non-irradiated ones has been proved. For samples irradiated with fluences more than 1014 e-/сm2 the decrease of hydrogen desorption was observed.

## **Author details**

Andrew Basteev and Leonid Bazyma *National Aerospace University "Kharkov Aviation Institute", Ukraine* 

Michail Obolensky, Andrew Kravchenko and Vladimir Beletsky *V.N. Karazin Kharkiv National University, Ukraine* 

Yuri Petrusenko, Valeriy Borysenko, Sergey Lavrynenko *National Science Center - Kharkov Institute of Physics and Technology, Ukraine* 

Oleg Kravchenko and Irina Suvorova *A.N. Podgorny Institute for Mechanical Engineering Problems, Ukraine* 

Vladimir Golovanevskiy *Western Australian School of Mines, Curtin University, Australia* 

## **Acknowledgement**

This research was supported by Science and Technological Center in Ukraine, project #4957. The Raman measurements were performed at the Physics Institute of the Penn State University by Dr. Humberto R. Gutierrez and Dr. Xiaoming Liu.

**Chapter 8** 

© 2012 Mu Jo, licensee InTech. This is an open access chapter distributed under the terms of the Creative Commons Attribution License (http://creativecommons.org/licenses/by/3.0), which permits unrestricted use,

distribution, and reproduction in any medium, provided the original work is properly cited.

© 2012 Mu Jo, licensee InTech. This is a paper distributed under the terms of the Creative Commons Attribution License (http://creativecommons.org/licenses/by/3.0), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

Since the excellent 6 to 8 wt% hydrogen storage using carbon nano-materials at room temperature and with atmospheric pressure was first reported in [3], several studies on hydrogen storage using SWNT, MWNT, GNF, active carbon, and active carbon fibers etc.,

The hydrogen is a clean fuel source, which produces water vapor as the only exhaust gas when it is burnt with oxygen. The chemical energy density of hydrogen (142 MJ/kg) is at least three times larger than that of other chemical fuels. When the hydrogen is electrochemically burnt using a fuel cell system, the efficiency can reach 50~60%, twice as much as the thermal process because the efficiency of the direct process of electron transfer from oxygen to hydrogen in a fuel cell system is not limited by the Carnot efficiency in [1]. However, the hydrogen volume is 3000 times higher than that of gasoline at room temperature and atmosphere because it is a molecular gas. Therefore, on-board hydrogen energy storage need compact, light, safe and affordable containment. The condensation of a monolayer of hydrogen on a solid leads to a maximum of 1.3x10–5 mol/m2 of adsorbed hydrogen. For automotive applications, the US DOE required a hydrogen storage capacity of greater than 6.5 wt% and ambient temperatures for hydrogen release and moderate storage pressures for industrial applications. Hydrogen storage in carbon materials is a very attractive field since high gravimetric storage capacities may be possible owing to the low specific weight and high specific surface area of carbon. The reversibly adsorbed quantity of hydrogen on nanostructure graphitic carbon amounts to 1.5 mass% per 1000 m2/g of specific surface area at 77 K (liquid nitrogen temperature) in [1]. On active carbon with the specific surface area of 1315 m2/g, 2 mass% of hydrogen was reversibly adsorbed at a temperature of 77 K in [2]. Carbon materials with different nanostructures are available for hydrogen storage, e.g. carbon nanofibers (CNF), graphite nanofiber (GNF), carbon nanohorns, multiwalled carbon nanotubes (MWNT), and single-walled carbon nanotubes (SWNT).

**Electrospun Nanofibrous Materials** 

**and Their Hydrogen Storage** 

Additional information is available at the end of the chapter

Seong Mu Jo

http://dx.doi.org/10.5772/50521

**1. Introduction** 

#### **5. References**

