Electrosynthesis of Hydrogen Peroxide in an Acidic Environment with RuO2 as a Water Oxidation Catalyst & Silver Nanoparticles in Zeolite Y: Surface Enhanced Raman Spectroscopic (SERS) Studies THESIS Presented in Partial Fulfillment of the Requirements for the Degree Master of Science in the Graduate School of The Ohio State University By Kevin D. Cassidy, B.S. Graduate Program in Chemistry The Ohio State University 2011 Committee: Professor Prabir K. Dutta, Advisor Professor Susan V. Olesik Abstract i Hydrogen peroxide (H2O2) was electrosynthesized by reduction of dissolved oxygen in a H2SO4 solution. In the electrosynthesis of H2O2 the evolution of oxygen on the anode is the rate limiting step. To increase the rate of O2 evolution at the reticulated vitreous carbon (RVC) anode, rutile RuO2 was electrodeposited onto the anode. The RVC anode electrodeposited with RuO2 showed a 200 % increase in current efficiency over the plain RVC anode of 16.77 % to 48.08 %, and demonstrated a comparable efficiency to a Pt wire anode. Operational parameters such as H2SO4 concentration, oxygen flow rate, effect of O2 vs. air being pumped into solution, and cathodic potential were systematically studied to improve the current efficiency of the electrochemical cell. Results indicated that the optimal conditions for the generation of H2O2 are a cathodic potential of -0.55 V vs. Ag/AgCl reference electrode, oxygen flow rate of 100 units, 0.1 M H2SO4 concentration, and O2 gas pumped into solution. ii Abstract ii Previous studies have shown that when silver nanoparticles are in close proximity (1-2 nm) and exposed to visible light the resulting electric fields overlap and produce a strong surface-enhanced Raman spectroscopy (SERS) signal greater than a single particle’s response. The difficulty lies in producing silver particles that are both of the proper size (no greater than 20 nm) and proximity. Zeolite Y is a mesoporous and microporous material whose structure’s pore size and distance between pores would be ideal to use as a platform for silver nanoparticle synthesis. The zeolite framework contains cations that are readily exchanged with silver ions and the pore size itself would prevent the silver from aggregating into an unsuitable size. In this work silver was ion-exchanged into Na zeolite Y from a 0.1 M AgNO3 solution. The Ag+ zeolite Y was then reduced with Hydrazine (N2H4) to form silver nanoparticles inside the zeolite cages. By varying the concentration of the hydrazine and injecting the hydrazine in portions over time a SERS capable platform was produced. iii Dedicated to my family and friends for keeping me sane iv Acknowledgements I would like to thank my advisor Dr. Prabir K. Dutta for his patience and guidance throughout my research projects. I would also like to thank for their suggestions and support past and present group members: John Spirig, William Schumaker, Toni Ruda, Haoyu Zhang, Joe Obirai, Cheruvallil Rajesh, Supriya Sabbani, Xiaogan Li, Weizhen Xiong, Brian Peebles, Jeremy White, Adedunni Adeyemo, Julia Rabe, Michael Severance, Betsy Heck, Andrew Zane, Suvra Mondal, Joselyn Del Pilar, and Prasenjit Kar. v Vita April 3rd, 1982.....................................................................Born – Portsmouth, OH 2005.......................................................................B.S. Chemistry, Shawnee State University 2006-present...........................................................Graduate Teaching Associate, The Ohio State University Fields of Study Major Field: Chemistry Minor Field: Analytical Chemistry vi Table of Contents Page Abstract..................................................................................................................ii Dedication.............................................................................................................iv Acknowledgements................................................................................................v Vita........................................................................................................................vi List of Tables..........................................................................................................x List of Figures.......................................................................................................xii Chapters: 1 Electrosynthesis of Hydrogen Peroxide in an Acidic Environment with RuO2 as a Water Oxidation Catalyst 1.1 Introduction.........................................................................................1 1.2 Experimental.......................................................................................10 1.2.1 Voltage Selection……………………………………………..…10 1.2.2 Cell…………………………………………………...........……..10 1.2.3 Electrode Holders……………………………………………….17 1.2.4 Membrane……………………………………………..…………22 1.2.5 Electrodes………………………………………………..………25 1.2.6 Electrosynthesis…………………………………………………30 1.2.7 Electroparamagnetic Resonance (EPR)……………………...31 1.3 Results and Discussion......................................................................32 vii 1.4 Conclusion.........................................................................................43 1.5 References........................................................................................44 2 Silver Nanoparticles in Zeolite Y: Surface Enhanced Raman Spectroscopic (SERS) Studies 2.1 Introduction........................................................................................48 2.1.1 Motivation……………………….............................................48 2.1.2 Previous Studies on SERS Substrates.................................52 2.2 Experimental......................................................................................56 2.2.1 Silver Loading and Reduction……………………………........56 2.2.2 X-ray Diffraction (XRD)……………………….........................57 2.2.3 Raman Spectroscopy…………………………………………..58 2.3 Results and Discussion......................................................................58 2.3.1 Formation of Highly Reduced Silver Zeolite.........................58 2.3.2 Raman Studies on Highly Reduced Silver Zeolite with Pyridine as Analyte........................................................................64 2.3.3 Raman Studies with Partially Reduced Silver Zeolites with Pyridine as Analyte........................................................................81 2.3.4 Raman Studies with Partially Reduced Silver Zeolites with Benzenethiol as Analyte................................................................87 2.3.5 SERS Sample Preparation by Initial Hydrazine Reduction Followed by Laser Reduction........................................................87 2.3.6 SERS Sample Preparation by Simultaneous Hydrazine and Laser Reduction............................................................................88 viii 2.3.7 SERS sample preparation by initial hydrazine reduction followed by photolysis of solid surface..........................................89 2.3.8 SERS Sample Preparation by Initial Hydrazine Reduction Followed by Photolysis of the Entire Sample................................90 2.4 Conclusion.......................................................................................109 2.5 References......................................................................................110 Bibliography………………………………………..…………………………………115 ix List of Tables Table 1.1: Common Industrially Available Oxidants..............................................3 Table 1.2: Plain RVC Working Electrode/Pt Wire Auxiliary Electrode.................33 Table 1.3: Plain RVC Working Electrode/Ruthenium (II) Oxide-Modified RVC...34 Table 1.4: Plain RVC Working Electrode/Plain RVC Auxiliary Electrode............35 Table 2.1: Pyridine Peak Assignment..................................................................68 Table 2.2: SER Spectral Data (cm-1) and Vibrational Assignments of Benzenethiol Adsorbed on Silver Powder............................................................94 x List of Figures Figure 1.1: Reactions of the AO process...............................................................6 Figure 1.2: Simplified Riedl-Pfleiderer Reaction....................................................7 Figure 1.3: Reduction Peak Position....................................................................11 Figure 1.4: Effect of De-Aerating the Solution.....................................................12 Figure 1.5: Initial Cell Design...............................................................................13 Figure 1.6: Tubular U-Shaped Cell Design..........................................................14 Figure 1.7: Current Cell Design...........................................................................16 Figure 1.8: Initial Teflon Electrode Holders (Images a and b are the lids for the anodic compartment, images c and d are for the cathodic compartment)...........18 Figure 1.9: Platinum Wire Electrode Holder........................................................19 Figure 1.10: Teflon Electrode Holder with Sleeve................................................21 Figure 1.11: NAFION® Chemical Formula...........................................................23 Figure 1.12: Electrodeposition of RuCl3 on RVC.................................................26 Figure 1.13: SEM Images of the RVC Foam Before and After Depositing RuO2 ............................................................................................................................28 xi Figure 1.14: RVC Anode After Decomposition in Cathodic Solution...................36 Figure 1.15: RVC Anode After Decomposition Dried...........................................37 Figure 1.16: RVC Anode Before Run in 1 M Sulfuric Acid...................................38 Figure 1.17: Plain RVC Dry..................................................................................39 Figure 2.1: Raman Scattering..............................................................................55 Figure 2.2: Comparison of Synthesized Nano-Scale Zeolite Y (Upper) to that of the Previously Characterized Nano-Scale Zeolite Y Standard (Lower)...............61 Figure 2.3: TEM of Excess Hydrazine Treated Ag+ Zeolite Y..............................62 Figure 2.4: XRD Pattern of Nano-Scale Zeolite Y Ion-Exchanged with 0.1M AgNO3 and Reduced with Hydrazine. Pattern Matches for Silver (Upper) and Zeolite Y (Lower) are Included for Comparison...................................................63 Figure 2.5: Liquid Pyridine (b), Aqueous Pyridine (c) Raman Spectra................66 Figure 2.6: SERS Spectra of Pyridine on Silver..................................................67 Figure 2.7: Raman Spectra of 0.1M Pyridine Solution at 3.2 mW Power with a 633 nm Excitation Line........................................................................................69 Figure 2.8: 3.2 mW Power Scan with a 633 nm Excitation Line of a 0.1 M Pyridine Solution on Nanoscale Ag Zeolite Y......................................................70 Figure 2.9: Nanoscale Ag Zeolite with 0.1 M Pyridine 0.4 mW Power 633 nm Excitation Line.....................................................................................................71 xii Figure 2.10: Micronscale Ag Zeolite with 0.1 M Pyridine 3.2 mW Power with a 633 nm Excitation Line.........................................................................................72 Figure 2.11: BaSO4 Raman Spectrum at 3.2 mW Laser Power with a 633 nm Excitation Line......................................................................................................75 Figure 2.12: BaSO4 Pellet with Ag Zeolite Y with 0.1 M Pyridine Cycling Focus Scan at 3.2 mW Laser Power with a 633 nm Excitation Line..............................76 Figure 2.13: BaSO4 pellet with Micron Ag Zeolite Y with 0.1 M pyridine at 3.2 mW Laser Power with a 633 nm Excitation Line.........................................................77 Figure 2.14: pH dependence of Pyridine/Pyridinium Conversion........................78 Figure 2.15: Calcined Ag Zeolite Y Pellet with 0.1 M Pyridine at 3.2 mW Laser Power with a 633 nm Excitation Line...................................................................79 Figure 2.16: Calcined Ag Zeolite Y Pellet with 0.1 M Pyridine Evaporated at 3.2 mW Laser Power with a 633 nm Excitation Line..................................................80 Figure 2.17: Controlled Addition of Hydrazine with 0.1 M Pyridine at 3.2 mW Laser Power with a 633 nm Excitation Line.........................................................83 Figure 2.18: 0.1 M Pyridine on Ag Zeolite Y after Laser Illumination 3.2 mW Power off Spot with a 633 nm Excitation Line......................................................84 Figure 2.19: Single Drop 0.1 M Pyridine on Ag Zeolite Pellet at 3.2 mW Laser Power with a 633 nm Excitation Line...................................................................85 xiii Figure 2.20: Single Drop 0.1 M Pyridine on Na Zeolite Pellet at 3.2 mW Laser Power with a 633 nm Excitation Line...................................................................86 Figure 2.21: Raman (top) and SERS spectra (bottom) of benzenethiol..............93 Figure 2.22: Raman Sample Holder 1 cm Wide x 1 cm Long x 1/2 cm Deep......94 Figure 2.23: Raman Spectra of Teflon Wafer at 3.2 mW Laser Power with a 633 nm Excitation Line................................................................................................96 Figure 2.24: 0.1 M Benzenethiol on Ag Zeolite Pressed in Wells at 3.2 mW Laser Power with a 633 nm Excitation Line...................................................................97 Figure 2.25: Signal Intensity of Benzenethiol Concentration 0.1 M Benzenethiol Red and 0.001 M Benzenethiol Black (Spectra Collected at 3.2 mW Laser Power with a 633 nm Excitation Line).............................................................................98 Figure 2.26: 0.001 M Benzenthiol on Ag Zeolite Reduced with 1.90*10-3 M Hydrazine at 3.2 mW Laser Power with a 633 nm Excitation Line......................99 Figure 2.27: 0.001 M Benzenthiol on Ag Zeolite with 9.51*10-3 M Hydrazine Reduction at 3.2 mW Laser Power with a 633 nm Excitation Line....................100 Figure 2.28: 0.001 M Benzenethiol on Ag Zeolite Pressed in Wells at 3.2 mW Laser Power with a 633 nm Excitation Line......................................................101 Figure 2.29: Spectral Shifts for Benzenethiol Binding to Different Cluster Sizes ..........................................................................................................................102 xiv Figure 2.30: Ethanol Raman Spectra at 3.2 mW Laser Power with a 633 nm Excitation Line....................................................................................................103 Figure 2.31: Effect of Hydrazine Concentration with Surface Photolysis Setup (Collected at 3.2 mW Laser Power with a 633 nm Excitation Line)...................104 Figure 2.32: Effect of Hydrazine Concentration with Suspension Photolysis Setup (Collected at 3.2 mW Laser Power with a 633 nm Excitation Line)...................105 Figure 2.33: 2.57 mM Hydrazine Reduction TEM (Top Left is at 50 nm Resolution, Top Right is at 20 nm Resolution, and Bottom is at 100 nm Resolution).........................................................................................................106 Figure 2.34: XRD of Photolyzed Zeolite Y Suspension with 640 C NIST Standard............................................................................................................107 Figure 2.35: XRD of 2.57 mM Hydrazine Reduced Ag Zeolite..........................108 xv Chapter 1 Introduction 1.1.1 Hydrogen Peroxide Wastewater historically was either treated with formaldehyde, chlorine or iron salt, but increasingly there has been a demand for safer and more environmentally friendly methods such as hydrogen peroxide treatment. The concentration of hydrogen peroxide required for wastewater treatment has expensive transportation and storage costs; this led to a demand for a cheaper on-site production method. Traditional techniques of hydrogen peroxide generation involve nonaqueous solvents and dangerous byproducts, whereas electrochemical production minimizes the byproduct formation [1]. By careful selection of electrodes and catalysts hydrogen peroxide can be electrochemically generated from water and oxygen. Hydrogen peroxide is used in a wide range of industries, such as; pulp and paper bleaching, textiles, detergents, electronics, metallurgy, wastewater treatment, and as a chemical oxidizer. Given its decomposition products of water and oxygen, H2O2 is by far a safer alternative than most chemicals used in these industries. There are a wide range of reactions that H2O2 can undergo, seen in equations 1-5. Hydrogen Peroxide can be added to urea to create urea hydrogen peroxide [Eq. (1)], a teeth whitener. Addition: H2O2 + (NH2)2CO (NH2)2CO H2O2 1 (1) H2O2 is considered to be an environmentally safe substance, because when H2O2 decomposes it breaks down into water and oxygen [Eq. (2)]. Decomposition: 2H2O2 2H2O + O2 (2) H2O2 is a strong oxidizing agent [Eq. (3)]. H2O2 is a more efficient oxidizing agent than most other oxidants as can be seen in Table 1.1, H2O2 has a higher active oxygen content than most commercially used oxidants and has a more benign environmental response since it reduces to water during the reaction. Oxidation: H2O2 + M MO + H2O (3) As a reducing agent H2O2 is capable of reducing oxidizing agents stronger than itself [Eq. (4)], such as KMnO4, which is used in this thesis for the determination of H2O2 produced, and Ce(SO4)2, which can also be used to determine the concentration of H2O2. Reduction: H2O2 + Rn+2 Rn +2H+ + O2 (4) H2O2 is also used in organic syntheses for substitution reactions [Eq. (5)]. Substitution: H2O2 + RX ROOH + HX 2 (5) Oxidant Active Oxygen (% w/w) By-Product H2O2 47.1 H2O tBuOOH 17.8 tBuOH HNO3 25 Nox, N2O, N2 N2O 36.4 N2 NaClO 21.6 NaCl NaClO2 35.6 NaCl NaBrO 13.4 NaBr KHSO5 10.5 KHSO4 NaIO4 29.9 NaI PhIO 7.3 PhI Table 1.1: Common Industrially Available Oxidants [2] 3 Hydrogen peroxide (H2O2) was first identified by Louis Jacques Thenard in 1818 as a product of the substitution reaction of barium peroxide and nitric acid, seen in equation 6. BaO2 + 2HNO3 → H2O2 + Ba(NO3)2 (6) Thenard then changed the reaction mixture from nitric acid to sulfuric acid [Eq. (7)]. BaO2 + H2SO4 H2O2 + BaSO4 (7) Prior to the 1940’s most commercial production of H2O2 involved inorganic processes with the electrolysis of an aqueous sulfuric acid solution or acidic ammonium bisulfate (NH4HSO4), followed by hydrolysis of the peroxodisulfate ((SO4)2)2− which is formed, this resulted in a higher concentration of H2O2 produced than the barium salts method. The most widely used current production method of H2O2 began in the 1940’s. This is the anthracene autoxidation process (AO), the main reactions follow the Riedl-Pfleiderer process [3]. A 2-alkylanthraquinone (AQ, typically 2ethylantraquinone) in an appropriate solvent or mixture of solvents is hydrogenated in the presence of a catalyst to a anthraquinol or anthrahydroquinone (AHQ). A side reaction involving the hydrogenation of the unsubstituted aromatic ring in AHQ results in the formation of 5,6,7,8tetrahydroanthrahydroquinone (THAHQ). This side reaction results in the need to replenish the AQ source eventually as the efficiency drops. The AHQ and THAHQ are separated from the catalyst and oxidized in the presence of air to 4 regenerate the AQ and form tetrahydroanthraquinone (THAQ) and an equal amount of H2O2. The series of reactions can be seen in Figure 1.1. A simplified mechanism for the whole reaction can be seen in Figure 1.2, which leads to the overall process governed by the reaction in Eq. 8. H2 + O2 H2O2 (8) This reaction doesn’t take into account the aforementioned, and other, side reactions that lead to a consumption of AQ. Since the process has been used there haven’t been any other methods efficient enough to convince most manufacturers to replace it. There has however been a good deal of research done to enhance the process. Most refinements in the process have had to deal with the catalyst used in the hydrogenation step. This step has the most side reactions occurring out of all of the steps. Ni and Pd catalysts supported on SiO2, Al2O3 or a mixture of Al2O3/SiO2 are the most common catalysts used in industry today [4]. Newer catalysts for this reaction have focused on amorphous Ni/B [5,6] and Ni/Cr/B [7] alloys. If La is added to the Ni/B alloy at an atomic ratio of La/Ni = 0.34 it leads to an increase in the hydrogenation activity. La causes a better dispersion of Ni which results in a greater number of hydrogenation sites [8,9]. The incorporation of the Cr into the Ni/B alloy leads to a greater stability in the reaction system, which results to an increase in yield of H2O2 and a minimization of side reactions [4]. From the 1950’s to 1980 Shell ChemicalTM produced H2O2 from the oxidation of primary and secondary alcohols, producing an aldehyde from 5 Figure 1.1: Reactions of the AO process 6 Figure 1.2: Simplified Riedl-Pfleiderer Reaction 7 primary alcohols and a ketone from secondary alcohols [10, 11]. These reactions can be seen in Equations 9 and 10. CH3-CH2-CH-OH + H2 H2O2 + CH3-CH2-CH=O (9) (10) Due to the solubility of alcohol in the peroxide phase the purity is lower with this method than the AO process. H2O2 was first electrochemically synthesized by Meidinger in 1853. Meidinger oxidized sulfate to persulfate at the anode and then produced H2O2 via the hydrolysis of the persulfate [12] at the cathode. This process was used as the primary synthesis method of H2O2 until the anthraquinone method displaced it. H2O2 can also be synthesized electrochemically by electrolysis of a dilute NaOH solution in an electrolytic cell, this is referred to as the Dow Process. The process involves the following reactions [Eq. 11, 12, 13]. Anode: 2OH- H2O + ½O2 + 2e- (11) Cathode: H2O + O2 + 2e- HO2- + OH- (12) Overall: NaOH + ½O2 HO2Na (13) A cell being supplied with 2.3 V and 62 mA cm-2 yields a NaOH/HO2- weight ratio ranging from 1.6–1.8:1 with a current efficiency of 90%. Pairing the trickle-bed cathode, where a co-current reactant gas and liquid flow through fixed beds of 8 catalyst particles, with an ion-exchange membrane affords a 2.1% w/w HO2solution in 5.0% w/w NaOH and increases current efficiency to 95% [13]. Lobyntseva et al. used a modification of the trickle-bed process above, where the trickle-bed electrode was replaced with a rotating disk cathode consisting of a high-surface area glassy carbon electrode modified with either an athraquinone derivative or gold nanoparticles paired with a platinum foil counter electrode and a saturated calomel reference electrode in a 0.1 M KOH solution [14]. The work done for this thesis is not the first time RVC has been utilized as a cathode material for H2O2 electrosynthesis, nor is it the first time H2O2 has been synthesized in an acidic environment. Alvarez-Gallegos and Pletcher utilized the high-surface area nature of RVC to fabricate a cathode for the electrochemical production of H2O2 for the removal of organics [15]. The solution was kept at an acidic pH due to the presence of Fe(II) as a catalyst for the oxidation of the organic compounds via H2O2. However, this is the first report of using ruthenium oxide on the anode to facilitate the oxygen reduction reaction. 1.1.2 RuO2 as a Water Oxidation Catalyst There has been a great deal of interest of finding catalysts for the splitting of water into hydrogen and oxygen, mostly from those interested in mimicking the process of photosynthesis for energy production. Ruthenium (IV) oxide (RuO2) is a well established water splitting catalyst [16]. RuO2 is an insoluble compound, an important feature for an aqueous system, which can form a rutile crystalline structure when heated to over 200 °C [17]. The mechanism for the oxidation of 9 water on RuO2 is not fully understood. Titanium dioxide (TiO2) is another important water splitting catalyst, which shares a similar structural unit as rutile RuO2 [18]. Along the c-axis of the rutile structure of RuO2, there are ruthenium atoms bridged by two oxygen atoms [17]. If these sites are important then the morphology also plays a role. Experimental 1.2.1 Voltage Selection Oxygen is known to undergo 2 e- and 4 e- reduction on glassy carbon electrodes at around -0.5 V and -0.8 V potential regions [19]. Cyclic voltammetry (CV) was used to probe the reduction potential of oxygen-saturated solution of 1M H2SO4 on the Reticulated Vitreous Carbon (RVC) electrode utilizing a Ag/AgCl reference electrode. The cyclic voltammogram (CV) of the air-saturated solution of H2SO4 is shown below in Figure 1.3. We also interrogated the effects of de-aerating the solution with N2 to see if the reduction waves were actually related to the oxygen. The CVs shown in Figure 1.4 suggested that de-aerating the solution resulted in the loss of the reduction wave related to O2 2e- process. 1.2.2 Cell The first cell design was a glass cube, with the top removed, with a glass divider in the middle to make two compartments. Each compartment was capable of holding 20 mL of solution. A hole was drilled into the divider and a spherical quartz frit was welded into that position, the frit had 5 micron pores. The frit was then coated with a NAFION® membrane, which will be discussed in 10 greater detail in a later section. A lid was placed over top of the cell with a slot to allow the RVC electrode to enter solution, and two small circular holes to allow the insertion of a Ag/AgCl reference electrode in the cathodic compartment and the Pt auxiliary electrode in the anodic compartment. The pore sizes for this frit were too small, which resulted in low concentrations of hydrogen peroxide production. Images of the first cell can be seen in Figure 1.5. The next cell designed revolved around a tubular U shape. A 25-50 micrometer pore size frit was placed in the middle to separate the two compartments. The frit was then coated with a NAFION® membrane. The cell was made of Pyrex of ⅛ inch thickness, the base measured 2 ⅝ inches in length and 1 ¼ inches in width, each cylinder was 3 ⅜ inches tall with an outer diameter of 1 inch. Each compartment was capable of holding a maximum of 28 mL. An additional cell was made identical to this cell; however the frit on the second cell had pore sizes ranging from 50-75 micrometers. This larger pore size however did not prevent hydrogen peroxide from travelling to the anodic compartment. Images for this design can be seen in Figure 1.6. 11 8 7 6 5 Current (mA) 4 3 2 1 0 -1200 -1000 -800 -600 Voltage (mV) Figure 1.3: Reduction Peak Position 12 -400 -200 0 -1 25 8 6 Deaerated Aerated 15 4 10 2 5 0 0 0 -200 -400 -600 Potential (mV) Figure 1.4: Effect of De-Aerating the Solution 13 -800 -1000 Aerated Current (mA) Deaerated Current (mA) 20 Cell cover 20 ml Ag/AgCl ref. electrode 20 ml RVC working electrode Figure 1.5: Initial Cell Design 14 Nafion membrane on quartz filter Platinum aux. electrode O2 Pumped in via Micropipette Teflon® Lids Ag/AgCl Reference Electrode RuO2/RVC Auxiliary Electrode RVC Working Electrode Magnetic Stir Bar Figure 1.6: Tubular U-Shaped Cell Design 15 NAFION® Membrane The current cell design is simply a modification of the previous cell. An Lshaped Pyrex® tube was joined to the cathodic compartment with the center of the tube positioned 2 cm above the base. The tube had an inner diameter of 1 cm. The tube was added to allow the insertion of a gas diffusion tube to minimize formation of oxygen bubbles. In addition, it also prevented O2 bubbles from sticking to the surface of the electrodes and to allow better dispersion of the bubbles into solution. This addition increased the maximum volume of the cathodic compartment to 35 mL. This cell included the frit with pore sizes ranging from 25-50 micrometers. This cell design can be seen in Figure 1.7. 16 Teflon® Electrode Sheaths Ag/AgCl Reference Electrode Gas Diffusion Tube RVC Working Electrode ® Magnetic NAFION Stir Bar Membrane Figure 1.7: Current Cell Design 17 RuO2/RV C Auxiliary Electrode 1.2.3 Electrode Holders Initially the electrodes were suspended in the solution using the tension provided by the connecting wires to keep them from dropping too far into solution, where the wire would touch the solution. The working and auxiliary electrodes would never be the same distance from each other between runs, also the reference electrode would at times touch the working electrode. This resulted in irreproducible runs, and it was decided that holders would have to be fabricated for the electrodes in order to minimize variations between runs. The first cell holders that were designed for the RVC electrodes were Teflon® lids sized to fit snugly on the tubes of the electrochemical cell. The Teflon® lids had slots cut into them for the RVC electrodes to be inserted. A small hole, 3/16 inch diameter, was also drilled into the Teflon® lid that was to go over the working electrode compartment to allow for the Ag/AgCl reference electrode to be inserted. A larger hole, ¼ inch diameter, was drilled behind the smaller hole to allow the insertion of a tube for pumping in gas. These lids can be seen in Figure 1.8. The cell holder designed for the platinum wire electrode was a Pyrex lid with a ⅛ inch diameter tube of 2 ¾ inches in length fused to the lid. The tubing had several small, ⅛ inch by ¼ inch, slots cut into to allow the solution easier access to the platinum wire and yet still hold the wire in position. The lid was sized to fit snugly on top of the auxiliary compartment tube. The Pyrex® lid can be seen in Figure 1.9. 18 Figure 1.8: Initial Teflon® Electrode Holders (Images a and b are the lids for the anodic compartment, images c and d are for the cathodic compartment) 19 Figure 1.9: Platinum Wire Electrode Holder 20 The Teflon® lids did help stabilize the electrodes, however they still allowed the electrodes to move around in the solution. The lids also added extra mechanical stress onto the electrodes. Because the alligator clip connects the electrodes to the voltage source was much heavier than the electrodes it caused the electrodes to rest on the slots to stabilize their positions. This combined with the fragility of the electrodes themselves resulted in many broken electrodes. Also gas being pumped in caused the electrodes on the working compartment, (which was the only compartment that had gas being pumped into solution) to jump up and down which added to the mechanical stress being applied to the electrodes. The current holder was designed to help alleviate this mechanical stress placed on the electrodes. In order to minimize the stress placed on the electrodes it was decided the wires attached to the electrode would first be wrapped around a screw and then the voltage supplier would be connected to the screw via an alligator clip. The electrodes themselves would be inserted into an open sleeve attached to the lid, the sleeve had windows cut into it to allow the solution greater access to the electrode. The sleeve and the lid were made from Teflon®. The sleeve was attached to the lid with nylon cotter pins. The lid also had a 3/16 inch diameter hole drilled into it behind the slot where the sleeve was attached, for the insertion of the Ag/AgCl reference electrode. The larger hole was removed from this design as the cell itself was redesigned for the pumping of gas. The most current holder can be seen in Figure 1.10. 21 Figure 1.10: Teflon® Electrode Holder with Sleeve 22 1.2.4 Membrane The electrochemical separation of the two compartments was achieved using a NAFION® 117 membrane deposited on the filter. The membrane formation used a NAFION® solution using ethanol as solvent. The NAFION® solution is deposited onto a glass frit in the electrochemical cell on both sides and allowed to dry, excess residue on the glass is removed with ethanol. NAFION® was chosen for its high degree of OH- ion rejection which is needed for hydrogen peroxide electrosynthesis. The chemical formula for NAFION® can be seen in Figure 1.11 [20]. NAFION® has excellent permeselectivity to protons, the transference number of H+ ions remains constant at unity until an external H2SO4 concentration of 2 M is reached [21]. It is necessary to regenerate the NAFION® membrane after a few hundred hours of use as polymer degradation can become a problem [22-24]. The old membrane is removed with ethanol and a new one is deposited onto the glass frit. Some suspect that membrane degradation is mainly caused by chemical attack of the polymer [21, 25]. Previous work has suggested that hydroxyl free radicals, generated from homolytic cleavage of H2O2 catalyzed by metal impurities, can attack polymer end groups having H-containing terminal bonds (such as –CF2COOH) that are formed during membrane processing [5]. Carbon radicals in the electrode and unknown radical centers in the membrane have been identified in a PEM fuel cell using electron spin resonance (ESR) [26, 27]. 23 Figure 1.11: NAFION® Chemical Formula 24 1.2.5 Electrodes Two sizes of reticulated vitreous carbon (RVC) foams were obtained from ERG Materials and Aerospace Corporation: ~2x125x125 mm and 4x125x125 mm, of 100 pores per inch (ppi) and 60 ppi, respectively. For a preliminary investigation, the 2x125x125 mm RVC was used to determine the reduction potential of oxygen in 1.0 M H2SO4. To achieve this, 2x5x40 mm RVC was cut from the as-received RVC and used as the working electrode in a three electrode electrochemical cell. The reference electrode was a Ag/AgCl (saturated with 3 M KCl) electrode and a coiled platinum wire was used as the counter electrode. The electrochemical synthesis of H2O2 in this project requires a specially prepared anode made of RuO2 deposited on a conducting material, carbon was chosen as the conducting material for this experiment. Two different methods of depositing RuO2 are investigated. The first method was a cathodic electrochemical deposition of a 5 mM solution of RuCl3 followed by thermal oxidation of the RuCl3 to RuO2 in a furnace, following the procedure used by Hu et al [29]. The second approach involved soaking the RVC in a saturated solution of RuCl3 and allowing the material to dry followed by thermal oxidation of the RuCl3 to RuO2 in a furnace. For the electrochemical deposition, 60 voltammetric cycles, at a rate of 50 mV/s, were performed and the features of the voltammograms were used to monitor the progress of the electrodeposition. The deposition bath consisted of 5 mM RuCl3:xH2O in 0.1M NH4Cl + 0.01M HCl in the cathodic compartment and 0.1M NH4Cl + 0.01M HCl in the anodic compartment. A Ag/AgCl reference 25 electrode and a Pt wire counter electrode were used. Though the voltammograms [Figure 1.12] were almost featureless, the growth of the deposited film could be ascertained from the oxidation potential around 0.6 V which shifted to 0.4 V as the deposition continued. The deposition was stopped after 60 voltammetric cycles and the electrode was rinsed with distilled water before transferring into a furnace and heat treated at 200 °C for 10 hrs. The second approach of depositing the ruthenium oxide on the RVC was to soak the RVC in a saturated solution of RuCl3. Several drops of a saturated RuCl3 solution in ethanol were placed on the RVC and allowed to dry each time. The dropping was continued until 2 ml content of the ethanol solution had been used. This was to make sure that enough quantity of the RuCl3 had been soaked onto the RVC. Following this, the RuCl3+RVC material was transferred into a furnace and heat treated at 250 °C for 10 hrs. The resultant material was washed with water and baked in the oven for about 5 hrs before analysis. It was observed that the washed material still had a lot of RuCl3 based on the brown residue that formed from the washing. 26 10 8 6 Current (mA) 4 -400 2 0 -200 -2 -4 0 200 400 60th -6 -8 Voltage (mV) Figure 1.12: Electrodeposition of RuCl3 on RVC 27 600 800 1000 1st 1200 The SEM images of the materials suggest that the electrochemical route gave a better surface modification than the solution-based process (Fig 1.13). The experiment therefore adopted the electrochemical deposition method for the anode preparation. It seems that while the SEM image shows that the ruthenium oxide had been deposited on the RVC, there might be some layer of the RuCl3 in-between the ruthenium oxide and the RVC surface thus making the electron transfer process from the oxide inaccessible to the RVC. 28 Plain as-received RVC Electrodeposited RuO2 on RVC Deposited RuO2 on RVC via ethanolic RuCl3:xH2O Figure 1.13: SEM Images of the RVC Foam Before and After Depositing RuO2 29 1.2.6 Electrosynthesis All electrosynthesis runs were performed with an EG&G Princeton Applied Research Model 273 Potentiostat/Galvanostat. Electrosynthesis runs were performed in a three electrode cell as described previously. Electrosynthesis runs were conducted under chronoamperometric mode with the following settings; purge time was passed, equilibriation time was set to 120 s, initial voltage of -0.550 V, final voltage of -0.551 V, run time of 3600 s, current maximum of 1 A, time/pt 5.000s, number of points 730, calibrated for a Ag/AgCl reference electrode. Chronoamperometry was chosen after voltage fluctuations were observed during a controlled potential run; by choosing two voltages close together in value one can simulate a controlled potential run using chronoamperometry. In order for the solution to be fully saturated with oxygen, oxygen is pumped into the solution for 15 minutes prior to a run. Initially oxygen was pumped into solution via a micropipette connected to an oxygen tank; the micropipette was inserted into the cathodic compartment behind the working electrode. A flow meter was used to control and monitor flow rate. This set up, particularly with the initial electrode holders, caused the electrodes to jostle violently causing structural damage to the electrodes. In this setup the bubbles from the introduced oxygen would often cling to the surface of the RVC electrodes thereby reducing usable surface area for the reaction. A stir bar was introduced into the cathodic compartment to try to remove 30 any clinging oxygen bubbles from the surface of the electrodes. The stir bar did help remove some of the clinging bubbles, but did not remove all of them. The cell was then redesigned, which can be seen above, by adding a Lshaped tube to the cathode compartment where oxygen could be bubbled into solution safely away from the electrode. The micropipette was exchanged with a gas diffusion tube as the method of introduction for the oxygen gas. This setup allowed the bubbles to then disperse into solution with no large clinging bubbles on the surface of the electrodes being observed. 1.2.7 Electron Paramagnetic Resonance EPR Possible radical presence was determined using Electron Paramagnetic Resonance (EPR) spectroscopy. Four samples of RVC electrodes were scanned using EPR; all samples were suspended in 1 mL of solution and placed into a capillary tube. The first sample consisted of RVC electrode that decomposed after ten reduction cycles suspended in 1 mL of the cathodic compartment solution. The second sample consisted of RVC electrode that decomposed after ten reduction cycles suspended in 1 mL of nanopure water. The third sample consisted of unused RVC suspended in 1 mL of 1 M H2SO4. The fourth sample consisted of unused RVC suspended in 1 mL of nanopure water. All EPR spectra were collected on a Bruker ESP300 spectrometer. Each spectrum consisted of 5 scans performed at 20 mW, with a modulating frequency of 100 kHZ, an amplitude of 0.525 Gauss, a microwave frequency of 9.77 GHz, and a center field of 3450 Gauss with a sweep width of 100 Gauss. 31 1.3 Results and Discussion Chronoamperometry measures the current as a function of time. By integrating the graph of current versus time, one can determine the total amount of charge (Q) passed during the trial. This Q value can then be used to determine the theoretical number of moles of oxygen reduced to hydrogen peroxide. The following equation was used to determine the theoretical number of moles of oxygen reduced from the Q values Moles = (Q/nF) (EQ 1) where Q is the total amount of charge passed during a trial; n is the number of electrons; and F is the Faraday constant. Potassium permanganate titrations, using 2 mM KMnO4, were performed on samples removed from the cathode compartment to determine experimentally the concentration of hydrogen peroxide generated during a trial. By comparing the theoretical number of moles of oxygen reduced to the experimentally determined number of moles reduced, the efficiency of the cell can be determined using the following equation. Efficiency = Experimental Number of Moles Reduced *100 Theoretical Number of Moles Reduced (EQ 2) Trial hydrogen peroxide generations were performed using the previously described experimental setup and a plain as-received RVC working electrode, Ag/AgCl reference electrode, and coiled Pt wire auxiliary electrode. The results can be seen in the table 1.2. The efficiencies for the trials were averaged to be 33.3 ± 5.4. Trial hydrogen peroxide generations were then performed using a plain 32 as-received RVC working electrode, Ag/AgCl reference electrode, and ruthenium (II) oxide-modified RVC auxiliary electrode. The results can be seen in the table 1.3. The efficiencies for the trials were averaged to be 33.56±6.47. Trial hydrogen peroxide generations were then performed using a plain as-received RVC working electrode, Ag/AgCl reference electrode, and a plain asreceived RVC auxiliary electrode. The results can be seen in the table 1.4. The efficiencies for the trials were averaged to be 16.77±3.89. 33 Table 1.2: Plain RVC Working Electrode/Pt Wire Auxiliary Electrode 34 Table 1.3: Plain RVC Working Electrode/Ruthenium (II) Oxide-Modified RVC Auxiliary Electrode 35 Table 1.4: Plain RVC Working Electrode/Plain RVC Auxiliary Electrode 36 The efficiency averages for the first two sets of experiments show comparable results using the Pt wire auxiliary electrode and the cheaper alternative of the ruthenium (II) oxide-modified RVC auxiliary electrode. While using plain RVC on both sides of the electrochemical cell produced resulted in over a 50% drop in efficiency compared to both the trials using RuO2 modified RVC as the anode and the trials using Pt wire as the anode. Qiang et. al. reported obtaining current efficiencies of 81% [28]. In this study pH was controlled using a pH-stat (Model pH-40, New Brunswick Scientific Co., Edison, NJ), HClO4 (1 M) and NaOH (1 M) solutions. Temperature was controlled using a thermostat (Model EX-200, Brookfield Engineering Laboratories, Inc., Stoughton, MA) and a water bath. This study included the use of sodium perchlorate (NaClO4) as an inert supporting electrolyte. Hydrogen peroxide generations had run times of 7200 s, which is twice what was performed in these experiments. They observed significant H2O2 degradation at elevated temperatures (greater than 23 ºC). The work involved in this present study did not optimize pH, temperature, or vary the run times of experiments. These optimizations could lead to possible increases in current efficiency. Gallegos reported obtaining current efficiencies of 20% at -1.5 V (vs. stainless steel), but drops to 10% at -2.0 V [29]. Utilizing voltages in this range involved competing 2 electron and 4 electron oxygen reductions. Voltages in this range can also lead to hydrogen gas evolution. Gallegos’ research involved the use of a stainless steel anode with the possibility of Fe3+ and Fe2+ ions dissolving into solution. Fe(II) is known to react with H2O2 to form the Fenton reagent, thus 37 lowering current efficiency [30]. Anodic decomposition occurs in the RVC electrodes, resulting in electrode failure after approximately 10 trial runs. EPR was performed in order to detect the presence of free radicals thought to responsible for the degradation of the anodes. Four samples were prepared; the first sample was taken from an anode after decomposition occurred with the anodic solution and can be seen in Figure 1.14, the second sample consists of a portion taken from a decomposed anode dried to see if the free radical was in the solution or on the electrode and can be seen in Figure 1.15, the third sample was taken from a piece of RVC anode before any runs and placed in 1 M sulfuric acid to see if the RVC anode itself contained anything that would be detected by EPR shown in Figure 1.16, the fourth sample was a piece of plan RVC anode material shown in Figure 1.17. Large peaks shown in Figures 1.14 and 1.15 clearly indicated the presence of unpaired electrons. Figures 1.16 and 1.17 showed no visible peaks indicating an absence of unpaired electrons. All EPR spectra were taken one week after decomposition occurred, this rules out the detection of any short lived free radical species, such as hydroxyl radicals [31]. It is possible that during the reaction a reactive oxygen species reacted with the anode causing its degradation. The observation of carbon-centered radicals by EPR suggests that these intermediates which exhibit extremely long lifetimes, detectable for months after being created [32] may be involved in the degradation. 38 Intensity Gauss Figure 1.14: RVC Anode After Decomposition in Cathodic Solution 39 Intensity Gauss Figure 1.15: RVC Anode After Decomposition Dried 40 Intensity Gauss Figure 1.16: RVC Anode Before Run in 1 M Sulfuric Acid 41 Intensity Gauss Figure 1.17: Plain RVC Dry 42 1.4 Conclusions The RuO2-Modified RVC electrode shows comparable efficiencies to the Pt wire electrodes. The RuO2-Modified RVC electrode does show an advantage over utilizing a plain RVC electrode, which results in a 50 % reduction in hydrogen peroxide production efficiency compared to the RuO2-Modified RVC electrode. Although the RuO2-Modified RVC electrode does show comparable efficiency to the Pt wire electrode the anodic decomposition of the RVC electrode renders it useless for multiple trials. The electrosynthesis of H2O2 on the RVC electrode is resulting in the generation of free radicals, which in turn is eroding the anode. With a more inert supporting material RuO2 should be a good candidate for a water splitting catalyst in the anodic compartment. 43 References 1. Schumb WC, Satterfield CN, Wentworth RL. Hydrogen peroxide Reinhold Publishing Co.: New York, NY, 1955. p. 392, 515, 535-546. 2. Campos-Martin, Jose M.; Blanco-Brieva, Gema; Fierro, Jose L. G. Hydrogen peroxide synthesis : an outlook beyond the anthraquinone process. Angewandte Chemie, International Edition (2006), 45(42), 6962-6984. 3. H.-J. Riedl, G. Pfleiderer (I. G. Farbenindustrie AG.), US2158525, 1939 [Chem. Abstr. 1939, 33, 49 337]. 4. Y. Hou, Y. Wang, F. He, S. Han, Z. Mi, W. Wu, E. Min, Matt. 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Goekdogan, Oezlem; Sulak, Meral; Guelce, Handan. Investigation of oxygen electroreduction on polyvinylferrocene coated glassy carbon electrodes. Chemical Engineering Journal (Amsterdam, Netherlands) (2006), 116(1), 39-45. 16. S. K. Das, P. K. Dutta, Synthesis and characterization of a ruthenium oxide-zeolite Y catalyst for photochemical oxidation of water to dioxygen, Microporous and Mesoporous Materials, 22, (1998), 475-483. 17. J. M. Fletcher, W.E. Gardner, B.F. Greenfield, M. J. Holdoway, M. H. Rand, J. Chem. Soc. (A) (1968) 653. 18. W. Rhittinger, G. C. Dismukes, Chem. Rev. 97 (1997) 1. 19. Xue, T. Mass transfer in Nafion membrane systems: effects of ionic size and charge on selectivity Journal of Membrane Science, v. 58 issue 2, 1991, p. 175. 20. Pourcelly, Gerald; Lindheimer, Arlette; Gavach, Claude; Hurwitz, Henry D. Electrical transport of sulfuric acid in Nafion perfluorosulphonic membranes. Journal of Electroanalytical Chemistry and Interfacial Electrochemistry (1991), 305(1), 97-113. 45 21. D.E. Curtin, R.D. Lousenberg, T.J. Henry, P.C. Tangeman, M.E. Tisack, J. Power Sources 131 (2004) 41. 22. E. Endoh, S. Terazono, H.Widjaja, Y. Takimoto, Electrochem. Solid-State Lett. 7 (2004) A209. 23. S.D. Knights, K.M. Colbow, J. St-Pierre, D.P.Wilkinson, J. Power Sources 127 (2004) 127. 24. M. Pianca, E. Barchiesi, G. Esposto, S. Radice, J. Fluorine Chem. 95 (1999) 71. 25. A. Panchenko, H. Dilger, E. M¨oller, T. Sixt, E. Roduner, J. Power Sources 127 (2004) 325. 26. C.-C. Hu, K.H. Chang, Electrochim. Acta 45 (2000) 2685. 27. G. Hubner, E. Roduner, J. Mater. Chem. 9 (1999) 409. 28. Qiang, Zhimin. Electrochemical generation of hydrogen peroxide from dissolved oxygen in acidic solutions Water Research, v. 36 issue 1, 2001, p. 85. 29. Gallegos, Alberto Alvarez; Garcia, Yary Vergara; Zamudio, Alvaro. Solar hydrogen peroxide. Solar Energy Materials & Solar Cells (2005), 88(2), 157-167. 30. Schumb WC, Satterfield CN, Wentworth RL. Hydrogen peroxide Reinhold Publishing Co.: New York, NY, 1955. p. 392, 515, 535-546. 31. Sutherland, R. A.; Anderson, R. A. Journal of Chemical Physics (1973), 58(3), 1226-34. 46 32. Yordanov, N.D. Introdcution to the theory of Electron Paramagnetic Resonance and its application to the study of aerosols. In Analytical chemistry of aerosols, Spurny, K. R., Ed. Lewis: Boca Raton, 1999; pp 197-213. 47 Chapter 2 2.1 Introduction 2.1.1 Motivation Traditional Raman scattering is a weak phenomenon, as the scattering observed is the result of weak inelastic scattering as compared to a more intense elastic Rayleigh scattering. Traditional Raman spectroscopy typically has a detection limit no greater than 0.1 M [1, 2]. The ultimate goal in chemical detection is the ability to detect the presence of single molecules/atoms, which cannot be accomplished with normal Raman spectroscopy. Sample fluorescence in the scanning range can also obscure important peak information in addition to the already weak signal. Raman scattering is the result of scattering with a change in frequency, corresponding to a change in the vibrational energy of a molecule. The Raman effect can be visualized as a transition from the ground state to a virtual excited state, followed by subsequent scattering to a vibrationally excited state. There are mainly three possible scattering mechanisms which can occur. The most intense seen is the elastic scattering or Rayleigh scattering that results in no energy change, the incident and emitted photon has the same energy. The inelastic scattering, Stokes and Anti-Stokes scattering, which occurs is where the Raman Effect is observed. In Stokes scattering a molecule is excited to a virtual state and the final vibrational state of the molecule is more energetic than its 48 initial state, this causes the scattered photon to be shifted to a lower frequency in order for the total energy of the system to remain balanced. However, if the final vibrational state is lower in energy than the initial state, then in order to balance the total energy the scattered photon will be shifted to a higher frequency, and this is known as Anti-Stokes scattering. Figure 2.1 shows the differing scatterings that can be observed. Surface-enhanced Raman spectroscopy (SERS) was first noticed in 1974 by Fleischmann with the molecule pyridine adsorbed onto a roughened silver electrode [3]. Fleischmann noticed that the electrochemically roughened coinage metal surface produced a Raman signal six orders of magnitude larger than was expected from the normal Raman cross-section. After this discovery many researchs tried to discover the mechanisms behind the 106 fold enhancement. The enhancement factor is considered to be the product of an electromagnetic (EM) enhancement mechanism and a poorly understood chemical enhancement mechanism. The mechanisms arise because the intensity of Raman scattering is proportional to the induced dipole moment, μind, which is itself a product of polarizability, α, and the incident electromagnetic field, E [4]. μind = α * E (1) The electromagnetic enhancement mechanism is often stated to correspond to 104 factor enhancement while the chemical enhancement theory accounts for the leftover 102 enhancement. The chemical enhancement effect is considered to arise from the electronic intracluster excitation via a type of Förster excitation transfer [5] or metal/adsorbate charge transfer resonance [6]. 49 The enhancement factor, based on the electromagnetic enhancement mechanism, E at each molecule is (approximately) given by E = |E(ω)|2|E(ω’)|2, (2) where E(ω) is the local electric-field enhancement factor at the incident frequency ω and E(ω’) is the corresponding factor at the Stokes-shifted frequency ω’ [7]. E is often approximated such that E(ω) and E(ω’) are considered equal, and hence E = |E(ω)|4. When an EM wave interacts with a roughened metal surface, or small nanoparticles, the wave may excite localized surface plasmons on the metal, which amplifies the EM fields near the surface. A localized surface plasmon, LSPR, is produced when the collective oscillation of valence electrons in a metal nanoparticle is in resonance with the frequency of incident light. For a spherical particle, (this shape is assumed for this thesis based on observed TEM and the size/shape of the zeolite supercages), with a radius a, and irradiated by z polarized light of λ wavelength, we can assume the electric field around the nanoparticle is uniform. This allows Maxwell’s equations to be replaced by the Laplace equation of electrostatics [7] and allows one to determine the EM field outside the particle, Eout, is given by , (3) where x, y, and z are the Cartesian coordinates, r is the radial distance, are the Cartesian unit vectors, and α is the polarizability which can be further broken down into the following 50 α = ga3, (4) g is a function of the dielectric constant of the nanoparticle, εin, and the dielectric constant of the medium , εout, expressed as, g = (εin-εout)/(εin+2εout). (5) Equation 3 illustrates the distance dependence of the EM enhancement factor. The field enhancement decays with r-3, indicating that adsorbates will have a stronger enhancement than molecules that are farther removed from the surface [8]. The EM field enhancement is taken to the fourth power, the distance dependence scales with this, increasing r-3 to r-12. One can imagine however that due to the distance enabling enhancement that shells of molecules can surround the nanoparticle increasing the surface area by a factor of r2. Taking this into account to one can calculate the SERS Raman intensity, ISERS, at a distance as follows: ISERS = [(a+r)/a]-10 (6) where a is the particle size and r is the distance between the analyte and the substrate. As the dielectric functions are wavelength dependent, the magnitude of the enhancement is also wavelength dependent. The maximum enhancement is seen in Equation 5, where εin=-2εout. This condition is met in the visible region of the electromagnetic spectrum for coinage metals such as gold and silver [9]. An enhancement factor, EF, can be determined experimentally by using the following equation: 51 EF = [(ISERS/INRS)*(NSURF/NSOL)] (7) ISERS is the intensity of the SERS active Raman scattering, INRS is the normal Raman intensity for a solution of the same concentration as used in the SERS experiment without the SERS active substrate, NSURF is the number of molecules bonded to the SERS active substrate, and NSOL is the number of molecules in the focal volume. Note that this equation does not take into account any analytes not directly bonded to the SERS active substrate but still within range of the enhancing fields. 2.1.2 Previous Studies on SERS Substrates An ideal SERS substrate will provide a substantial enhancement factor, be in uniform in composition, reproducible, and stable. Previously studied SERSactive substrates have included; Ag and Au aggregated colloids [10-15], metal electrodes [16-19], metals generated by reduction of silver-exchanged zeolites [20-21]. Coinage metal nanoparticles have shown that it is possible to detect single molecules of rhodamine 6G with Raman [22], unfortunately reproducibility of particle size and long-term stability of the colloidal solution plagues this method [23-25]. Metal electrodes are yet another commonly studied SERS substrates, in fact they were the initial SER substrates. These electrodes typically undergo a roughening process via electrochemistry or chemical etching to produce more prolate structures suitable for SERS work [26]. The metal electrodes do not have issues with particles falling out of solution due to aggregation, thus are much more stable than colloidal solutions. The roughened 52 surfaces on the electrodes do not provide as great an enhancement factor as seen in the colloidal solution. The work done in this thesis utilizes the unique properties of the zeolite to facilitate the formation of a SERS substrate. Zeolites are photochemically and thermally stable. Many types of zeolites, including zeolite Y, contain exchangeable cations present in the framework that are needed to balance out the negative charge of the framework itself. Zeolites have been used before as a host for the formation of metal and semiconductor clusters [27]. A number of metallic and organometallic compounds have been formed in zeolites, of which silver is one. Ag is the only noble metal whose ion can be completely exchanged into a zeolite from an aqueous solution because it is the only noble monopositive charged cation that forms a stable mononuclear species in water [28-30]. At lower Ag+ ion exchange levels, all the Ag+ in hydrated zeolites are easily reduced to form clusters, the water has been suggested to facilitate the diffusion of silver [31]. There is also the added benefit that the redox of Ag zeolite is reversible, and that the oxygen treatment of dehydrated Ag-Y causes a migration of Ag+ ions into the sodalite units from the supercages [32]. There have only been two studies published using zeolites as a SERS platform. The first study was performed by Dutta and Robins, where Robins produced a silver-coated zeolite Y substrate. Ion-exchanged Ag zeolite Y was reduced with hydrazine, and Robins observed that the silver had migrated to the surface of the zeolite forming a silver-coating around the surface [20]. Yan investigated silver-coated zeolite A and zeolite NaX crystals deposited by 53 vacuum deposition as surface-enhanced Raman scattering (SERS) substrates. Yan found that the substrates were active for the enhancement of Raman signal. scattering from uranyl ions with a detection limit of 10-5 M for uranyl was obtained using silver-coated zeolite A [21]. 54 Energy Virtual Energy Level Rayleigh Scattering Stokes Shift First Excited State Ground State Figure 2.1: Raman Scattering 55 Anti-Stokes Shift 2.2 Experimental 2.2.1 Silver Loading and Reduction A 500 mg sample of Na+ Zeolite Y was calcined at 550°C for 24 hours under a flow of oxygen to remove any trace organics. The calcined zeolite was then treated with humidified air during the cool down cycle once the temperature reached 80°C, to prevent the reintroduction of organics inside the zeolite framework. Then 100 mg of the hydrated calcined zeolite was removed and placed into a 20 mL screw top vial, the remaining zeolite was placed into a dessicator in another screw top vial for storage. The 100 mg sample was added to 5 mL of a 0.1 M AgNO3 solution and stirred overnight for Ag+ exchange with the Na+ in the zeolite framework. The solution was then washed repeatedly to remove any unreacted AgNO3 remaining in solution, and the resulting supernatant was treated with NaCl in the dark for detection of Ag+ ions. The Ag+ Zeolite Y was placed into 5 mL of nanopure water and 1 mL of hydrazine at different concentrations. The first method involved adding 1 mL of 99.7% hydrated hydrazine to the zeolite suspension; this resulted in the previously white suspension turning to a dark gray almost black color. This color shift indicates that the silver aggregated into large clusters during reduction. The next method involved adding several lower concentrations of hydrazine to the zeolite suspension. The third method utilized was a controlled addition of the concentrations from method 2. In the controlled addition method, while the zeolite suspension was being stirred 10 μL aliquots of the hydrazine solution 56 were added to the zeolite suspension every 6 minutes for an hour, for a total of 100 μL of the hydrazine solution. During one of the Raman sequential scans, the peaks changed noticeably as the scans progressed for the first few scans and then stabilized. This seemed to indicate that the silver clusters may be undergoing further reduction from the laser light. Following this observation several Raman scans were performed on the hydrazine reduced Ag zeolites following sample illumination by the laser at varying power levels. These studies only provided illumination onto a tiny part of the sample, and in order to maximize the sample exposure to light the hydrazine treated Ag zeolite was suspended in 1 mL of nanopure water and illuminated in a photolysis chamber while being stirred with a microstir bar. Bulk photolysis experiments were also performed where 100 g of hydrazine treated Ag zeolite was suspended in 50 mL of water with a stir bar and stirred while exposed to light from the photolysis set-up. 2.2.2 X-ray diffraction (XRD) In order to determine whether the zeolite supercage structure was left intact from Ag+ reduction, X-ray diffraction (XRD) studies were performed first on a Na Y zeolite sample and on reduced Ag Y zeolite. XRD studies were carried out on a Rigaku Geigerflex diffractometer with a nickel filtered CuKa source with a wavelength of 1.5405 Å. The Cu source irradiated X-rays at 40 kV and 25 mA. Diffraction measurements were taken at a scan rate of 0.02 degree/step, with a dwell time of 0.5 s/step, and a scan range of 3-50 degrees. The x-rays were 57 collected by a scintillation counter, with a divergence slit of 0.6 degrees, and scattering and receiving slits of 0.5 degrees. 2.2.3 Raman Studies All Raman spectra were collected on a Renishaw - Smiths combined Raman - IR Microprobe utilizing either a 514.5 nm laser line of an Ar ion laser or a 632.8 nm laser line of a He – Ne laser. The laser was edge-focused for all spectra, and both dynamic and static scans were performed. 2.2.4 Transmission Electron Microscopy (TEM) Reduced silver zeolite samples were imaged by a transmission electron microscope (TEM) to characterize zeolite and silver particle size, and silver particle dispersion and uniformity. Silver zeolite samples were taken from the same batches as used for Raman and XRD experiments. All images were obtained using a Tecnai F20 TEM. All samples were dispersed into distilled water to create a 10 % w/w solution, a 2 μL aliquot was then placed on a 300 nm copper TEM grid and allowed to evaporate. 2.3 Results and Discussion 2.3.1 Formation of Highly Reduced Silver Zeolite Nano-scale zeolite Y was synthesized with a modification of the Holmberg method [1]. The Holmberg method mixes a solution of aluminum isopropoxide (Al(OC3H7)3), H2O, and tetramethylammonium hydroxide (TMAOH) with a Ludox SiO2 solution. The aluminum source and silica solutions are then stirred for one hour until the solution turns clear at which point tetramethylammonium bromide (TMABr), as a templating agent, is added to the solution. The solution is then 58 stirred again for one hour and then transferred to a bomb and placed in a 100 °C oven for 72 hours. Instead of adding base directly to the aluminum source, as is called for by the Holmberg method, it was split (80/20) between the aluminum source and the silica source. This was done to help dissolve the silica source before mixing. Also, the Al(OC3H7)3 is slightly insoluble so it was heated in a water bath between 60-70 °C until the solution was clear before adding the TMABr. Only after these two steps was the aluminum and silica source mixed. XRD was performed on the newly made samples, prior to silver-ion exchange, in order to determine if proper crystalline structure was observed. Figure 2.2 clearly shows that the newly synthesized sample matches up with the previous nanoscale zeolite Y synthesis, and consistent with reported patterns. Smaller scale crystallites show broader peaks in their patterns relative to larger scale crystallites. In order to determine the size, uniformity, and position of the silver particles inside the zeolite, TEM was performed. As can be seen in the two TEM images in Figure 2.3 the silver particles greatly vary in size. Most particles are clearly over 10 nm in diameter making them much too large to be located in the interior of the zeolite and therefore must be located on the surface. Once the synthesis method was verified with XRD, a silver-ion exchange was performed on the nano-scale zeolite. A 100 mg sample of the nano-scale zeolite was placed into 5 mL solution of 0.1 M AgNO3 and stirred overnight. The ion-exchanged nano-scale zeolite then underwent washing several times until no excess Ag was observed. The freshly washed sample was then treated with 1 mL of 19.26 M hydrated hydrazine, the sample immediately shifted from a milky 59 white suspension to a dark grey/black suspension. In order to determine if the crystallinity of the zeolite Y was still intact the sample was once again subjected to XRD analysis. Figure 2.4 shows that the sample still matches up with zeolite Y, indicating that the supercage structure is mostly still intact however there is a noticeable decrease in peak intensity showing some degradation of the zeolite has taken place. The 2 new peaks at 38.1 2Θ and 44.3 2Θ are due to silver. 60 Figure 2.2: Comparison of Synthesized Nano-Scale Zeolite Y (Upper) to that of the Previously Characterized Nano-Scale Zeolite Y Standard (Lower) 61 Figure 2.3: TEM of Excess Hydrazine Treated Ag+ Zeolite Y 62 38.177 44.301 Figure 2.4: XRD Pattern of Nano-Scale Zeolite Y Ion-Exchanged with 0.1M AgNO3 and Reduced with Hydrazine. Pattern Matches for Silver (Upper) and Zeolite Y (Lower) are Included for Comparison 63 2.3.2 Raman Studies on Highly Reduced Silver Zeolite with Pyridine as Analyte Pyridine is an extensively studied SERS substance, and seemed well suited to determine if the silver zeolite Y produced in this thesis was a good candidate for SERS activity. Figures 2.5 and 2.6 show the normal Raman response for neat liquid pyridine, aqueous pyridine, and SERS response for pyridine on silver, as determined by Pagliai et. al.. The peak assignments and relative intensities determined by Muniz-Miranda are shown in Table 2.1. These reported bands shifts are used as comparisons to determine if the Raman spectra observed in this thesis are illustrating a SERS response. The main bands of interest are the very strong peaks associated with the ring-breathing modes in the non-SERS Raman position of 1000 cm-1 and 1032 cm-1 which blue shift in the SERS response to 1008 cm-1 and 1036 cm-1 (as seen by comparison of Figure 2.5 and 2.6). These shifts are used to verify a surface-enhancement effect. A 1 mL sample of a 0.1 M pyridine solution was placed in a capillary tube with the ends capped. The pyridine sample was then placed in the Renishaw Raman instrument and scanned using a 633 nm He-Ne laser at 3.2 mW. The resulting spectrum can be seen in Figure 2.7, which matches the expected spectrum seen in Figure 2.4c. Another 1 mL sample from the same 0.1 M pyridine solution was added to 10 mg of nano silver zeolite Y and placed in a capillary tube and then into the Raman instrument. The 3.2 mW power scan and the 0.4 mW power scans can be seen in Figures 2.8 and 2.9, respectively. The 64 3.2 mW power spectrum exhibited a great degree of fluorescence masking any possible peaks in the spectrum. Dropping the power to 0.4 mW helped to alleviate the fluorescence masking the peaks, but only resulting in very weak peaks. The peaks observed matched more closely to the expected peak positions associated with the SERS effect at 1008 cm-1 and 1036 cm-1 The synthesis process for the nano-scale zeolite Y has templated organics which lead to the fluorescence problems. However the micron-scale zeolites have no organics involved in their synthesis, for this reason it was decided to switch from the nano-scale to the micron-scale synthesis. The micron-scale synthesis was developed by the Dutta group, it requires that two solutions be combined slowly and then stirred for 4 hours. Solution A consists of 85 mL of DI water, added to 7.2955 g or 0.1838 moles of NaOH, combined with Solution B which consists of 13.8574 g of Ludox SM-30 for the silica source added to 2.208 g or 0.01081 moles of Al(OH)3. Once the solution has stirred for 4 hours it is then placed in an autoclave at 90 °C for 24 hours, it is then removed from the autoclave and allowed to cool and then undergoes a washing process to remove any unreacted reagents. A 10 mg sample of micron-scale zeolite Y was added to 1 mL of a 0.1 M pyridine solution and placed into a capillary tube and then scanned with the Raman instrument. The resulting spectrum can be seen in Figure 2.10, the 1002 cm-1 and 1034 cm-1 peaks from this spectrum more closely match up with the aqueous pyridine Raman spectrum of 1000 cm-1 and 1032 cm1 than the SERS peak positions of 1008 cm-1 and 1036 cm-1. Without silver particles, the zeolite Y itself is incapable of facilitating a SERS response. 65 Raman Shift cm-1 Figure 2.5: Liquid Pyridine (b), Aqueous Pyridine (c) Raman Spectra [33] 66 Intensity Raman Shift cm-1 Figure 2.6: SERS Spectra of Pyridine on Silver [33] 67 Table 2.1: Pyridine Peak Assignments [34] 68 Intensity Raman Shift cm-1 Figure 2.7: Raman Spectra of 0.1M Pyridine Solution at 3.2 mW Power with a 633 nm Excitation Line 69 1800000 1600000 1400000 Intensity 1200000 1000000 800000 600000 400000 200000 0 0 200 400 600 800 1000 1200 1400 1600 -1 Wavenumber Raman Shift cm Figure 2.8: 3.2 mW Power Scan with a 633 nm Excitation Line of a 0.1 M Pyridine Solution on Nanoscale Ag Zeolite Y 70 1800 Intensity Raman Shift cm-1 Figure 2.9: Nanoscale Ag Zeolite with 0.1 M Pyridine 0.4 mW Power 633 nm Excitation Line 71 Intensity Raman Shift cm-1 Figure 2.10: Micronscale Ag Zeolite with 0.1 M Pyridine 3.2 mW Power with a 633 nm Excitation Line 72 The capillary setup was fraught with instability issues leading to loss of laser focus. Though the Raman instrument was situated on a stabilizing bench, because the capillary was situated unsecured on a glass slide, any vibrations experienced would result in a physical shift of the capillary. In order to alleviate these stability issues, a small vessel was made that had a base with a screw-top cap with a glass window. The base had a well bored into that had a 2 cm diameter and was 2 cm deep. It was then decided to switch from a suspension to having a BaSO4 pellet composed of 10% w/w silver zeolite Y. The barium sulfate was to act as a Raman reference, to ensure that laser was optimally focused. Figure 2.11 shows a Raman spectrum of the BaSO4 used for the pellet formation. Figure 2.12 shows the Raman spectrum of a BaSO4/Ag zeolite Y pellet with a 1 mL drop of 0.1 M pyridine placed on top, the spectrum shows both the SERS pyridine peaks and the BaSO4 peaks. Figure 2.13 is the result of 30 accumulated Raman scans of a 90/10% w/w BaSO4/Ag zeolite Y pellet with a 1 mL drop of 0.1 M pyridine (laser focused on the zeolite), this resultant spectrum is missing the peak of 987 cm-1 from BaSO4 but shows the 1008 and 1035 cm-1 peaks corresponding to the pyridine SERS response. A closer inspection of the area between the two 1000 cm-1 peaks shows a third peak at 1029 cm-1. Our explanation for the 1029 cm-1 peak is that it is coming from pyridine converting to pyridinium by reacting with H+ contained in the zeolite. This assignment is supported by literature as seen in Figure 2.14, pyridine predominately makes up the solution at a basic pH of 8.3 and as the solution becomes more acidic pyridine starts reacting to form 73 pyridinium, both pyridine peaks (1035 cm-1 and 1002 cm-1) and prydinium peaks (1029 cm-1 and 1011 cm-1) can be seen at pH 5.3 and once the solution reaches an acidic pH of 2.8 pyridine peaks disappear showing only pyridinium peaks. The first step in lowering the fluorescence background was to calcine the zeolite to remove any organics, while the micron scale synthesis does not itself introduce any trace organics some may have been absorbed into the zeolite while it was dried. Figure 2.15 shows a slight reduction in the heightened baseline from the calcination process. Pyridine was evaporated from a sample and then subjected to Raman spectroscopy in order to determine whether pyridine was reacting with the silver or is just physisorbed onto the zeolite, Figure 2.16 shows though that no peaks indicative of pyridine were present, which indicates that pyridine is only physisorbed onto the silver zeolite. 74 2500000 Intensity Intensity 2000000 1500000 1000000 500000 0 150 315 480 645 810 975 Raman Shift cm Wavenumber 1140 1305 1470 1635 -1 Figure 2.11: BaSO4 Raman Spectrum at 3.2 mW Laser Power with a 633 nm Excitation Line 75 Intensity Raman Shift cm-1 Figure 2.12: BaSO4 Pellet with Ag Zeolite Y with 0.1 M Pyridine Cycling Focus Scan at 3.2 mW Laser Power with a 633 nm Excitation Line 76 Intensity Raman Shift cm-1 Figure 2.13: BaSO4 pellet with Micron Ag Zeolite Y with 0.1 M pyridine at 3.2 mW Laser Power with a 633 nm Excitation Line 77 Figure 2.14: pH dependence of Pyridine/Pyridinium Conversion [35] 78 Intensity Raman Shift cm-1 Figure 2.15: Calcined Ag Zeolite Y Pellet with 0.1 M Pyridine at 3.2 mW Laser Power with a 633 nm Excitation Line 79 Figure 2.16: Calcined Ag Zeolite Y Pellet with 0.1 M Pyridine Evaporated at 3.2 mW Laser Power with a 633 nm Excitation Line 80 2.3.3 Raman Studies with Partially Reduced Silver Zeolites with Pyridine as Analyte The previous studies involving an “overkill” dose of 19.26 M hydrazine resulted in silver particles that were not only too large and of varying size, but also located outside of the zeolite supercage structure. It was decided to then shift from a one dose treatment in hopes of reducing as much silver as possible to a controlled addition of hydrazine in the hopes that the silver would be smaller sized and placed within the zeolite. Varying concentrations of hydrazine were made, in each case 100 mg of silver ion-exchanged zeolite Y was placed in 10 mL of DI water. The zeolite suspension was then stirred in the dark while 10 µL of a hydrazine solution, concentrations given in Figure 2.17, was added every 6 minutes over an hour for a total of 10 additions. The solution was then washed to remove any excess hydrazine and the zeolite was allowed to dry before it was pressed into a pellet, BaSO4 was no longer used in the pellet formation as it proved difficult to press reliably. The pellet was then placed on a Teflon spacer inside the sample holder and a 2 µL drop of 0.1 M pyridine was added to the each sample and studied with Raman spectroscopy. Figure 2.17 shows that the 6.42*10-3 M or 6.42 mM solution resulted in the best spectrum, with greatest intensities at the 1012 cm-1 and 1039 cm-1 bands. While watching as spectra were accumulated during a 30 scan sequence it was noticed that peak positions and intensities were shifting as time elapsed. One hypothesis is that this peak shifting is due to further reduction of the silver due to the laser light. In order to study if this was in fact true, the hydrazine 81 treated zeolite was illuminated for 10 minutes prior to a run with 3.2 mW laser power at a focused point. Spectra were then collected at the laser focus point and at a position removed from the laser focus point. Figure 2.18 shows the resultant spectrum from an area outside of the laser focal site, the pyridine peaks do correspond to those associated with the SERS effect however enhancement appears to be low because the much weaker zeolite peak at 512 cm-1 is in greater intensity than the two characteristic pyridine peaks of 1010 cm-1 and 1040 cm-1. The on laser site can be seen in Figure 2.19; the pyridine peaks clearly match with the expected SERS response peaks, and are of a greater intensity than either of the characteristic peaks of either Teflon at 733 cm-1 or zeolite Y at 505 cm-1. A cross check sample was performed on micron-scale zeolite Y pellet without any silver present; the sample was illuminated for 10 min at 3.2 mW laser power with a 633 nm laser just like the previous experiment. The results can be seen in Figure 2.20, which shows no characteristic SERS peaks, only those expected from a normal Raman response of an aqueous pyridine sample along with a small peak at 505 cm-1 from the zeolite Y. 82 Figure 2.17: Controlled Addition of Hydrazine with 0.1 M Pyridine at 3.2 mW Laser Power with a 633 nm Excitation Line 83 Raman Shift cm-1 Figure 2.18: 0.1 M Pyridine on Ag Zeolite Y after Laser Illumination 3.2 mW Power off Spot with a 633 nm Excitation Line 84 Raman Shift cm-1 Figure 2.19: Single Drop 0.1 M Pyridine on Ag Zeolite Pellet at 3.2 mW Laser Power with a 633 nm Excitation Line 85 Raman Shift cm-1 Figure 2.20: Single Drop 0.1 M Pyridine on Na Zeolite Pellet at 3.2 mW Laser Power with a 633 nm Excitation Line 86 2.3.4 Raman Studies with Partially Reduced Silver Zeolites with Benzenethiol as Analyte Other SERS molecules include benzenethiol. Benzenethiol has a Raman cross-section even larger than pyridine [36], has a similar structure, and has been extensively studied. Figure 2.21 shows the normal Raman spectrum for neat liquid benzenethiol and the SERS response for benzenethiol on silver, as determined by Aggarwal et al., these responses are used to determine if the Raman spectra observed in this thesis are eliciting a SERS response, specifically the red shifts of the 1002 cm-1, 1026 cm-1, and 1093 cm-1 bands to 999 cm-1, 1022 cm-1, and 1073 cm-1, respectively. The peak assignments and relative intensities determined by Tai Ha Joo can be seen in Table 2.2. A new sampling technique was devised; the Teflon spacers that had been used were modified to contain 5 sample wells in an X formation. All wells were cut to be 2 mm wide x 2 mm long x 1/2 mm deep, seen in Figure 2.22. Each well would contain a separate sample to allow for faster analysis. Because the wells were so much smaller than the previous setup, a scan of the Teflon surface was needed to ensure if any of the peaks in the Raman were arising from the Teflon. By focusing on the Teflon well, the spectrum obtained can be seen in Figure 2.23. 2.3.5 SERS Sample Preparation by Initial Hydrazine Reduction Followed by Laser Reduction The silver zeolite Y was pressed into the well after an initial hydrazine reduction, and then illuminated for 10 minutes at 3.2 mW laser power, after which 87 a 2 μL aliquot of a benzenethiol solution was placed on the surface and the Raman spectrum obtained. Four sites were chosen on the sample and compared to determine homogeneity. As seen in Figure 2.24 all four sites show similar results and the shifting of the 999 cm-1, 1026 cm-1 and 1093 cm-1 peaks to 999 cm-1, 1026 cm-1, and 1073 cm-1 confirms that a SERS effect is taking place. In order to determine the limit of detection the benzenethiol was then diluted by a factor of 100 to 1 mM, and the resulting spectrum was compared to a 0.1 M sample. The results seen in Figure 2.25 show comparable intensity, this led to the thought that even lower concentrations should be readily detectable. However when a solution of 1*10-5 M benzenethiol was added to the silver zeolite, none of the characteristic peaks of SERS or normal response was seen. 2.3.6 SERS Sample Preparation by Simultaneous Hydrazine and Laser Reduction The next set of experiments involved simultaneous reduction via dilute hydrazine and laser light. Two samples were prepared in which silver-ion exchanged zeolite Y was pressed into two separate wells, one well had a 2 μL aliquot of 1.90*10-3 M benzenethiol added to it and the other had a 2 μL aliquot of 9.51*10-3 M benzenethiol added, and then both samples were illuminated for 10 minutes with 3.2 mW laser power before being scanned. The resulting spectrum can be seen in Figures 2.26 and 2.27, respectively. Both spectrum show peaks characteristic of a SERS response, however the sample reduced with 9.51*103 M benzenethiol also appears to exhibit peaks characteristic of a normal Raman response at 1093 cm-1 and large unknown peaks at 883 cm-1 and 1048 cm-1. 88 The benzenethiol was dissolved in an ethanol solution, and neither peak corresponds to an ethanol spectrum. A second trial using the same conditions was carried out, the scan was set between the 800 and 1300 cm-1 region to monitor the three suspect bands and the three SERS response bands. The new trial matched up with the previous experiment and can be seen in Figure 2.28. After searching the literature it was thought that the new peaks may be due to an interaction with a Ag7 cluster as seen in Figure 2.29. A fresh sample was prepared following the same sample preparation method utilized in Figures 2.27 and 2.28, but with no benzenethiol present in the ethanol solvent, the peaks shown in Figure 2.30 clearly match with the three suspected peaks seen in 2.27 and 2.28. This removes any notion that the three suspect peaks were likely due to benzenethiol bound to a Ag7 cluster, and are purely caused by a denaturing agent in the ethanol solvent. Switching to absolute ethanol should alleviate this problem. 2.3.7 SERS sample preparation by initial hydrazine reduction followed by photolysis of solid surface The simultaneous reduction of the silver-ion exchanged zeolite resulted in only a small portion being properly reduced because of the small size of the laser focus, leaving most of the sample containing only partially reduced silver particles. In order to create a more uniform reduction, unreduced samples were pressed into the Teflon wells, had a 2 μL aliquot of varying hydrazine concentrations added, and placed into a photolysis setup where UV light was focused on the samples and illuminated for 30 minutes. The samples were then 89 exposed to 1mM benzenethiol and spectra were collected. The 1.90*10^-3 M solution of hydrazine showed the sharpest peaks and the least amount of noise as can be seen in Figure 2.31. When the samples were removed it was noticed that only the surface layer exposed to the UV light was properly reduced, the rest of the sample remained white. 2.3.8 SERS Sample Preparation by Initial Hydrazine Reduction Followed by Photolysis of the Entire Sample Further modification of the reduction method involved the following. The 20 mg of the unreduced zeolite was placed into 1 mL of water, a 10 μL aliquot of varying hydrazine concentrations added, and placed into a photolysis setup where UV light was focused on the samples and illuminated for 30 minutes while being stirred via a magnetic stirbar. The samples were then exposed to 1mM benzenethiol and Raman spectra were collected. The 0.193 mM solution of hydrazine was the only reduced sample that showed characteristic SERS peaks for benzenethiol, which can be seen in Figure 2.32. The samples reduced via photolysis of the suspension were subjected to TEM imaging. The TEM images can be seen in Figure 2.33; the silver particles now are far more uniform in size than in the previous TEM of the reduction via excess hydrazine. The size of the particles based on the TEM scale seems to be approximately 1 nm, which indicates that the silver particles are small enough to be contained within the zeolite itself and not only present on the surface. The Scherrer Equation seen in equation 7 can be used to calculate the silver particle size, τ, as long as the particles are below 100 nm. Where Κ is the 90 shape factor, equal to 0.9 typically, λ is the X-ray wavelength, β is the FWHM or breadth in radians, and Θ is the Bragg angle. A powder diffraction standard with known particle size is used as a reference to calculate the silver particle size. Because the standard has minimal strain, any broadening of the peaks is considered to be contributed solely by the instrument itself. The reduced silver zeolite was mixed with NIST 640 C powder diffraction standard in a 50/50 ratio with a calibrated particle size of 4.9 μm and characterized with XRD. The resulting XRD pattern can be seen in Figure 2.34. The standard has two peaks that fall within the scanned range, one at 28.4409 2Θ and one at 47.3003 2Θ. Due to the intensity of the peaks observed from the standard all silver peaks were lost in the pattern. XRD was repeated on the same Ag Zeolite source without the NIST 640 C standard to measure the β of the silver peaks and can be seen in Figure 2.35 The peak at 47.3003 2Θ being the closest to a silver peak, at 44.301 2Θ, was used to determine the breadth, β. The breadth, β, refers to the broadening due to the particle-size effect alone, equation 8 is used to determine β from the measured breadth of the sample in question βm and βs the measured breadth of the standard. The Jade program was used to deconvolute the peaks where silver and zeolite Y pattern peaks overlap. The silver particle size was calculated to be 40.7 nm after adjusting for the inherent broadening from the instrument. The difference calculated by the Scherrer Equation than that seen in the TEM images is attributed to the heterogeneity of the particles, as some large (greater than 50 nm) silver particles were observed. (7) 91 β2 = β2m-β2s (8) 92 Figure 2.21: Raman (top) and SERS spectra (bottom) of benzenethiol [36] 93 Table 2.2: SER Spectral Data (cm-1) and Vibrational Assignments of Benzenethiol Adsorbed on Silver Powder [37] 94 Figure 2.22: Raman Sample Holder 2 mm Wide x 2 mm Long x 1/2 mm Deep 95 10000 733 9000 8000 7000 Counts 6000 5000 4000 1381 3000 2000 1297 1210 1000 0 400 600 800 1000 1200 1400 1600 Raman Shifts Figure 2.23: Raman Spectra of Teflon Wafer at 3.2 mW Laser Power with a 633 nm Excitation Line 96 1800 999 1073 1022 Raman Shift cm-1 Figure 2.24: 0.1 M Benzenethiol on Ag Zeolite Pressed in Wells at 3.2 mW Laser Power with a 633 nm Excitation Line (Multiple Focal Sites) 97 Raman Shift cm-1 Figure 2.25: Signal Intensity of Benzenethiol Concentration 0.1 M Benzenethiol Red and 0.001 M Benzenethiol Black (Spectra Collected at 3.2 mW Laser Power with a 633 nm Excitation Line) 98 Raman Shift cm-1 Figure 2.26: 0.001 M Benzenthiol on Ag Zeolite Reduced with 1.90*10-3 M Hydrazine at 3.2 mW Laser Power with a 633 nm Excitation Line 99 Raman Shift cm-1 Figure 2.27: 0.001 M Benzenthiol on Ag Zeolite with 9.51*10-3 M Hydrazine Reduction at 3.2 mW Laser Power with a 633 nm Excitation Line 100 Raman Shift cm-1 Figure 2.28: 0.001 M Benzenethiol on Ag Zeolite Pressed in Wells at 3.2 mW Laser Power with a 633 nm Excitation Line 101 Figure 2.29: Spectral Shifts for Benzenethiol Binding to Different Cluster Sizes [38] 102 70000 60000 50000 Intensity 40000 30000 882.605 20000 10000 1047.86 1092.36 0 800 850 900 950 1000 1050 Raman Shifts (cm-1) 1100 1150 1200 Figure 2.30: Ethanol Raman Spectra at 3.2 mW Laser Power with a 633 nm Excitation Line 103 1.93 mM Hydrazine Controlled Dilution 9.63 mM Hydrazine Controlled Dilution 3.85 mM Hydrazine Controlled Dilution 2.57 mM Hydrazine Controlled Dilution 0.193 mM Hydrazine Controlled Dilution Raman Shift cm-1 Figure 2.31: Effect of Hydrazine Concentration with Surface Photolysis Setup (Collected at 3.2 mW Laser Power with a 633 nm Excitation Line) 104 0.193 mM Hydrazine 1.93 mM Hydrazine 3.85 mM Hydrazine Raman Shift cm-1 Figure 2.32: Effect of Hydrazine Concentration with Suspension Photolysis Setup (Collected at 3.2 mW Laser Power with a 633 nm Excitation Line) 105 Figure 2.33: 2.57 mM Hydrazine Reduction TEM (Top Left is at 50 nm Resolution, Top Right is at 20 nm Resolution, and Bottom is at 100 nm Resolution) 106 7000 28.440 6000 5000 Counts 4000 3000 47.30 2000 1000 0 0 -1000 5 10 15 20 25 30 35 40 45 50 2-Theta Figure 2.34: XRD of Photolyzed Zeolite Y Suspension with 640 C NIST Standard 107 2500 2000 Counts 1500 1000 500 44.30 0 0 5 10 15 20 -500 25 30 35 2 Theta Figure 2.35: XRD of 2.57 mM Hydrazine Reduced Ag Zeolite Y 108 40 45 50 2.4 Conclusion SERS response can be verified by observing the red shift of the 1093 cm-1 peak to 1073 cm-1 peak in the benzenethiol, as well as the blue shifting of the 1000 cm-1 and 1032 cm-1 to 1008 cm-1 and 1036 cm-1 in pyridine. 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