chemical physics of discharges - Argonne National Laboratory

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214 states of molecular oqgen are also present. It is instructive to compare these results with measurements of the activation energy of graphite with atomic oxygen removed from the luminous discharge. In severearly studies a vdue of zero was reported (2) (16). Hennig (8) observed no dependence on temperature at a pressure of 1.0 torr and a value of 7 Kcal/mol at 10 torr. This difference was attributed to ozone formation. In a recent detailed study of the atomic oxygen-graphite reaction, Marsh et al. (U) reported an activation energy of 10 Kcal/mol between U and 2OO0C, which approached zero at 350°C. 'Although the rate of oxidation in these studies was considerably lower than that obtained in the plasm, their values are consistent with the belief that atomic oqygen is a major reactant within the discharge. Of a variety of specimens, only graphite exhibited an abrupt change in activation energy near 3Oo0C. For example, the apparent activation energy in the decomposition of sucrose is approximately 4 Xcal/mol over the entire measurement range. The independence of oxidation rate for graphite at high temperatures is ascribed to the formation of surface oxides. Numerous studies of graphite combustion have shown that such surface compounds control rate at elevated temperatures in excess oxygen. As anticipated, increasing radiofreqiiency power to the discharge does not measurablv increase the rate of graphite oxidation at high sample temperature. The exhaust gas of the ovgen-graphite reaction contains both carbon monoxide a d carbon dioxide, with the latter predominating. Tn the lumi~ous discharge region these gases react with graphite. The results of measuremepts in which carbon dioxide was passed through the radiofrequency field and then exposed to graphite rods activated are shown in figure 3. Between 150 and 4OOOC the Arhennius equation fits well, yielding an apparent activation energy of 3.2 Kcal,/mol. Below 120°C less than one mg per hour of carbon was removed. This small weight loss is attributed to ion and electron bombardment. W& Conditions: In a number of experiments, increasing power beyond an optimum value led to the anomolous result of reducing ashing rate. Earlier it was noted that placing a dry ice-acetone trap in the exhaust stream extended the length of the luminous discharge (5). To study this effect, wall temperatures were varied while the carbon rod was maintained at 200°C. The results of a series of measurements are shown in figure 4. Assuming that the decrease in oxidation rate at increased wall temperature ip due to recombination of active species at the wall, the overall activation energy at low temperatures for this process is approximately 2 Kcal/ml. The major sources leading to loss of active oxygen species are recombination of atomic oxygen and ions at the'walls of the vessel. The recombination of discharged oxygen on glass surfaces has been investigated. Linnett and Marsden (10) reported that the recombination coefficient of atomic oxygen on clean borosilicate glass (Pyrex) was independent of temperature. However, positive values were observed on contaminated surfaces. In a later series of papers Greaves and Linnett (7) studied a number of oxide surfaces, in all cases the recombination coefficient was temperature ' dependent. For silica apparent activation energies were 1 to 13 Kcal/mol over the temperature range 15 to 3OOOC. The exceptional nature of Pyrex was noted. ' The second major source of loss of active species results from electron-ion recombination at the chamber walls. The electric field restricts the drift of ions to the chamber walls. Rate of-recombination is controlled by ambipolar diffusion, but is limited by the presence of negatively charged oqgen ions in the discharge (15). Although diffusion is not dependent on wall temperature, a distortion of the symmetric electrical field will enhance wall recombination, producing an inarease in This effect is noted in t&le 1. The presence of a 6-cm long metallic ring on the exterior wall of the reduced oddation rate by more than ten per cent. Grounding the ring in comn with . wall temperature and a reduction of oxidation rate. of gassification vs. temperature for graphite rods exposed to carbon dioxide discharge. 5c 4c 3c 20 IC 1.5 2 .o 2.5 3.0 3.5 WALL TEMPERATURE, x lo3 Fig. 4. Effect of wall temperature on the oxidation rate of graphite.
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)i 1 reesonably complete and accura
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3 inquire about the component of ve
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4 I I 5 To find (t2)av, we assume t
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\ vnich, it is noted can be negativ
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I 7 than or smaller than the second
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i I i I I I ) ) i L , I I . INT1:OD
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13 field per electron is and per co
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. 11. 5. CharRe-Transfer and Ion-Mo
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17 In the followin:: sections much
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above. With that EIN, an estimate o
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21 region in w!iich large, nighlv l
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i ’ understanding: 23 (a) Electro
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Obviously, the secondary ion must h
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27 (22) Franklin, J. L., Munson, M.
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Tables 1-6 present examples of rela
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Table 8 Some Ions Formed by Process
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33 velocity of the reacting partn r
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35 must be added to the Langevin cr
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37 In our laboratory a microwave di
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+ . 4 . r 39 as well as N in a cor0
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ION-MOIECULE REACTION RATES MEASUFI
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43 excitntion 2onditions so that th
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45 In 2 like manner Fig. 3, showing
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47 Absorption Spectra of Transient
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50 maximum fiela. In this manner, a
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52 3 % %- %- 5- a- 7 h W P H 0 L v)
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References I I . A.B.Callear, J.A.G
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._ . _-.. - , , . . ,. . The Pyrex
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58 0 0 0 VI J > I cv . u H a
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.... . 0 2 e I / m 0 H F4 : 1
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\ 0.9 0.8 0.7 06 0.5 0.4 0.3 0.2 01
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65 ' cause of the reduction in the
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INTRODUCTION I' Attachment of polar
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I 69 EXPERIMENTAL The mass spectrom
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+ Figure 1 Mixed water and methanol
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73 ' , radius might be expected bec
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75 Negative Ion Mass Spectra of Som
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A b 1 1 I H I I I FILAMEN T CONTINU
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79 for positive and negative ions,
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51 out to answer some of the questi
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93 INTERACTIONS OF EXCITED SPECIES
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L 4 I*C z 0'2 = a, a U x I m 4 m 0
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I L I, ; > > E Fig. 3 I50 200 150 1
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I 300 r 1 - 200 i io ;' a cn I I. 0
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where DISCUSSION OF XESULTS PERTAIN
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93 where the bar indicates values c
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'I i 'I 0 2. 4 6 8 2 [ N]* x' I 0-2
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Fig. 14 IO 8 6 4F [NO] x IO-" (mole
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for chemiluminescent excitation in
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101 Chemiluminescent Reactions of E
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103 All gases were taken directly f
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10; He: + N2 -. 2He + h': (8) whi!?
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description for both diffusion and
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B. Ions and Electrons I Consider a
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' 112 axial diffusion through the d
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the tube walls occurs continuously
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E2R M ' $6"
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1. 2. 3. 4. 5. 6. 7. 8. 9- 10. u. -
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120 . Dlschorge zone Reactor zone 1
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122 In radiation chemistry the cust
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124 4. chemistry seem limited essen
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126 Conversion of Mixtures into Mor
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Hydrazine Synthesis in A Silent dle
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{;I . - . .. . - .., . . .. _- .. .
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1 \ \ \ , \ , \ \ Pmer hnrity K.W.
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. I operating fact that the sloGe i
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_- of ' . 8. - 7 6, Residence Time
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135 Ionic Reactions in Corona Disch
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GAS OUT GAS IN i.ho QUADRUPOLE MASS
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- + ( ~ ~ + 0 H ) ~ O ~ ( H~o)~H+ +
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144 i I , , , , . + 1- u 3c w Inu c
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146 SYNTHESIS OF ORGANIC COIGhTDS B
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mi5 a- dz CI n I a I n +4 - 0 -I- k
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0 z cu I I I
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I- I - t d m a .rl Y x c, t-' d k
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, 155 This result is significant in
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Compound Bond he rgy Li I 82 UBr 10
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, ”..’ 3or 25 - 5 20 - s 3 w Y
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I 161 THE GLOW DISCHARGE DEPOSITION
Page 163 and 164: Fig. 1 Process Apparatus -__l.ll__
Page 165 and 166: v) t- at- InIo Io0 t-Q) loo lcua O
Page 167 and 168: This study is only an approximation
Page 169 and 170: Mole Reaction Material ratio time e
Page 171 and 172: \ i (4) Effect of System Pressure T
Page 173 and 174: 173 Pressure. Since pressure is a c
Page 175 and 176: 175 Table VI X-RAY DATA OF DEPOSIT
Page 177 and 178: 177 Another source of weakness is t
Page 179 and 180: 179 PLATING IN A CORONA DISCHARGE R
Page 181 and 182: \ 3 , ,\ 110 v 60 CPS MANOMETER . F
Page 183 and 184: I i , \ I i & a - P Fig. 3 Reaction
Page 185 and 186: \ \' C 0 .d * d .- C U d 0) c( 1) L
Page 187 and 188: I i I . Q) I, s w 0 v) Y 0 a w W a
Page 189 and 190: I (b) Polarized Light Fig. 6 Cross
Page 191 and 192: i m v) Y C i! u o) 23 a a- + 191 m
Page 193 and 194: i, d C .d c c W Q ) 0 0 L1Y 0 000 0
Page 195 and 196: i e 4 0 wcr -4 4 al 0 0 0 c) cr 13:
Page 197 and 198: \ E ‘ 1 TIME FOR RUN 13-1 14-1 -
Page 199 and 200: 199 a red heat in this cell using d
Page 201 and 202: \ , t j \ I, v) 2 Y . C 0 u m .I C
Page 203 and 204: 203 VAPOR PHASE FORMATION OF NONCRY
Page 205 and 206: BELL JAR STANC TO VACUUM SYSTEM U T
Page 207 and 208: 207 of the boron oxide film, the fi
Page 209 and 210: i I, 4 I.( Y I- * 0 i f i 3 0.t I I
Page 211 and 212: 211 The Reacticn 3f Oxygen with Car
Page 213: 2 E, W t- a Z 9 I- a 2 X 0 I50 too
Page 217 and 218: I- z W 0 w a a 100 80 60 40 20 215
Page 219 and 220: s., Literature Cited Berkley, C. ,
Page 221 and 222: 7 h \ F 221 600°C and 1 atmosphere
Page 223 and 224: 223 e I'
Page 225 and 226: R L ' -1 9mm O.D. 5mm I.D. 45mm 0.D
Page 227 and 228: Figure 5.- Paschen's law curves. 2-
Page 229 and 230: \ '? I The water-free product gases
Page 231 and 232: N I + 0" ON i I + 0 u / 0 0 I 0 cu
Page 233 and 234: - 233 SOME PROBLEMS OF THE KINETICS
Page 235 and 236: .. . :. ,. .I , . i ? .. . , ... .
Page 237 and 238: 237 Table 2 Experimental Variables
Page 239 and 240: 239 Zhbie I Eerccnt Consumption of
Page 241 and 242: 241 Discussion The systematic varia
Page 243 and 244: I \ 1 243 FORMATION OF HYDROCARBONS
Page 245 and 246: h z - a o m a 20 T IME, minutes . F
Page 247 and 248: I 1 I I I I 0 I 2 3 4 5 TIME, minut
Page 249 and 250: The next five coluws in table 1 sho
Page 251 and 252: \ .\ t 251 Given the existence of t
Page 253 and 254: I L 253 Epple, R. P. and C. M. Apt.
Page 255 and 256: 1 ' Fig. 1 Schematic of flow discha
Page 257 and 258: 5' . ' I 1 257 co, with excess H2,
Page 259 and 260: 1 1 1 moo 1400 1300 c V' I IPOO I I
Page 261 and 262: i 25i The Dlssocfatior of ToIuere V
Page 263 and 264: L ! , c PRODUCTS FROM A 28 MC. DISC
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'\ J ?. , .. . : PRODUCT FORMATION
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'9 / I '\ "1 BENZYL CATION AND RADI
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a
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271 tube serve? as the high voltare
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273 ion (1L.). Zxcitei-ion by colli
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Apparatus and Procedure 275 EXPERIM
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. 277 6. A freshly prepared sam le
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observed. The polystyrene (10% solu
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i i (12) c (11) (14) I 281 LITERATU
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FLOW- METER I ADDITIVE SUPPLY * ,28
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285 TABLE 2 Effect of Haloqenated A
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ANALYTICAL RESULTS Some evidence wa
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DISCUSSION 289 The salient features
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? ~ MENBERSHIP IN THE DIVISION OF F
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292 flow of the reactant gas stream
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294 have suitable residence times i
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0 E < h( E l! d K c 0 .- Y 0 t u t
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298 yields of many chemical product
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- ;i Y . 15. Pressure lOmm 5 > 10-
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302 the best and in many practical
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GENERATION AND MEASUREMENT OF AUDIO
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. The transformer secondary and the
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Vaccum-Tube Amplifier The mobile co
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310 f = Power supply frequency in c
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FUFARCI! INSTITUTE OF TFYDLC UNIVER
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J # I / 4) I . . '8 r4 0 r( P
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317 i Cuencb svsten w.nnar;itus use
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epcrte? the noss~kil.itv of nroduct
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1' b t +
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323 ....... - . . . . . . . . . . .
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1 \ i I i , / / / 8 3 1 325 To205 +
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- .- - - . - - . . . - . 327 n + c
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' POWER PLASMA GAS l e , ' I ! I I
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331 f'ENI?AL PF'FCLCCFC Dernis, P.R
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i J 333 ; mosphere (as opposed to a
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; it raised the question, still &?z
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p .I V I .= - - HCN/C(CALC. WITH C
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1 1 339 atmospheric ressure and ach
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RESULTS 341 Composition Dependence
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0.09 0.08 0.07 9 0.06 2 U - .$ 0.05
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II \ to the Slot So that less of th
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i 4 2 HYDROCARBON-NITROGEN REACTION
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I 1 349 c M m ; a e, k M x
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1.0 I - a. I n TEMPERATURE - OK Fig
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353 the experimental results in the
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,) 355 The ceaswed conversion cf ni
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1 6 357 Freezing. 3jpotnesise thzf
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359 \ Frozen Compositior: Calcillat
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I 1 \ 361 -. ne reaction proceecis
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\ 36 3 ' h, I 26. H. Purnell, Gas C
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In experiments on the direct conver
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367 used as blnders, with different
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369 ' i 1. REFERENCES Berber, John
Page 372 and 373:
Distribution and yield rates of pro
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. . I . I 370 . . . . ., . . .. . .
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4 372 090- > E w - m c N O - 0 z :
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A-Feed tank 6-Thermocracker GReceiv
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80 \ 0 70 60 e 40 a U VI 9 30 20 10
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COAL DEASH& AND HIGH-PURITY COKE Wa
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3Pn _. -. - L -J:,J.-;~~~L, ):as se
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S ~ l ~ o n~pg:ading r is the resul
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The range ~f temperatures and gener
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. .. 386 9 * - r. Y 2 .' d a f' r.
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.) .L m 388 I
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TABLE 4 390 DELAYED COKING OF DEASH
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, ! I- on '---
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394 The present method is to keep t
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396 ‘c erperature, while the pres
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2, '! ! Proximate Analysis, wt $ Mo
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0 IS 0 14 LL 9 013 e \ 3 b- m *- 01
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402 HYDROGEN CYANIDE PRODUCED FROM
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404 Before startup, the system is p
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4 OL. ' , I. . TesCs. With.Coals .o
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Table 3.- Product Gas Analyses and
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410 BIBLIOGRAPHY 1. American Public
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Figure 2. Enclosure surrounding hyd
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0 0 f v) C 0 u m I z 2 c 2 r d J w
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0. E c .4 7 .. .c . I ( - Low tempe
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418 cual. A mjor aa\;antage or' the
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420 Ir ?Y ? ? 9 9 9 pc rod n o c o
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422 Table 3. Room-texperature M'dss
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424 state, depending on the strengt
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Table 4. Room-?;ergerature isomer s
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I' 1.3 . /o 9 IO 9 6 a 425 F F 33 I
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Brooks J.D. and Sternhell S. (1957)
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(52) Gib3 T.C. and Greenwood N.N. (
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434 transducer vas then introduced
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436 yield is quite similar. The con
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?-!??? 0 mv, Uh\OhIe . . . . eirlrl
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4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 4
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442 CHEMICAL REACTIONS IN A CORONA
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helium 444 CORONA REACTOR SYSTEM Fi
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446 The ultraviolet spectrum. for t
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Biphenyl Fraction 448 The low molec
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LUd The actual structural definitio
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I I I I I In m 9 In 2 , I: r- In m
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’. 454 Mechanism I The available
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456 , , . The relatively low yield
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458 h/lethylacetylene, allene and b
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Introduction VAPOR PHASE DECOMPOSIT
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462 more efficient hydrogenation. T
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464 place in parallel with fragment
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466 P rl 0, k 7 rnI rn al k a I hl
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458 TABLE I. COMPOSI'IION OF GASEOU
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REFERENCES 1. C. Hirayama and D. A.
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i 472 Reciprocal Arc Enthalpy ,-> F
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474 be pumped down without altering
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476 Instead a hydrogen deficient fi
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i 478
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480 FATTY ACIDS AND n-ALKANES IN GR
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482 TA5L,E 2. - Carbon number distr
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6. 7. a. 9. 484 Lawlor, D. L., and
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' I ' Sample No. 6 ' 12 IO 8 6 z 4
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. 488 uiolecular weight of which ca
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Xississippi (Sample GS). Stock solu
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492 found at 5.7 and 4.9& for the W
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494 mechanisms. However, the voltad
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For pure polynuclcar arom.i;ic hydr
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- '-'. . ' . . values are listed in
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500 (1;) Ten, T. 17.: a;1d,Dic;
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- ~ Resistivity Czlculation 2: 1 j:
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504 o ' C 0s 2 0 v x i 8 2 0 ! P -
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506 i
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d 601 L P LL
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I I I I I I I I m W N W N 0 (D ? 0
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514 was heated under nitrogen in a
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The line broadening at 79OK of the
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13. 14. 15. 16. 17. 18. 19. 20. 21.
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W L, Z 6 m (1: 0 6 d j o 2 ' 1 0.0
Page 526 and 527:
Coals 522 Studies of the 1600 cm-l
Page 528 and 529:
L in ole i c a c id - 0' Two sample
Page 530 and 531:
526 Table 1.- Ultimate analyses of
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528 6. Friedel, R. A., and H. Retco
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egeneration. The system can be seen
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532 and can be expressed in terms o
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534 in the vapor increases with inc
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NH3 NH3 NH3 NH3 Pyridine Pyridine P
Page 542 and 543:
Mole Ratio of Test No. Quinoline to
Page 544 and 545:
IXPROFJCTION D; M. Mason Institute
Page 546 and 547:
-4:c~rciiny to recent studies o ;i4
Page 548 and 549:
544 Table 1. LIGHT EMISSION OF Y"TR
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emission in a few cases may be by d
Page 552 and 553:
LITERATUR2 CITED i. C. -. .' * il.
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co, CH,,OR 1 - OTHER ADDITIVE FRITT
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FRIT 'TED CO, CH,.OR 4 ___ OTHER AD
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340 350 300 400 4 50 500 600 700 80
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0 554 WITH COOLING (PLATE AT 40°C)
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5 56 then t = to when e = 0 2) the
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5 58 The surface heat transfer coef
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Discussion and Results 560 Three br
Page 568 and 569:
__- ._ 562 Table I THERMAL AND PHYS
Page 570:
ln 4 I 0 4J v \ 1.0 0.8 0.6 L - 0.4
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