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RAD CALS

• W. E. Wilson, Jr. and R. M. Fristrom In

adicals are an essential in in a steady-state it is only necessary that R . Although present in low concentra­ chain branching balance chain breaking. tions, they are responsible for ignition and for the These species are so reactive that their lifetimes rapid reaction rates observed in flames. A are very short. It is necessary, therefore, to utilize is an or group of , which, in chemical unusual techniques to study them. Cochran, terms, has a free valency and may react to form a Adrian, and Bowers~ in a recent article, discussed more stable . Except for unusual cases or the use of liquid helium to stabilize at low tempera­ extreme environments, radicals may be considered ture radicals formed by photolysis. l as highly reactive, transient chemical species. Some The present paper will discuss the study of radicals of the important radicals in and hydro­ in the high-temperature environment of flames. carbon flames are hydrogen atoms (H), hydroxyl Since the general problem of studying flames radicals (OH), atoms (0), and methyl has been discussed previously by Fristrom and radicals (CH3). Westenberg,2 only the determination of radicals in An illustration of how radicals enhance the rate flames and the application of these results to the of a reacting system may be had by examining the study of will be considered here. hydrogen-oxygen flame. An undisturbed mixture of H 2 and O 2 is quite stable at room temperature. Deterlllining Radical Concentrations However, if a few H or OH radicals are introduced, in Flallles the following reactions take place with sufficient Determination of the concentrations of atoms and rapidity to maintain a flame: radicals has been a major problem in chemical (I) OH + H 2 ~ H20 + H kinetic studies for a number of years, and has usually been avoided by application of the "steady­ (2) H + O 2 ~ OH + 0 state approximation." This assumes that radicals

(3) 0 + H2 ~ OH + H TABLE I (4) H + H + M ~ H 2 + M ATTAINMENT OF STEADY STATE IN A HYDROGEN- FLAME These illustrate several peculiarities of radical reac­ tions. In (I), we see that a radical-molecule reaction Required Time may generate a new radical, which in turn may re­ Temperature (OK) Available act with another molecule, regenerating the origi­ (% ) nal radical. This is called a chain reaction. Re­ actions (2) and (3) are examples of chain branch­ 1050 ing where one radical may generate two more. 1200 5 Trimolecular chain-breaking reactions, such as 1300 10 reaction (4), are much slower than the bimolecular reactions. This mechanism, whereby one active 1 E . L. Cochran, F. J . Adrian, and V. A. Bowers, "Trapped Free Radi­ cals," APL Technical Digest, 2, Jan.-Feb. 1963 , 2-9. species gives rise to many more, is responsible for the rapid rate of reactions involving radicals. While 2 R. M. Fristrom and A. A. Westenberg, "Fundamental Processes and Laminar Flame Structure," APL Technical Digest, 1, Jan.- Feb. 1962, chain-branching reactions are essential to ignition, 10-15.

2 APL Technical Digest Radicals in flames may be studied by: direct, molecular-beam, ; optical ; probe techniques; or by derivation from kinetic constants. It has been shown that radical concentrations greatly exceed equilibrium values and that active species diffuse from the reaction zone back into cool gases. Profiles of hydrogen, oxygen, hydroxyl, and methyl radicals in a -oxygen flame are given as examples. The chemical kinetic constants of elementary reactions are the most important information to be derived.

react at the same rate at which they are formed and local concentrations must be determined with con­ that their concentration may be determined from siderable precision point by point through the flame equilibrium considerations. The validity of this front. The latter requirement is quite stringent assumption in rapidly reacting systems is highly since flame fronts are normally only a few milli­ questionable. An illustration of this point is given meters thick.3 Because a number of separate de­ in Table I, in which the reaction time required terminations of local concentration are necessary, to reach the steady state is compared to the actual the primary requirement is spatial resolution well time available in a hydrogen-bromine flame. 3 below a fraction of a millimeter. Clearly, in this flame there is not sufficient time Although none of the present methods is com­ available for operation of the steady-state approxi­ pletely satisfactory, they have enabled investigators mation. The determination of radicals in flames to make much progress on a problem once thought becomes, therefore, an experimental problem. to be completely impossible. VVe will discuss Free radicals have been investigated in several briefly the methods that have been used, with ways: absorption, paramagnetic reso­ emphasis on the techniques we have used and with nance, mass spectrometry, gas-phase titration, opti:" which we are most familiar. cal spectroscopy, and recently, a new technique RADICAL CONCENTRATIONS DETERMINED BY DIRECT developed at APL called "scavenger sampling." MASS SPECTROMETRy-One of the most reliable For two important reasons, only a few of the ex­ methods for determining radical concentrations in perimental techniques mentioned above are suit­ flames is direct mass spectrometry. The radicals able for quantitative flame studies. The experi­ must enter the spectrometer chamber with only mental problems are complicated by the high a few, or preferably no, collisions after sampling. temperatures in flames; and for quantitative work, This is best accomplished by using a molecular beam-sampling mass spectrometer of the type developed by S. N. Foner and R. L. Hudson GAS-SAM PLING SYST EM at APL (Fig. 1).4 This system has been used primarily for studying radical reactions induced by electric discharge, but it has also been successfully applied to the study of radicals in diffusion flames and to the study of stable species in flames. 5 Through use of the apparatus, it was established

that H02 was not present in detectable amounts in MASS diffusion flames of hydrogen and oxygen, but could ANALYZER be produced in substantial quantities in discharge­ tube systems.

Fig. I.-The determination of atoms and radicals by 4 S. N. Foner and R. L. Hudson, "The Detection of Atoms and Free direct mass spectrometry. Radicals in Flames by Mass Spectrometric Techniques," J. Chern. Phys., 21, Aug. 1953, 1374-1382.

a G. C. Frazier, Jr., R. M. Fristrom, and J. F. Wehner, "Microstructure 5 R. Prescott, R. L. Hudson, S. N. Foner, and W. H. Avery, "Composi­ of a Low Pressure Hydrogen-Bromine Flame," A.l.Ch.E. Journal tion Profiles in Pre-Mixed Laminar Flames," J. Chern. Phys., 22, Jan. (accepted for publication, 1963). 1954, 145-146.

July -August 1963 3 The instrument was intended for identification 10 to 50 microns in diameter. A large pressure drop of radicals and is not suitable in its present form is maintained across the probe by pumping on it, for quantitative studies of flame structure. The inlet with the result that the system acts as a miniature disturbs the flame and gives poor distance resolu­ supersonic nozzle. The sample being withdrawn tion. While it should be possible to design a experiences a rapid adiabatic decompression, and molecular-beam probe that would circumvent within a few microseconds the temperature and many of the problems of determining radicals, pressure are so low that reaction rates in the gas molecular-beam mass spectrometers are expensive phase become negligible. This is the well-known and difficult to build, requiring, in particular, frozen flow that occurs in rocket nozzles. Even powerful vacuum pumps to maintain high pumping reactive radical species survive a number of centi­ speeds at low pressures. meters down the probe before they recombine on RADICAL CONCENTRATIONS DERIVED FROM SPEC­ the probe walls (gas-phase recombination is negligi­ TROSCOPIC STUDIEs-Radical concentrations have ble under these conditions). been determined spectroscopically in flames, using In some cases it is possible to inject into the both absorption and emission, a technique that has sampled gas stream a stable substance that reacts the virtue of not disturbing the flame. Its major quantitatively and specifically with the radical disadvantages are the difficulties in finding suitable species under study to give a stable product that can absorption lines, interpreting the emission spectra, be analyzed by mass spectrometry; the injected re­ and obtaining sufficient spatial resolution. It has actant is called a " scavenger. " Thus, the radical been limited in practice to the study of hydroxyl concentration can be deduced from its one-to-one radicals (absorption) (Fig. 2) 6 and hydrogen atoms correspondence with the product species. This (emission). Absorption spectroscopy is quite technique has been used successfully to study hydro­ straightforward in principle, although the experi­ gen atoms by reaction with chlorinated hydrocar­ mental problems are moderately complex. The bon, methyl radicals by scavenging with iodine, absorption of light is directly related to the concen­ and oxygen atoms by scavenging with tration, i.e. partial pressure, of the absorbing dioxide. Its extension to the study of other radicals molecule. The interpretation of emission data is depends on finding suitable scavenger reactions. more complex, the most successful studies having DERIVATIONS FROM KINETIC CONSTANTS- It is been made by an ingenious technique that involves possible to deduce radical concentration in flames introducing a trace C::::::~ lO-5 mole fraction) of a from the measured concentration of stable species pair of the alkali metals, one of which forms a stable hydride, the other, not. The concentration of hydrogen atoms can be derived from measurements of the relative intensity of the lines of the two alkali metals and the known equilibrium con­ LIGHT stant of the reaction. This latter technique has been SOURCE used to study the radical recombination region in 7 hydrogen-air flames. 0.06 ,------.------,------.-----....., RADICAL CONCENTRATIONS BY THE SCAVENGER PROBE TECHNIQUE-A method recently developed 0.05 1------+---1-- --""""';::---- at APL for the study of radical concentrations in flames, the "scavenger sampling probe technique" z 0.04 I------+---II ---+-----~..,___---~ (Fig.3A), combines the techniques of microprobe Q 8 f- sampling and chemical scavenging. The quartz U B microprobe used for studying stable species in ~ 0.03 1------1--,----+------+------1 flames consists of a small, uncooled, quartz tube w o-' with a tapered tip ending in a small sampling orifice "2 0.Q2 I----jf---+-I'------+-----+-----~

6 U . Bonne, T . Grewer, and H. Gg. Wagner, "Messungen in der p=20 mm Hg Reaktionszone von Wasserstoff-Sauerstoff-und Methan-Sauerstoff­ 0.0 I I---f-.f-- -F+------+-----="'!""'- ...... =- -~ Flammen," Zeitschrift filr Physikalische Chemie, Frankfurt, 26, 1960, 93-110. O ~~------~------~------~------~ 246 7 C. G . James and T . M. Sugden, "Photometric Investigation of Alkali o DISTANCE FROM BURNER SURFACE, Z (em) Metals in Hydrogen Flame Gases. I-A General Survery of the Use of Resonance R adiation in t he Measurement of Atomic Concentrations," Fig. 2.-The determination of con­ Proc. Roy. Soc ., 227,1955, 312-329. centrations in low-pressure Hames. (A ) Schematic

8 R . M. Fristrom, "Scavenger Probe Sampling: A Met hod for Studying of the apparatus; and (B ) OH profiles for severa] Gaseous Free Radicals," Science, 140, Apr. 19 , 1963,297. stoichiometric methane-oxygen Hames.

4 APL T echnical Digest 0.025 ,------Results of Radical Concentration DETAIL OF PROBE Studies in Flallles ------GAS SAMPLE "",CONTAINING One of the first results of quantitative studies was 0.020 I------,I-~ NO 2--.0 ~ - OXYGEN the discovery that the radical concentration in O+NOz- NO+02/ ATOMS flames was much higher than that predicted by z l~, thermal equilibrium. This led to the realization g0 .0 15 /----1---, U that the rapid bimolecular reactions involving free < s: radicals do not reduce the overall radical concen­ w 00.0 I0 1----I---+-----"~---____1I__---_I tration but merely change one radical into another, L B and that the radicals must be removed by slower trimolecular reactions. Consider the reactions of 0.005 1----I---+----+--~Io..-__1f__---___j the H 2-02 flame mentioned earlier. In the later stages of the flame, the reverse reactions must be considered also. However, reactions such as (1), o ~~---~------~------~ ______~ o 1.0 2.0 3.0 4.0 (2), and (3) do not reduce the number of radicals; 1600 DISTANCE FROM BURN ER SUR FACE, Z (em) they maintain a quasi-equilibrium among the bi­ I II I I I I I 350 1500 1700 1600 1500 1400 1300 1200 1100 molecular steps so that the ratio of H, OH, and 0 TEMPERATUR E (OK) is the same as in thermal equilibrium, hence Fig. 3.-Scavenger probe technique for determining calculable from thermodynamics, while the total radical concentrations in Hames. (A) Schematic of radical concentration may be far out of equilib­ the apparatus for studying oxygen-atom concen­ rium.7 trations; and (B ) an oxygen-atom concentration When two small radicals combine, as in reaction profile in a methane-oxygen Harne. (4), they release more energy than can be absorbed internally so that the molecule would be dissoci­ if the kinetic constants of the species that react with ated unless there were a third body available to the radical are known. This procedure is valuable carry away the excess energy. Such trimolecular since it allows estimates, not otherwise available, reactions are slower because of the lower prob­ to be made of radical concentrations. ability of three colliding simultaneously For example, consider the reaction given by the than of two molecules doing so. At atmospheric chemical equation pressure the number of three-body collisions is only co + OH P CO2 + H. (1) one for every thousand bimolecular collisions; this ratio is proportional to pressure. Below a tenth of For this reaction it is possible to write a mathe­ an atmosphere,the recombination is so slow that the matical equation, flame gases may reach the walls of the apparatus before recombination can occur. In many such systems, the heat losses to the wall cool the flame where R is the rate of formation of CO2, K f is the gases so rapidly that the radical concentration may rate constant in a forward direction, Kr is the rate be frozen far out of thermal equilibrium. constant in a reverse direction (where K is a func­ Another aspect of radicals in flames is that be­ tion of temperature), and the terms in brackets cause of diffusion effects they can often 'f'eact in a indicate the concentration of the mixture com­ region of a flame upstream of, and hence earlier in ponents. the reaction path than, the point at which they are Measurements of R, [CO], and [C02] can be formed. This peculiarity is responsible for the made. If K f is known, and K r[C02] [H] is small rapidity of the reactions and for the elimination of compared with the forward rate, it is possible to many of the slow, complex steps found in lower­ calculate [OH] from the equation temperature oxidations. In order to give a mathe­ R matical description of this effect, it is necessary to [OH] = Kf[CO] . (3) introduce a new variable, flux, which is the amount of a species passing through a unit area in a unit This approximation is to be distinguished from time, as opposed to concentration, which is the the steady-state method that assumes that the amount of species per unit volume at a point. The radical concentration can be expressed in terms of two variables are related by the equations the stable species and equilibrium constants. The assumption that the reverse reaction can be (4) neglected is usually better in the early stages of a and flame. (5)

Ju ly -August 1963 5 where G is fractional mass flux, D is the diffusion transfer to the walls, resulting in partially "frozen coefficient, f is mass fraction, v is mass average radical concentrations;" characteristic profiles for velocity, V is diffusion velocity, z is distance, and this system are shown in Fig. 5. Temperature pro­ subscript i refers to species i. In flames in which the files were measured with small, silica-coated, Pt, concentration gradients are very steep and the Pt-IO % Rh thermocouples. Composition profiles effects of diffusion are appreciable, Vi.can become of the stable species were determined by micro- greater than v. This means that for this species the diffusional flow due to concentration gradients is TEMPERATURE (OK) larger than the overall species mass flow; overall 750 1000 1500 1680 1675 mass flow remains unchanged, of course. An ex­ r-~------~------~------ample of this behavior is given by the oxygen atoms VELOCITY (em/sec) in a methane-oxygen flame. Oxygen atoms are 150 200 250 263 225 200 formed in the main flame reaction zone but diffuse back into the unburned gases to initiate reactions (Fig. 4). In the ordinary flow system, where dfd dz is very small, the two variables are identical when H O expressed in dimensionless units (such as mass "I 2 85 14 fraction and fractional mass flux). z~ « z UJ l!) 8 12 >- The Spherical Prelllixed Methane­ X d' A 0 Oxygen Flallle U 10 80 0 . c5 UJ The most complete information on radical con­ l!) i ' « centrations has been obtained from a spherical, f- 0 Z low - pressure, methane - oxygen flame 9 having O 2 U trY or: spherical symmetry and supported on a spherical « UJ f- a... ball in a large flask. At low pressure the radical Z UJ recombination is so slow that radical equilibrium U 0 ~ 75 L is not attained until the walls of the flask are UJ 4 reached. The flame is not adiabatic because of heat 0 L

0.02 0 70

1.4 I Z 0.0 1 o i= u l or:« LL .~ ,7 12 ~ UJ -' " NEGATIVE FLUX DUE o ~\ 1.0 " / TO BACK DIF FUSION L_O.OI 2.0XI0-; UJ l!) « \ ' / ~ C------~ u f- B " "I (l) z 0.8 \,l 1' .0 -0.02 u -B------'..... -- ---..~ Ql ~ 0 UJ 0.6 ..s. -' UJ 0 A- Rt:gE.C ATO . -1 .0 ':( L or: 0.4 -, B _ )< (E. A UV FOR'v1A 0 -2.0 '--_~_-' _~_-,-~_c -~~B ~ 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 DISTANCE FROM BURNER SURFAC E. Z (em) 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 Fig. 4.- Reaction of oxygen atOInS in a Inethane­ DISTANCE FROM BURNER SURFACE, Z (em) oxygen BaIne, showing (top) concentration and Bux fraction and (bottoIn) reaction rates. Fig. 5.-Characteristic profiles of a preInixed, spherical, Inethane-oxygen BaIne (CH 4-7.8%

9 R. M. Fristrom, Sec. 2.1 of Experimental Methods in Re­ O 2-92%; p= 0.05 atIn); (A) stable species, and (B) search, J. Surugue, ed., Pergamon Press, New York, 1961. radical species.

6 APL Technical Digest probe sampling and mass spectral analysis;lO velocity was calculated from the density and area. i135 ~ The radical concentrations for the methane­ 13.0 oxygen flame were derived by several techniques. 5 7 9 X 10-4 H ydrogen atoms were estimated from the disap­ ~ I/ T pearance rate of oxygen, assuming known kinetic constants and that the reaction H + O 2 ~ 6 } FLAME OH + 0 is responsible for oxygen disappearance. ~ STRUCTUR E ~ STU DIES The order of magnitude of the results was confirmed o by scavenger probe studies on a similar flat flame. z + } FLOW REACTOR Oxygen atom concentrations were measured using o X STU DIES i= scavenger probe sampling based on the scavenger U w« reaction 0 + N0 2 ~ NO + O 2. The OH con­

Applications the simpler flame systems that can account quanti­ The most important information to be derived tatively for the observed behavior. One of the in­ from radical concentration studies are the chemical teresting points is that in all of the reaction schemes kinetic constants of the elementary reactions. If it proposed, radicals play a dominant role. is possible to obtain a profile of the radical concen­ Since radicals are so important in the propa­ tration as well as the stable species and rate pro­ gation of flames, yet are present in small amounts, files, then it is possible to compute K (see Eq. 3). we may properly wonder if flames cannot be in­ An example of this procedure is given by the reac­ fluenced by manipulation of radical concentrations. tion of the hydroxyl radical in methane-oxygen It is possible, for example, to double the flame speed flames. Here it has been established that both car­ of the carbon-monoxide-oxygen flame by changing bon monoxide and methane react primarily with the concentration from 0.1 % to 0.2 %. The the hydroxyl radical. Since the kinetic constants water provides a source of OH and H radicals. for are reasonably well known, This allows CO to be oxidized by the reaction the hydroxyl concentration may be calculated. CO + OH ~ CO2 + H, which is much faster than This in turn may be used to determine the kinetic any set of reactions utilizing CO + O 2 or CO + O. constants of the methane-hydroxyl radical reac­ The OH is regenerated by the reaction H + O 2 ~ tion. By combining high-temperature data from OH + 0 to permit a rapid chain reaction. flame-structure studies with low-temperature data In the opposite direction, a small research effort from the reaction of methane in a discharge tube, it at APL is devoted to the study of slowing down .has been possible to derive kinetic constants of flames by removing radicals or substituting unre­ good precision (Fig. 6). The excellent agree men t active radicals for the chain carriers. The method of between these two temperature extremes demon­ operation of such chemical extinguishers as strates that the identification of these reactions is carbon tetrachloride and bromotrifluoromethane essentially correct and that simple collision models (CF3Br), now used in many fire extinguishers on of chemical reactions are adequate for describing aircraft, is the substitution of the less reactive such systems in the extremes of temperature found or bromine atom radical for the oxygen, in flames. hydroxyl, oY hydrogen radical. Since chlorine and It has been possible to identify and obtain kinetic bromine atoms are relatively stable and unreac­ constants for a number of elementary reactions in tive, they do not propagate the chain reactions. flames, and to write reaction schemes for some of Similarly, the tetraethyl added to gasoline is a free radical scavenger that controls the free radical ) 0 A. A. Westenberg and R . M. F ristrom, " Methane-Oxygen F la me Struc­ distribution and concentration in the internal t ure. IV. Chemical Kinetic Considerations," J . Chern . Phys., 65, Apr. 1961, 591- 601. combustion engine, preventing too early ignition.

Ju ly - August 1963 7