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烃类燃料氧化动力学机理与模拟研究

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烃类燃料氧化动力学机理与模拟研究(on_the_kinetics_of_hydrocarbons_oxidation_from_natural_gas_to_kerosene_and_diesel_fuel)

摘要:

本文系统研究从天然气到煤油、柴油的烃类燃料氧化动力学,采用激波管、搅拌射流反应器与层流火焰实验,构建层级式详细化学反应机理。以甲烷、乙烷、丙烷等小分子组分构建天然气模型;以正癸烷、丙基环己烷、丙基苯替代煤油;以正十六烷、异辛烷等模拟柴油。机理覆盖烷烃、环烷烃、芳烃氧化路径,经组分浓度、点火延迟、火焰速度验证,能较好预测天然气与煤油氧化行为,柴油模拟因缺少多环芳烃机理仍需完善。研究明确关键基元反应与灵敏度,为工程燃料燃烧模拟提供模型与机理支撑。


Kinetic reaction mechanis ms are necessary for modeling the combustion, oxidation and ignition of commercial fuels consisting of complex mixtures of hydrocarbons. Since they are generally too complex to be considered in the models directly, simple model-fuels are preferred. These model-fuels consist in a simple mixture of hydrocarbons for which kinetic oxidation models are validated. The oxidation of a large variety of hydrocarbons was studied experimentally in a jet-stirred reactor to build the needed kinetic reaction

mechanis ms. These detailed kinetic reaction mechanis ms were assembled to model the oxidation of commercial fuels. The capabilities of these kinetic models to simulate the oxidation of natural gas, kerosene and gas oil are presented together with needs for new kinetic measurements.

Introduction

Practical fuels such as natural gas, gasoline, kerosene, gas oil (diesel fuel) are complex mixtures of hydrocarbons. In order to improve the combustion of these fuels while reducing the formation of pollutants, it is necessary to propose and validate kinetic reaction mechanis ms in simple and well-defined labora- tory  conditions  (i.e. plug-flow  reactors,  jet-stirred  reactors, shock-tubes, premixed flames) for the combustion of selected simple hydrocarbons representing the major components of practical  fuels. A practical  fuel will  then  be  represented  in the model by  a  simple  mixture  of hydrocarbons  called  the model-fuel. Results obtained for the kinetic modeling of the oxidation of practical fuels using simple model-fuels are pre- sented.  They  rely  on  experimental  results  obtained  in  this laboratory using jet-stirred reactors and shock-tubes and on experimental results taken from the literature (ignition delays, flame speeds, flame structures)


Experimental set-up used to obtain mode validation data

The  kinetic  reaction  mechanis ms  were  primarily  developed based on experimental data obtained in a jet-stirred reactor (JSR). The JSR experiment used was described earlier.1,2  The reactor consisted of a 40 mm diameter sphere made of fused silica (to prevent wall catalytic reactions) equipped with 4 noz- zles of 1 mm id for the admission of the gases which are achiev- ing the stirring. A nitrogen flow of typically  100 L h__1  was used to dilute the fuel. All the gases were preheated before injection, minimizing  temperature  gradients  inside  the  JSR. A regulated heating wire of ~1.5 kW maintained the tempera- ture of the reactor at the desired working temperature. The reactants  were  diluted  by  nitrogen  (<50  ppm  of  O2    and H2O; <1000 ppm of Ar; <5 ppm of H2), and mixed at the entrance of the injectors.1  High purity reactants were used in the experiments: oxygen was 99.995% pure and the neat hydro- carbons  were  >99%  pure.  Furthermore,  when  liquid  fuels were studied, they were thoroughly sonically degassed before use. A piston pump or an HPLC pump was used to deliver  the liquid fuel to an atomizer–vaporizer assembly maintained at  100–250 oC,  depending  on  the  boiling  point  of  the  fuel. The  reacting  mixtures  were  probe-sampled  by  means  of  a low-pressure sonic quartz probe. The samples (≤30 Torr 三 4 kPa) were  taken  at  steady  temperature  and  residence  time. They were an alyzed on-line by means of a GC-MS, and off- line, after collection in 1L Pyrex bulbs: low vapor-pressure che- micals  were  an alyzed  on-line  whereas  high  vapor-pressure compounds  and permanent  gases were  an alyzed  off-line.  In the experiments involving nitric oxide, a FTIR spectrometer was used for on-line an alyses. The experiments were performed at steady state, mostly at a constant mean residence time, t, the reactants flowing continually in the reactor, varying stepwise the temperature of the gases inside the JSR. A high degree of dilution was used (0.07–0.9% vol. of fuel), reducing tem- perature  gradients  in  the  JSR  and  heat  release  (no  flame occurred in the JSR).

Several gas chromatographs (GC), equipped with capillary columns (Poraplot U, Molecular Sieve 5A, DB5ms, DB624, Plot Al2O3/KCl, Carboplot P7), thermal conductivity detector (TCD) and flame ionization detector (FID), were used for the measurement  of  stable   species.  Compounds  identifications were made through GC/MS an alyses of the samples. An ion trap  detector  operating in  electron  impact  ionization mode (GC/MS Varian Saturn) was used. CH2O and CO2  were mea- sured by FID after hydrogenation on a Pt/H2  catalyst con- nected to the exit of the GC column. A good repeatability of the measurements and a good carbon balance (±10%) were generally obtained.


Kinetic modeling

The chemical kinetic modeling of the JSR experiments was performed using the PSR computer code3  that calculates spe- cies concentrations from the balance between the net rate of production of each species by chemical reaction and the differ- ence between the input and output flow rates of species. These rates were computed from the kinetic reaction mechanis m and the rate constants of the elementary reactions calculated at the experimental temperature, using the modified Arrhenius equa- tion: k = A × Tb × exp(__E/RT).

The ignition delays were computed, using the Senkin computer program,  assuming the validity of the constant volume approximation under reflected shock wave conditions.

The fuel-air burning velocities at 298 K, Su , were computed using the Premix computer package.5  Care was taken in the calculations to reach the final  solution  (no evolution  of Su when  the  number  of  mesh  points   is  increased);  typically > 100 points were computed.

The kinetic scheme used here is based on the comprehensive mechanis m developed for the reduction of NO by natural gas blends in simulated reburning conditions using a natural gas blend,6   methane,  ethane,  ethylene,  acetylene,  propane,  pro- pene,   n-butane   and   isobutane7–15    and   the   oxidation   of 1,3-butadiene,16      benzene,17      toluene,18      n-propylbenzene,19 cyclohexane and n-propylcyclohexane.2,20 The reaction mecha- nis m has a strong hierarchical structure; it is available from the author. The rate constants for reverse reactions were computed from forward rate constants and the appropriate equilibrium constants, Kc = kforward/kreverse , calculated using thermoche- mical  data.21–23   The  pressure  dependencies  of unimolecular reactions and of some pressure-dependent bimolecular reac- tions were taken into account when information was available (i.e., k(P, T)). In the course of the model development, first- order local sensitivity an alyses, Si,j = ∂ln(mole fraction of i)/ ∂ln(kj), were performed as well as reaction rates an alyses by computation of rates of consumption and rates of production for every species.

The oxidation and combustion of natural gas

Natural gas (NG) is a major and the simplest fuel widely used on earth. Its composition varies from one source to another (see Table 1). Nevertheless, methane, ethane and propane are the main hydrocarbon constituents of NG. To sustain and enhance the competitiveness of NG use in the production of energy and forecast the effects of changes in composition, we need to pro- vide engineers with predictable tools allowing the design of still higher  performance  burners.  Among  these  tools,  predictive kinetic reaction mechanis ms are needed. Such mechanis ms have been proposed based on methane oxidation, ignition and com- bustion  data, mostly. Very few used  data  obtained for  the oxidation, ignition and combustion of NG. Tan et al.24,25  pro- posed such a mechanis m that was further used and tested26–28 for the ignition, oxidation and combustion of natural gas. This natural gas kinetic reaction mechanis m was validated against JSR experimental results, consisting of mole fraction profiles of reactants and products, obtained in a wide range of condi- tions (1–10 atm, from fuel lean to fuel-rich conditions, 800– 1400 K, and variable residence time). Fig. 1 presents a compar- ison between the experimental data and the kinetic modeling for the oxidation of methane, a methane–ethane mixture, a methane–ethane–propane mixture and a standard NG oxidized in the same experimental conditions. These results clearly show that NG oxidizes easier than methane and that the methane– ethane–propane mixture is the best model-fuel to be used in these  conditions.  More  details  can  be  found  in  previous papers.24,25  Sensitivity an alyses indicated that in the JSR con- ditions, the most sensitive reactions are:

H + O2  → OH + O

H + O2 + M → HO2  + M HO2 + OH → H2 O + O2

HCO + M → H + CO + M

CH4 (+M) → CH3 + H(+M)

CH3 + HO2  → CH3 O + OH

2CH3 (+M) → C2 H6 (+M)

CH3 + O2  → CH3 O + O

CH3 + O2  → CH2 O + OH

The proposed kinetic model was also used to simulate the igni- tion of various methane and NG blend mixtures24,25  and the methane–air  flame  speeds.24    Fig.  2  provides  a  comparison between  our  recent  modeling  and  that  obtained  using  the GRI  3.0 mechanis m.29  As can be  seen from  this figure the models are in close agreement with the data.

The burning velocities were mostly sensitive to the kinetics of:

H + O2  → OH + O

H + O2 + M → HO2  + M

CO + OH → CO2 + H

HCO + M → H + CO + M

CH3 + H(+M) → CH4 (+M)

Further  validation  of  the   proposed  kinetic   scheme  were obtained for the interaction of NO with C1 to C4 hydrocarbons and  natural  gas  blends.6,7    Figs.  3–5  present  a  comparison between our modeling and the JSR data obtained by Chen and Malte    and at CNRS for the reduction of NO by methane, a methane–ethane mixture, and ethane. Again, the agreement between the data and the modeling is good, supporting the kinetic scheme used. However it was demonstrated7  that the GRI 3.0 mechanis m29  could not represent all these data due to  missing  reactions  in  the  NOx  sub-mechanis m.  Our  NG kinetic reaction mechanis m was used as a C0–C6  base set for the modeling of the oxidation of the more complex practical fuels considered here. These studies showed that the kinetics of the reactions producing and consuming HCCO was critical. Also, the kinetics of vinyl decomposition is very influential. Unfortunately, there is a lack of kinetic data for this reaction particularly concerning its pressure and temperatures depen- dencies.

image.png

image.png

Fig.  1    The oxidation of methane and mixtures with higher alkanes in a JSR at 1 atm and a residence time of 0. 14 s. A: CH4 0.3%, O21.2%; B: CH4 0.3%, O2  1.2%, C2H6  0.03%; C: CH4  0.3%, O2  1.2%, C3H8  0.03%; D:   CH4    0.3%,   O21.2%,   C2H6     0.03%,   C3H8    0.0046%;   E:   CH4 0.3%,O21.2%, C2H6  0.033%, C3H8  0.0063%, n-C4H10  0.00024%, iso- C4H10   0.00031%,  n-C5H12   0.00017%, iso-C5H12   0.00017%, n-C6H14 0.00017%). The symbols represent experimental data while the lines are the computed results.

image.png

Fig.  2    Methane–air flame speeds at 1 atm and 298 K. Our modeling is compared with the predictions of the GRI 3.0 mechanis m and the available data (AB72: ref. 30; AB73: ref. 31; GJ72: ref. 32; R71: ref. 33; L68: ref. 34; DL98: ref. 35).

image.png

Fig.  3    The reduction of NO by methane in a JSR at  1580 K, t = 9 ms, 5000 ppm of NO.36  The data (symbols) are compared to our mod- eling (lines).

image.png

Fig.  4    The reduction of NO by methane in a JSR at  1800 K, t = 9 ms, 5000 ppm of NO.36 The data (symbols) are compared to our mod- eling (lines).

image.png

Fig.  5    The reduction of NO by a NG blend (CH4/C2H6  10 : 1 mix- ture) at  1 atm (1350 K; t = 0. 12 s;  1000 ppm of NO; 7272 ppm of CH4 ; 728 ppm ofC2H6 ; [TFN] = [NO] + [HCN]). The data (symbols) are compared to our modeling (lines).

image.png

Fig.  6    GC/MS  an alysis  of  a  kerosene  TR0  sample  showing  the importance of n-alkanes.

oxidation rates in JSR37–39  and in flame conditions.40  Fig. 7 presents a comparison between JSR results obtained for the oxidation of kerosene and n-decane at 10 atm. It clearly shows that n-decane is an acceptable model fuel for modeling kero-sene oxidation if the formation of aromatics is not a major issue. However, more complex model fuels are necessary to model the formation of aromatics from the oxidation of kero- sene. The use of surrogates consisting of binary mixtures of n- decane and toluene or n-propyl benzene showed that the level of aromatics was difficult to simulate in JSR conditions.41,42 A much better agreement between the experimental results and the modeling can be obtained using a mixture of n-decane, n-propylbenzene and n-propylcyclohexane, as presented here. This results from the important reactions of the cycloalkane fraction of the fuel. The detailed kinetic reaction mechanis ms for these pure compounds had first to be established before merging the sub-mechanis ms to yield a kerosene kinetic reac- tion mechanis m.

image.png

Fig.  7    Comparison  between JSR experimental results obtained for the oxidation of kerosene (large symbols), n-decane (s maller symbols and interpolation line) and the modeling using n-decane as model-fuel (s mall symbols and spline line). The initial conditions were: 0. 1% of fuel, residence time = 0.5 s, 10 atm).

The oxidation of n-decane

The oxidation of n-decane was studied in a JSR over a wide range  of  experimental  conditions  (1–40  atm,  500–1400  K, equivalence ratio φ = 0.2 to 2). Most of the data have been reported in the literature.37–39,41,42  The kinetics reaction sub- mechanis m was built based on general scheme: initiation by thermal  decomposition  and  reaction  with  O2 ,  propagation via H-atom abstraction by s mall radicals (see Table 2), radical decomposition, isomerization and reaction with O2 . Fig. 8 pre- sents a comparison of the experimental results obtained for the oxidation of n-decane at 1 atm in fuel-rich conditions. As can be seen from this figure the model is in very good agreement with the data and can be used as a subset of a kerosene detailed kinetic reaction mechanis m. The sensitivity an alyses indicated that besides the reactions of the C0–C1   sub-mechanis m, the reactions of the fuel with H, O, OH and HO2  are sensitive.


The oxidation of simple cycloalkanes

So far, the oxidation of cycloalkanes in the high temperature regime was only studied in JSR conditions.2,20,43  The results of these  studies were used  to propose  a  kinetic  scheme  for the oxidation of cyclohexane and n-propylcyclohexane.

1.    Cyclohexane. A detailed kinetic reaction mechanis m was recently proposed for the oxidation of cyclohexane,20  improv- ing a former mechanis m2  that over-predicted the formation of cyclohexene and  1,3-cyclohexadiene. The initiation reactions for the oxidation of cyclohexane included C–C and C–H bond cleavage. The cyclohexyl (cy-C6H11) chemistry was detailed: The  isomerization  of  cyclohexyl,  yielding  linear   C6H11-16 (5-hexenyl) was not explicitly included previously.2

cy-C6 H11  → C6 H11 -16

This radical isomerizes yielding  1-hexen-3-yl (C6H11-13) and 1-hexen-2-yl (C6H11-12).

C6 H11 -16 → C6 H11 -13

C6 H11 -16 → C6 H11 -12

1-Hexen-2-yl isomerizes yielding 1-hexen-5-yl.

C6 H11 -12 → C6 H11 -15

5-Hexenyl decomposes, yielding 3-butenyl and ethylene,

C6 H11 -16 → 3-C4 H7 + C2 H4 and 1-propyl and allene.

C6 H11 -12 → nC3 H7 + aC3 H4

The decomposition of 1-hexen-5-yl yields allyl and propene; that of 1-hexen-3-yl forms ethyl and  1,3-butadiene and also 1,3-pentadiene and methyl.

C6 H11 -15 → aC3 H5  + C3 H6

C6 H11 -13 → C2 H5 + C4 H6

C6 H11 -13 → C5 H8 -13 + CH3

The kinetics for the above isomerizations and decompositions were estimated by an alogy with similar reactions for which kinetics had already been established. The inclusion of these reactions improved the modeling of cyclohexane avoiding the  over-prediction of cyclohexene and cyclohexadiene at low fuel- conversion. Again, kinetic data are missing for important reac- tions in this submechanis m. This is particularly the case for the reactions of decomposition of the fuel and of its primary radi- cals  produced  by  methatesis.  Fig.  9  presents  a  comparison between the JSR data and the modeling. As can be seen form this figure, the oxidation of cyclohexane in a JSR is well-pre- dicted by the proposed model.


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