Pyrolysis of Furan at Low Pressures
J. Phys. Chem. A, Vol. 102, No. 38, 1998 7481
contribution to the initiation of a radical chain mechanism is
discussed below. It should be noticed that the heat of formation
for the biradical L-furan has not been determined experimentally.
8
Organ and Mackie estimated a value of ∆Hf,298 K ) 297 kJ/
mol for L-furan and a heat of reaction of ∆Hr,298 ) 332 kJ/mol
for the initial dissociation step using group additivity techniques
described in ref 9. This value is in good agreement with the
experimental activation energies at high pressures of 324 or 327
8
kJ/mol obtained in SPST experiments. The overall heats of
reaction for the formation of final products are very well
established. Because of the large variety of products, they
concluded that the pyrolysis must include some contribution
from a chain mechanism, which may be started by reaction 1c
or by the unimolecular dissociation of either of the products
C3H4 and CH2CO.
The SPST studies were performed at total pressures of around
and 20 bar. One would then expect that the unimolecular
26
8
Figure 1. LS profile showing vibrational relaxation in a 2% furan/
krypton mixture at P ) 68 Torr and T ) 1168 K. The dashed line
represents the exponential fit to the final decay.
dissociation rate constant of a molecule the size of furan is close
to the high-pressure limit. Consistent with this, there are no
significant differences in the rate constants from the study at 2
bar and the study at 20 bar. The rate constant of the 2 bar
study of Lifshitz et al. is even a little higher than the data from
the 20 bar study of Organ and Mackie, but within experimental
error they agree with each other.
shock velocity was measured by interpolation of intervals from
five pressure transducers spaced about the observation window
at 120 mm apart. Using thermodynamic properties of the
reactants, the diluent, and the reaction products, postshock
temperatures without relaxation and for fully relaxed conditions
were calculated with an accuracy of (10 K.
6
While the high-pressure limiting rate constant k1,∞ for the
unimolecular furan dissociation seems to be well established,
there is no information regarding falloff behavior or the low-
pressure limiting rate constant. In addition, the temperature
dependence of the branching ratio between the two dominant
molecular channels 1a and 1b is still uncertain. Therefore, time-
resolved kinetic measurements in shock waves combining the
time-of-flight (TOF) and the laser-schlieren (LS) techniques are
indeed helpful to improve the understanding of the pyrolysis
mechanism of furan. The first low-pressure measurements of
the rate constant for the initial rate-determining step (the C-O
bond cleavage) and the real time measurements of major product
formation are presented, giving a new measure of the branching
ratio between the dissociation channels. Additionally, accurate
rates at low pressures will be provided, allowing the observation
of falloff effects in this reaction. Furthermore, the vibrational
relaxation and incubation time measurements represent a unique
opportunity to improve the understanding of collisional energy
transfer and dissociation in polyatomic molecules.
Time-of-Flight. A 2% furan-98% Ne mixture was prepared
from reagents obtained from the following sources: furan from
Aldrich (purity >99%) and research grade neon from Matheson
(99.999%). Furan was introduced into the gas-handling system
by vaporization of the liquid sample, condensed by LN2, and
doubly distilled. The middle fraction was retained for the
mixture. Mass spectrometric analysis of the pure furan and of
the 2% furan/neon mixture revealed an absence of impurities
within the detection limit of TOF, ca. 300 ppm. The following
mixtures, all with neon diluent, were prepared to determine the
mass spectrometric sensitivity factors: 2% C2H2, 2% CO, 2%
allene, 2% propyne, and 2% diketene. The calibration experi-
ments were performed at nonreacting temperatures. For the
diketene mixture, the dissociation of diketene at 1050 K occurred
shortly after shock front arrival; the mass peak due to ketene,
m/e 42, was constant during the observation period. The
sensitivity factors for allene and propyne were found to be
identical.
The temperature and pressure ranges covered by the TOF
experiments are 1300-1700 K and 175-250 Torr. The mass
balance is ∼100%.
Experimental Section
The details of the experimental setup for both shock tubes
including the LS and TOF detection techniques have been
described in previous publications.
10,11
Results and Discussion
Therefore, only relevant
details of the furan dissociation experiments will be mentioned
here.
Vibrational Relaxation. At temperatures below 1200 K and
pressures below 100 Torr, the density gradients in the gas are
solely due to vibrational relaxation. The typical semilog laser-
schlieren profile of Figure 1 shows a markedly slow and
nonexponential time dependence of the density gradient for
mixtures of furan in krypton. The density gradients increase
during the first 2 µs, reach a maximum, and then decrease
exponentially after about 3 µs. In a small temperature range
(503-620 K) and for total pressures around 10 Torr, we were
able to resolve vibrational relaxation in pure furan (Figure 2).
The vibrational relaxation is faster than that in furan/Kr mixtures,
but the nonexponential time dependence of the laser-schlieren
profile remains (see Table 1). Final decay times were extracted
by fitting the exponential decay well after the maximum in the
semilogarithmic plot. These times were corrected to Bethe-
Laser Schlieren. Furan was obtained from Aldrich (purity
>
99%) and was vacuum degassed using the middle fraction
for the experiments. For the experiments in pure furan, the
shock tube was directly filled with the purified vapor. Diluted
mixtures of 5% and 2% furan in Kr were also prepared
manometrically in a 50 L glass bulb with excimer grade krypton
(Spectra gases, >99.997%). The molar refractivity of the gases
was taken as a constant 6.367 for krypton and 18.432 for furan.
To produce the combination of low postshock pressures and
temperatures necessary for vibrational relaxation or incubation
studies, various Laval nozzles were used to slow the shock wave.
These nozzles are made from brass and inserted in the driven
section of the shock tube close to the diaphragm. The incident