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α  =  8.3 × 10 −18 × exp  (+22750 / T) × [M] −1 (4)
As the temperature increases, Ï„ becomes smaller and also decreases with increasing total con-
centration [M] or, equivalently, with increasing pressure at constant temperature. This also
means that, as pressure increases, the critical temperature for ignition decreases gradually.
Usually, the autoignition occurs at temperature between 1050 and 1100 K. The consistency
of this temperature is a recognized feature of HCCI combustion. Not surprisingly, this tem-
perature is comparable to the ignition temperature that is observed during engine knock in
SI engines [25].
4. Comparison of combustion characteristic between test fuels in HCCI
engine
This section will compare the combustion characteristics of the test fuels in HCCI engine. As
discussed in conjunction with Figure 3, each respective test fuel shows different autoignition
delay times even for the same initial condition due to its fuel autoignition reactivity. Because
of this, we should expect quiet different combustion phasing for each fuel depending on the
resistance to autoignition under the constant initial condition. The combustion phasing is a
critical parameter impacting the thermal efficiency of HCCI engine. If the combustion is too
advanced, knocking combustion occurs easily, thus quickly increasing to the risk for engine
damage and NOx emissions. On the other hand, excessive combustion-phasing retard leads
to unacceptable coefficient of variation (COV) of HCCI combustion with partial-burn and/
or misfire cycles. To facilitate comparison of the combustion characteristics in HCCI engine,
the initial temperature is adjusted in the numerical simulation to set the 50% burn point
(CA50) at 0degATDC (i.e. TDC). Effectively, the reported combustion phasing refers to
CA50 for the main combustion event, starting at the crank angle of minimum heat-release
rate between LTHR and HTHR. Presenting the data referring to the main combustion event
alone is considered more relevant from the standpoint of quantifying the onset of the main
combustion event.
With the effects of fuel autoignition reactivity isolated, Figure 6 compares (a) in-cylinder
temperature, (b) heat-release rate, (c) magnified view of heat-release rate and (d) accu-
mulated heat release for the test fuels. The required initial temperature (To) to maintain
CA50 = 0degATDC is 559.5, 301.5, 464.d and 350.5 K for methane, DME, iso-octane and
n-heptane, respectively. If the fuel has high resistance to autoignition (i.e. methane and iso-
octane), high in-cylinder charge temperature is required during the compression stroke in
order to ensure autoignition. As can be seen, methane and iso-octane both require relatively
high To, which typically has a negative influence on the peak load that can be obtained. This
happens because these two fuels exhibit single-stage ignition at this calculation condition.
For a given initial pressure (Po), higher To causes high peak combustion temperature, as
shown in Figure 6a, so excessive NOx can become the load-limiting factor. Furthermore, as
Figure 6b shows, the increase of peak combustion temperature contributes to the increase
Advanced Chemical
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book Advanced Chemical Kinetics"
Advanced Chemical Kinetics
- Title
- Advanced Chemical Kinetics
- Author
- Muhammad Akhyar Farrukh
- Editor
- InTech
- Location
- Rijeka
- Date
- 2018
- Language
- English
- License
- CC BY 4.0
- ISBN
- 978-953-51-3816-7
- Size
- 18.0 x 26.0 cm
- Pages
- 226
- Keywords
- Engineering and Technology, Chemistry, Physical Chemistry, Chemical Kinetics
- Categories
- Naturwissenschaften Chemie