PDF(230 KB)
Research articles
Research articles
Numerical study of ignition mechanism of n-heptane
direct injection compression-ignition engine
- Xiaoping GUO1,Zhanjie WANG2,
Author information
+
1.School of Energy and
Power Engineering, Dalian University of Technology, Dalian 116023,
China; 2.School of Electronic
and Information Engineering, Dalian University of Technology, Dalian
116023, China;
Show less
History
+
Published |
05 Dec 2009 |
Issue Date |
05 Dec 2009 |
Abstract
A detailed chemical dynamical mechanism of oxidation of n-heptane was implemented into kiva-3 code to study the ignition mechanism of a high-temperature, high-pressure, three-dimensional-space, transient turbulent, non-homogeneous, mono-component fuel in the engine. By testing the quantity of the heat released by the chemical reaction within the cylinder cell, the elementary reaction showing an obvious increase in the cell temperature was defined as ignition reaction and the corresponding cell as ignition position. The main pathway of the ignition reaction was studied by using the reverse deducing method. The result shows that the ignition in the engine can be divided into low-temperature ignition and high-temperature ignition, both of which follow the same rule in releasing heat, called the impulse heat releasing feature. Low-temperature ignition reaction, whose ignition reaction is c5h9o1-4=ch3cho+c3h5-a, follows the oxidation mechanism, while high-temperature ignition reaction, whose ignition reaction is c2h3o1-2=ch3co, follows the decomposition mechanism. No matter which ignition it is in, the chemical reaction that restrains the ignition reaction from lasting is the deoxidization reaction of alkylperoxy radicals.
Keywords
compression-ignition engine /
ignition mechanism /
elementary reaction /
n-heptane
Cite this article
Download citation ▾
Xiaoping GUO, Zhanjie WANG,.
Numerical study of ignition mechanism of n-heptane
direct injection compression-ignition engine. Front. Energy, 2009, 3(4): 432‒439 https://doi.org/10.1007/s11708-009-0050-9
{{custom_sec.title}}
{{custom_sec.title}}
{{custom_sec.content}}
This is a preview of subscription content, contact
us for subscripton.