Troels Dyhr Pedersen.indd - Solid Mechanics
Troels Dyhr Pedersen.indd - Solid Mechanics
Troels Dyhr Pedersen.indd - Solid Mechanics
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6 The basics of HCCI combustion<br />
- 16 - -<br />
6.1 Combustion principle<br />
The HCCI combustion process concept is based on auto ignition in a lean premixed<br />
fuel/air charge. The combustion event is therefore governed mainly by chemical kinetics,<br />
which clearly separates it from the diffusion combustion in DI CI engines as well as the<br />
flame propagation in SI engines.<br />
The abbreviation HCCI has become a covering term for internal combustion technologies<br />
that utilize lean premixed combustion at low temperatures. The temperature region for<br />
low temperature combustion starts around 1500 K, which is the minimum temperature<br />
required for satisfactory conversion of CO to CO2 in the power stroke. The highest<br />
temperature allowed is usually determined by the amplitude of the engine knock.<br />
Knocking is a high pitched sound caused by large pressure gradients in the combustion<br />
chamber due to very rapid combustion. This limit is reached around 1800-2000 K with<br />
DME as fuel, corresponding to an excess air ratio of approx. 2.5. At this temperature<br />
level the formation of NO is also increasing notably, thereby reducing one of the<br />
important advantages of lean premixed combustion.<br />
6.2 Combustion characteristics<br />
In general, the highly premixed fuel/air charges will burn to completion within a few<br />
milliseconds near TDC. The ideal HCCI combustion process is therefore not much<br />
different from a constant volume explosion due to the very short duration of the<br />
combustion. The term explosion implies that the process is spatially uniform and hence<br />
the pressure rise rate is also uniform. Although an explosion is usually connected with<br />
destructive events, it does not have any damaging effect on the engine as long as the end<br />
pressure is within the design limits of the engine.<br />
With an excess air ratio of 3 or less, the majority of the heat release lies within less than<br />
one millisecond in a well mixed charge. This results in a fast pressure rise rate, typically<br />
above 10 bar per one tenth of a millisecond or higher. At this rate of combustion it is<br />
common that not all of the charge reacts simultaneously, which can be caused by<br />
temperature gradients and uneven fuel distribution in the chamber. As a result, large<br />
pressure gradients are created in the combustion chamber. This causes the air to oscillate<br />
with high amplitude in the chamber. The frequencies of the oscillations are identical to<br />
the resonance frequencies, which may be calculated or determined by computer<br />
simulations. The oscillations are similar to those observed in SI engine knock. HCCI<br />
knock may - like SI engine knock - be harmful to the engine if the load is high enough;<br />
otherwise it may run continuously at knocking conditions without any damaging effects<br />
to the piston or cylinder walls. Knocking does however shorten the life of cylinder<br />
pressure transducers, since the membranes of the transducer are typically loaded beyond<br />
their design specifications when they are impacted by pressure waves.<br />
Part of the energy contained in the pressure waves in knocking combustion is transferred<br />
to the engine and causes the engine exterior surfaces to emit acoustic noise. As higher