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Decomposition Analysis of an Automotive Powertrain Design ...

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Engine Model<br />

The engine model is based on the model <strong>of</strong> Kuzak et al. (1984) but accounts for m<strong>an</strong>ifold<br />

tuning effects slightly differently. We use the friction model <strong>of</strong> Patton et al. (1989), include a<br />

simple NOx model, <strong>an</strong>d account for effects <strong>of</strong> combustion stability degradation with burn duration.<br />

The expression for torque is developed in terms <strong>of</strong> me<strong>an</strong> effective pressure, which is<br />

torque normalized against swept displacement volume. The expression for engine torque is<br />

T e = 7.955 x 10 -6 P bmep b 2 s π /4 n c (40)<br />

where P bmep has units <strong>of</strong> bars. The brake me<strong>an</strong> effective pressure, P bmep , is the difference<br />

between indicated me<strong>an</strong> effective pressure <strong>an</strong>d friction me<strong>an</strong> effective pressure<br />

P bmep = P imep - P fmep (41)<br />

The indicated me<strong>an</strong> effective pressure is the amount <strong>of</strong> fuel energy converted to indicated work<br />

normalized against displacement volume. It is given by the product <strong>of</strong> the mass <strong>of</strong> fuel, the lower<br />

heating value <strong>of</strong> the fuel, Q, the thermal efficiency <strong>of</strong> the engine cycle, η t , <strong>an</strong>d the air-to-fuel<br />

ratio, R af ,<br />

P imep = 3.479 x10 -2 η t ( p it / T m ) Q/ R af . (42)<br />

The thermal efficiency is expressed as<br />

η t = 0.9 ( 1 - c r (-0.33 - .01 Regr/30) )f c - S v (1500/N e ) 0.5 (4.137/P imep ) 0.2 (43)<br />

where<br />

f c = (1.18 - 0.18 φ /0.8) φ ≤ 1<br />

= (1.655 - 0.7 φ) φ > 1 (44)<br />

S v = 0.83 (12s + (c r - 1)( 6b + 4s) ) / (b s (2 + c r )). (45)<br />

The 0.9 multiplier accounts for losses due to finite combustion times <strong>an</strong>d is considered valid for<br />

displacements <strong>of</strong> 400 - 600 cc/cylinder <strong>an</strong>d bore to stroke ratios <strong>of</strong> 0.8 - 1.2. The air-fuel<br />

correction factor, f c , is based on the well-known effects <strong>of</strong> air-fuel ratio on idealized Otto cycles<br />

(Taylor, 1985). Heat tr<strong>an</strong>sfer is strongly dependent upon surface-to-volume ratio. The S v term is

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