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Material Type: Notes; Professor: Dwyer; Class: Combustion Engines; Subject: Engineering Mechanical; University: University of California - Davis; Term: Spring 2008;
Typology: Study notes
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The purpose of this note is to fix the engine geometries for both the spark ignition and compression ignition engines that we will use for the remainder of the course at WOT, Wide Open Throttle. These engines will be the engines to use unless it is specifically stated otherwise in the problem assigned.
Spark Ignition Engine โ BMW 335i Turbo
Bore=88 mm Stroke=89.6 mm Displacement= 2.979 liters Compression Ratio = 10. Four stroke Six cylinder RPM(Max) = 5300 ER = 1.0 Fuel = C8H18 R = r/a = 4. Max Power: 225 kW @ 5800 RPM Max Torque: 306 J @ 5800 RPM
Compression Ignition Engine โ Detroit Diesel M4 โ 12.8L Turbo Heavy Duty Engine at Maximum Power and Torque
Bore = 128 mm Stroke = 166 mm Compression Ratio = 18/ Four stroke Six cylinder RPM(Max) = 2100 ER = .8 Fuel = C12H26 R = r/a = 9 Max Power: 450 hp @ 1900 RPM Max Torque: 1650 ft-lb @ 1200 RPM
In order to calculate finite rate NO we must know the ratio of the connecting arm, r, to the crank arm, a, for a given engine or R given above.
Assume that the SI engine is turbocharged, unless specified, and that the inlet pressure and temperature to the engine are the following: P 1 = 1.5 bar and T 1 = 310 K. The exhaust pressure is assumed to be 1.05 bar. For the diesel engine the inlet temperature and pressure will be given as data.
Note: The fuel/air equivalence ratio (or equivalence ratio - ER) is defined as
actual stoichimetric
In Europe they use the inverse of the fuel/air ratio, and the symbol used is ฮป.
Fuel burning characteristics for both engines
Part I: 20% fuel at constant volume and at TDC
Part II: 80% fuel at constant pressure starting at TDC
Compression Polytropic Coefficient: k = 1.
Expansion Polytropic Coefficient: k = 1.
Percentage of residual gases to intake gases
a. Spark Ignition Engine - 6% b. Compression Ignition Engine - 3%