Lecture Notes on Typical Engine Characteristics and Geometrics | EME 163, Study notes of Thermodynamics

Material Type: Notes; Professor: Dwyer; Class: Combustion Engines; Subject: Engineering Mechanical; University: University of California - Davis; Term: Spring 2008;

Typology: Study notes

Pre 2010

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ME 163 IC Engines
Spring 2008 Instructor โ€“ Professor Harry A. Dwyer
Typical Engine Characteristics and Geometries
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 = 10.2
Four stroke Six cylinder RPM(Max) = 5300
ER = 1.0 Fuel = C8H18 R = r/a = 4.5
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 = 18/1
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: P1 = 1.5 bar
and T1 = 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.
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ME 163 IC Engines

Spring 2008 Instructor โ€“ Professor Harry A. Dwyer

Typical Engine Characteristics and Geometries

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

mass of fuel mass of air

mass of fuel mass of air

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%