Thermodynamic Cycles for CI engines In early CI engines the fuel was injected when the piston reached TC and thus combustion lasted well into the expansion.

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Presentation transcript:

Thermodynamic Cycles for CI engines In early CI engines the fuel was injected when the piston reached TC and thus combustion lasted well into the expansion stroke. In modern engines the fuel is injected before TC (about 20 o ) The combustion process in the early CI engines is best approximated by a constant pressure heat addition process  Diesel Cycle The combustion process in the modern CI engines is best approximated by a combination of constant volume & constant pressure  Dual Cycle Fuel injection starts Early CI engineModern CI engine

Modern CI Engine Cycle vs Dual Cycle A I R Combustion Products Fuel injected at 20 o bTC Intake Stroke Air TC BC Compression Stroke Power Stroke Exhaust Stroke Q in Q out Compression Process Const pressure heat addition Process Expansion Process Const volume heat rejection Process Actual Cycle Dual Cycle Q in Const volume heat addition Process

Process 1  2 Isentropic compression Process 2  X Constant volume heat addition Process X  3 Constant pressure heat addition Process 3  4 Isentropic expansion Process 4  1 Constant volume heat rejection Dual Cycle Q in Q out X X

Thermal Efficiency For cold air-standard the above reduces to: where r c = v 3 /v X and  = P 3 /P 2 Note, the Otto cycle (r c =1) and the Diesel cycle (  =1) are special cases:

The use of the Dual cycle requires information about either the fractions of constant volume and constant pressure heat addition (common assumption is to equally split the heat addition), or the maximum pressure P 3. Transformation of r c and  into more natural variables yields For the same inlet conditions P 1, V 1 and the same compression ratio: For the same inlet conditions P 1, V 1 and the same peak pressure (actual design limitation in engines):