Consider the effects of exhaust gas recirculation on the
combustion process. Mixing exhaust gas with the fuel-air gas
changes the initial temperature, density, molecular weight and
effective heat of combustion of the charge within an SI
engine.
Consider an SI engine with compression ratio 9 which uses fuel-air
mixture of the equivalence ratio 1.1. The fuel-air mixture enters
the intake manifold at a pressure p1 and temperature 290K. Perform
an analysis of the effect of EGR on an ideal cycle. Assume the
intake and exhaust processes both occur at the same pressure of
1atm.(fuel C3H8)
a) Use a major product model to determine the composition of the
EGR. Note: For the remaining questions, carry out the STANJAN
computations for an EGR mass fraction of 0, 10, 20 and 30%. Assume
that the charge only consists of EGR and fuel-air.
b) Assuming that the recirculated exhaust is at a pressure of 1 bar
and a temperature of 900 K, compute the temperature of the
fuel-air-EGR mixture before it enters the cylinder (State 1).
c) Carry out an adiabatic compression computation to determine the
pressure and temperature at the end of the compression stroke
(State 2).
d) Perform a constant-volume combustion computation to determine
the peak pressure and temperature (State 3). Use full set of
products to determine states 3 and 4.
e) Perform an adiabatic expansion computation to find the final
pressure and temperature at the end of the expansion stroke (State
4).
f) Use the computed energies in states 1 and 4 to find the work per
cycle expressed as IMEP (Indicated Mean Effective Pressure).
g) Show the effect of EGR on the combustion process using the
graphs of your choice
Consider the effects of exhaust gas recirculation on the combustion process. Mixing exhaust gas with the...
Consider the following figure Otto cycle Heating at constant volume (fuel combustion) Он 3) Adiabatic expansion power stroke ed 0 rV Adiabatic compression (compression stroke) Cooling at constant volume (cooling of exhaust gases) (a) For the Otto cycle shown in the figure above, calculate the changes in entropy of the gas in each of the constant-volume processes b 无, and Td and the number of moles n and the heat capacity Cv of the gas. (Use any variable or symbol...
Ignition power stroke adiabatic expansion compression stroke adiabatic compression Pressure 4. (25 pts) in an internal combustion engine, the compression ratio (c), or the ratio volumes in an expansion or compression step, is an important for calculating efficiency. An Otto Engine cycle consists of (see diagram to right): an adiabatic compression step (1-2), a constant volume heating step (2-3). an adiabatic expansion step (3-4), and a constant volume cooling step (4-1). Based on this information, show: a. V3/V4 = V2/...
Α 4-stroke spark-ignition engine has a compression ratio of 10 and operates on the ideal constant volume cycle with intake pressure of 50 kPa (throttled) and intake temperature of 300 K. The exhaust pressure is 100 kPa. The heat input from combustion is 2500 kJ/kg and γ = 1.3 for the working fluid. a. Draw the p-V diagram of the full cycle and indicate all the processes. b. Calculate the residual gas fraction and the temperature decrease during the exhaust...
Question 1 (based on the example to the example we worked in class) (30 points) Consider an Air Standard Otto Cycle in which an engine cylinder has 2x10 kg of fuel with a heat of combustion of 45,000 kJ/kg. The volume at top dead center (i.e., the clearance volume) is 0.055x103 m3, and the volume at bottom dead center is 0.555x 103 m2. The air fuel ratio is 14:1 and the mixture temperature at start of compression is 300 K....
Methane (CH4) is burned with 110.9 % of theoretical air. The mixture enters the combustion chamber at 25°C. 1) Find the Air/Fuel ratio for this mixture: AF = (+ 0.03) 2) Find the adiabatic flame temperature for the mixture. Tadiabitic flame = OC (+ 20°C) 3) Find the mole fraction of the N2 in the exhaust. YN2 =
. A 4 stroke 4 cylinder spark ignition engine runs on a stoichiometric mixture of ethanol and air at wide open throttle. The 1 liter engine has a compression ratio of 9:1 and operates at 5000 rpm. The intake manifold conditions are standard pressure and temperature, no residual gas in engine combustion chamber. Using k-1.35 for all calculations the a. Calculate the indicated work done by the engine, in joules per cycle b. Calculate the indicated thermal efficiency c. Calculate...
An Otto engine is operating with natural gas which can be approximated as an ideal gas. Assuming the engine is at standard condition (25°C, 1 atm) before the compression process. Also, temperature of the Otto cycle after the combustion process is 1500 K. (a) Assuming compression ratio of the Otto engine as 8, 9 and 10, determine the corresponding temperatures of the natural gas-air mixture (natural gas with 100% excess air) after the compression. (b) Determine the thermal energy release...
A compression ignition engine is being analyzed. The residual gas fraction is xr=0.02. The fuel-to-air equivalence ratio is f=0.6. At the end of the compression stroke the temperature is T2=1300 K and specific volume is v2=0.19 m3/kg-air. The maximum cycle pressure is P3=4000 kPa. At the end of the power stroke the specific volume is 1.00 m3/kg-air. Calculate the temperature at the end of the combustion process, T3b, and calculate the work done [kJ/kg-air] during the power stroke.
2. Analyze an Audi 3.0-liter TDI V6 Biturbo diesel engine using an air-standard Diesel cycle that addresses the "real" effects of non-isentropic compression/expansion, air-fuel ratio, fuel heating value, incomplete combustion, exhaust residual, and heat loss. The engine is four-stroke, has six cylinders with a compression ratio of 16.0, and develops maximum power at 4250 rpm. Assume the following: the diesel fuel heating value is Quv 42,600 kJ/kg, the air-to-fuel ratio (AF) at maximum power is 25, and the combustion efficiency...
INTERNAL COMBUSTION ENGINES Practice Problems ME 436 A 3 cylinder, 2.7 liter SI engine operates on a 4 stroke cycle at 3300 RPM with a compression ratio of 8.6:1. At the start of the compression stroke, the temperature is 47°C and the pressure is 82kPa. Assume 3% residual gases. The mechanical efficiency is 81%, combustion efficiency is 96%, and the air-fuel ratio is 16.3, and the fuel heating value is 43,000 kJ/kg. The combustion process starts at TDC and is...