Project

Predicting the emission characteristics of W and OMEGA type piston in CAT 3410 Engine

AIM: To understand the emission characterization of CAT 3410 engine.

PROCEDURE:

A Diesel Engine is a fuel injection engine where the fuel is directly injected into the combustion chamber when the air is compressed so that the fuel ignites as soon as it comes in contact with high temperature air whic was previously compressed. Since we are just performing the compression and power stroke we are going with sector simulation since we do not deal with any incomming or outgoing fluids.

Here we are provided with the bowl profiles of two different types of pistons namely W-type and Omega-type. Both the pistons have to built using the bowl profile and a sector have to modelled by taking the sector angle of 45 deg, which is specified from boundary.in file.

A W-type sector

Bore: 0.13716 m

Stroke: 0.1651 m

Connecting rod: 0.263 m

Compression ratio: 17.5

An Omega-type sector

Bore: 0.13716 m

Stroke: 0.1651 m

Connecting rod: 0.263 m

Compression ratio: 17.5

The input file are provided prior which have to be imported for case setup process

Case setup:

1. Application type - Crank angle bsed IC engine application.

2. Materials:

Gas Simulation -

Parcel simulation -

Global transport parameters - default

Reaction mechanism -

Species -

Parcel - DIESEL 2

Internal passive - HIROY_SOOT, NOX

3. Simulation Parameters:

Run parameters - solver: Transient - Simulation mode: Full hydrodynamaic.

Simulation time parameters -

Start time: -147 deg

End time: 135 deg

Initial time step: 5e-7 s

Min timme step: 1e-8 s

Max time step: 2.5e-5 s

Solver parameters - default

4. Boundary Conditions

Piston - type: wall - region: Incylinder region

Velocity - motion type: translating - surface movement: moving - Piston motion check.

Temperature - law of wall - 553K

Front face - type: Periodic - region: IN cylinder region

Periodic type: stationary - periodic shape: Rotational - Angle 45 deg.

Back face - type Periodic - region: In cylinder region

Periodic type: Matched Boundary

Matching Boundary: Front face

Cylinder wall - type:wall - region: in cylinder region

Velocity - motion type: translating - surface movement: Fixed

Temperature - law of wall - 433K

Cylinder head - type:wall - region: in cylinder region

Velocity - motion type: translating - surface movement: Fixed

Temperature - law of wall - 523K

5. Initial Conditions and Events

Regions and initializations -

In cylinder region -

Temperature: 355 K

Pressure: 197000 Pa

Species: CO2(0.0014304), H2O(0.0006296), N2(0.76765), O2(0.23029).

Passive: HIROY_SOOT(0), NOX(0).

6. Physical Models:

Spray modeling -

General - Turbulent dispersion: O'Rourke model

Use evaporation model - species: C7H16

Injectors - add an injector and click on edit

Injected species - Diesel 2

Models - Kelvin-Helmholtz model, Rayleigh-Taylor model, Discharge coefficient model.

Time/temp/tke/eps/mass/size - Injection temporial type: cyclic

cyclic period: 720 deg

start of injection: -9 deg

Injection duration: 21 deg

Mass: 2.70167e-5kg

Nozzles - create a nozzle

Radial position: 0.00097 m

Axial position: 0m

Tilt angle in xz plane 62.5 deg.

Spray Modelling is used for fuel injection into the chamber in the case if diesel engine. A spray model is a combination of Eulerian and Lagrangian type, where initially it is eulerian flow and later it gets converted into parcels which are fuel parcels where we use lagrangian approach. We use a solid cone spray method for our case.

Combustion modeling - model: SAGE

General: Fuel - C7H16

Temporal output - sequential

stary time - -10 deg

end time - 135 deg

SAGE is a most commonly and highly powerful chemistry solver for IC engine applications.

Emissions modeling -

Therml NOx model - equilibrium assumption

Hiroyasu-NSC soot model -

Turbulence modeling - RNG k-e

7. Grid Control:

Base grid - 0.004m

Adaptive Mesh Refinement - Active region: In cylinder region

Velocity - SGC: 2m/s if parcel count exceeds 50.

Temp - SGC: 5k with start of -12 deg and end at 180 deg.

Fixed embedding -

1. type - nozzle

mode: sequential

scale: 2

start time: -12 deg

end time 15 deg

ID: injector 0

radius 1: 0.001m - radius 2: 0.003

length: 0.01m

2. type - Boundary

ID: Piston

mode: sequential

scale: 1

start time: -20 deg

end time: 180 deg

3. type - Boundary

ID: cylinder head

mode: sequential

scale: 1

start time: -20 deg

end time: 180 deg

end of case setup

RESULTS:

Mesh:

W_type link: https://youtu.be/JrSWezo46jI

Omega_type link: https://youtu.be/sMcK16r_OHE

Cell count:

Here we can see that omega piston has a rapid rise in cell count which depicts that the AMR which we have used made the cell count to rise due to high change in velocity and temperature values with time. At the end of the cycle we observe that W type piston setup has more enumber of cells.

Pressure:

The pressure plot provides us with the information that the W type piston has high pressure which means the volume that is compressed is higher than in the case of omega type which is increasing the pressure with combustion.

W_type link: https://youtu.be/ZycD0ZBHW5I

Omega_type link: https://youtu.be/i3AmF5ezwfw

Temperature:

The temperature reached by the Omega type is higher which means the combustion is also higher but we cannot say that W type is properly cumbusting the fuel properly. There can also be a case where the Omega is unnecessarily producing high temperature which is nit required which can damage piston as well.

W_type link: https://youtu.be/5r4UV8t1oU0

Omega_type link: https://youtu.be/JJv18xhYtiI

Heat release:

The rate heat release is way fast in the case of Omega while the W type is rising slowly and at a steady state.

NOx

This clearly says the reason behind low NOx in W type which concludes that their is an improper combustion which might be due to the fuel impingment on the piston surface which is reducing the atomization of the fuel.

W_type link: https://youtu.be/nNoqtoH9jDI

Omega_type link: https://youtu.be/xjsAhxVGaR8

soot

The higher amount of soot in W type is also because of improper combustion and irregular atomization which is due to the fuel spray on the piston surfave.

W_type link: https://youtu.be/TnbhFQnflxg

Omega_type link: https://youtu.be/nAW_C5kRUOM

Unburnt hydro carbons

The same concept of fuel residual due to irregular atomization states that fuel is not properly burnt in W type leading to higher unburnt hydro carbons.

W_type link: https://youtu.be/archWtv1YP0

Omega_type link: https://youtu.be/jHiTBLDXi9o

Carbon monoxide

W_type link: https://youtu.be/vANw-XEQ1Ug

Omega_type link: https://youtu.be/WH0RuKIh2GU

Mass

PV diagram

Performace parameters like power and torque can be calculated from engine performace parameters.

W_Type

Work = 3028.53 Nm

Time Duration = 270.156 deg

Time in sec = 270.156 * (60/(360*1600)) = 0.028141 sec/deg

Power = work/time

=> Power = 107619.84 W

Power = 2*pi*N*T/60

=> Torque = Power*60/(2*pi*N)

=> Torque = 642.634 Nm

Omega Type:

Work = 3409.28 Nm

Time duration = 270.171 deg

Time in sec = 0.02814281 s

Power = Work/Time

=> Power = 121142.131 W

Power = 2*pi*N*T/60

=> Torque = Power*60/(2*pi*N)

=> Torque = 723.38 Nm

From the above calculation we can see that the power and torque for the omega type is higher.

CONCLUSION:

From the above simulation we can clearly conclude that omega piston is highly relaiable due to less emission and high performance when compared to W type piston. The main drawback of the W piston is that the fuel is directly injected onto the piston surface which is reducing the atomization due to incorrect injector angle. The angle of spray has to be change inbetween 55 and 65 which can reduce the pollutants atleast.

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