combustion chamr design

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    Combustion Chamber Design

    Bradford Grimmel

    Nicholas ToroIan Fulton

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    Topics

    Combustion Chamber

    Defined

    Design Considerations Chamber Shapes

    Fast Combustion

    Volumetric Efficiency Heat Transfer

    Low Octane

    Requirement

    Knock Flow Inside A

    Cylinder

    Turbulence

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    Combustion Chamber Defined

    The combustion chamber consists of an

    upper and lower half.

    Upper half- Made up of cylinder head andcylinder wall.

    Lower half- Made up of piston head (Crown)

    and piston rings.

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    Design Considerations

    Minimal flame travel

    The exhaust valve and spark plug should be

    close together

    Sufficient turbulence

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    Design Considerations

    A fast combustion, low variability

    High volumetric efficiency at WOT

    Minimum heat loss to combustion walls

    Low fuel octane requirement

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    Chamber Shapes

    A basic shapes

    Wedge - Hemispherical

    Crescent - Bowl in Piston

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    Chamber Shapes

    Wedge

    Asymmetric design

    Valves at an angle andoff center

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    Chamber Shapes

    Hemispherical

    (Hemi) Symmetric design

    Valves placed on a arc

    shaped head

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    Chamber Shapes

    Bowl-in-Piston Symmetric design

    Valves are placedperpendicular to head

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    Chamber Shapes

    Crescent (Pent-Roof)

    The valves are placed

    at an angle on flatsurfaces of the head

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    Fast Combustion Effect of spark plug location

    Side plug w/o swirl

    Side plug with

    normal swirl

    Side plug with

    high swirl

    Central plug w/o

    swirl

    Two plugs w/o swirl

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    Fast Combustion

    in Relation to Shape

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    Fast Combustion

    in Relation to Shape

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    Comparison of Burn Angles

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    Volumetric Efficiency

    Size of valve heads should be as large as

    possible

    Want swirl produced

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    Heat Transfer

    Want minimum heat transfer to combustion

    chamber walls

    Open and hemispherical have least heattransfer

    Bowl-in-piston has high heat transfer

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    Low Octane

    Octane Requirement related to knock

    Close chambers (bowl-in-piston) have

    higher knock at high compression ratiosthan Open chambers (hemispherical and

    pent-roof)

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    Octane Rating

    Research Octane Number (RON)

    Motor Octane Number (MON)

    Octane is one factor in the combustion process

    that another group will speak about

    Straight chain C-H bonds such as heptane have

    weaker C-H bonds than branched chained C-H

    bonds in branch chained HC such as iso-octane Straight bonds are easier to break

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    Chemical Compositions

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    Knock

    Surface ignition

    Caused by mixture igniting as a result of

    contact with a hot surface, such as an exhaustvalve

    Self-Ignition

    Occurs when temperature and pressure ofunburned gas are high enough to cause

    spontaneous ignition

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    Flow

    2 types of flow

    Laminar flow

    Minimal microscopic mixing of adjacent layers

    Turbulent flow

    Characterized as a random motion in three-

    dimensions with vortices (eddies) of varying size

    superimposed on one another and randomly

    distributed in the flow

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    Why Turbulence?

    Decrease burn time

    Reduces knock

    Reduces emissions (NOx

    )

    Allows for leaner mixture (stratified charge)

    Reduces emissions (HC)

    Decreases in combustion temperature

    Reduces knock Reduces emissions (CO)

    Reduces power

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    Inducing Turbulence

    Valve configuration

    and valve timing

    Turbulence generation

    pot

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    Characterizing Turbulence

    Eddies are defined by length scales

    The Integral Scale lI measures the largest

    eddies of the flow field

    The Kolmogorov scale lkmeasures the

    smallest eddies

    The Taylor microscale lm relates fluctuating

    strain rate of flow field to intensity

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    Characterizing Turbulence

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    Characterizing Turbulence

    Swirl

    Axis of rotation is

    parallel to cylinder

    Generate swirl about

    valve axis (inside port)

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    Swirl

    Impulse Swirl Meter

    Honeycomb flow straightener measures totaltorque exerted by swirling flow.

    A swirling ratio is defined:

    Rs=s/2N

    This ratio is the angular velocity, s, of a solid-

    body rotating flow (equal to angular momentum ofactual flow) divided by the crankshaft angularrotational speed

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    Swirl

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    Characterizing Turbulence

    Tumble

    Axis of rotation is

    perpendicular to

    cylinder axis

    Associated with swirl

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    Characterizing Turbulence

    Rt is the tumble ratio,

    Rt=t/2N

    This ratio compares the angular velocity,

    t, of the solid-body rotation with same

    angular momentum as actual velocity

    distribution in tumble to angular velocity of

    the crankshaft (N)

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    Squish

    Radially inward gas

    motion that occurs

    toward end ofcompression stroke

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    Conclusion

    Optimum chamber

    Central spark plug location

    Minimum heat transfer

    Low octane requirement

    High turbulence