gas power cycles 1 (1)

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    MECH 351 PM Wood-Adams Fall 2006

    Classification of Thermodynamic

    Cycles

    We can classify thermodynamic cycles

    according to their desired output:

    the state of the working fluid:

    or whether or not the working fluid is

    replaced in each cycle

    Power cycles vs. refrigeration cycles

    Gas cycles vs. vapor cycles

    Closed cycles vs. open cycles

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    Heat engines

    Internal combustion:

    the heat is supplied tothe working fluid by

    burning the fuel within

    the system boundaries

    e.g. automobile

    engines

    External combustion:

    heat is supplied to theworking fluid from a

    source external to the

    system

    e.g. steam power

    plants

    We can also classify heat engines in terms of

    how the heat is supplied to the working fluid.

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    Analysis of gas cycles

    actual gas power cycles are difficult to

    analyze because of non-idealities such asfriction and non-equilibrium conditions

    We make simplifications and strip thecycle of internal irreversibilities. Then we

    end of with an ideal cycle that closely

    resembles the actual cycle.

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    Simplification of a real process to allowfor analysis

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    Analysis of gas power cycles The working fluid remains a gas through

    out the entire cycle.

    Examples of such cycles: spark-ignitionengines, diesel engines, conventional gas

    turbines. All of these engines are internal

    combustion engines. This means that the

    working fluid undergoes chemicalreactions in the cycle:

    air + fuel combustion gases

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    MECH 351 PM Wood-Adams Fall 2006

    Air standard assumptionsSet of assumptions that we make in the analysis

    of internal combustion engines: the working fluid is air which is an ideal gas

    all processes of the cycle are internally

    reversible the combustion process is replaced by a heat-

    addition process from an external source

    the exhaust process is replaced by a heatrejection process that restores the working fluidto its initial state (i.e. we consider a closed cycle)

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    Reciprocating engines

    top dead center: position

    of piston when it forms

    smallest volume in cylinder

    bottom dead center:position of piston when it

    forms largest volume in

    cylinder

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    MECH 351 PM Wood-Adams Fall 2006

    Volumes

    TDC

    BDC

    min

    max

    VV

    VVr ==

    Compressionratio:

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    Mean effectivepressure

    A fictitious pressurethat, if it acted on

    the piston over the

    entire power stroke,

    would produce the

    same amount of net

    work as the actual

    cycle.

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    MECH 351 PM Wood-Adams Fall 2006

    Classification of reciprocating engines

    Spark ignition (SI): combustion is

    initiated by a spark plug. Ideal cycle is theOtto cycle.

    Compression ignition (CI): air-fuelmixture is self ignited as a result of

    compressing the mixture above its self

    ignition temperature. Ideal cycle is theDiesel cycle.

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    4 stroke spark ignition engine

    Actual

    cycle

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    4 stroke spark ignition engine

    Ideal cycle

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    2 stroke reciprocatingengine

    Same for 4 functionsare executed in just 2

    strokes: the power

    stroke and the

    compression stroke.

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    MECH 351 PM Wood-Adams Fall 2006

    Otto CycleApply the air-standard assumptions to SI engines we

    get the idealized version: the Otto cycle

    Process 1-2: isentropic compression, Process 2-3: constant

    volume heat addition, Process 3-4: isentropic expansion,

    Process 4-1: constant volume heat rejection.

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    MECH 351 PM Wood-Adams Fall 2006

    Analysis of Otto Cycle:

    Ideal gas w/ constant Cv.

    The cycle is

    executed in aclosed system,

    i.e. a cylinder.

    ( )23v

    23in

    TTc

    uuq

    ==

    ( )14v

    14out

    TTcuuq=

    =

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    Thermal efficiency of the Otto cycle

    Constant Cv

    1k

    in

    netotto,th

    r11

    qw

    ==

    How do we derive this?

    compression ratio

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    Isentropic relations for ideal gas

    with constant specific heat

    k

    2

    1

    consts1

    2

    k)1k(

    1

    2

    consts1

    2

    1k

    2

    1

    consts1

    2

    v

    v

    P

    P

    PP

    TT

    vv

    TT

    =

    =

    =

    =

    =

    =v

    p

    C

    Ck=

    These equations are used torelate the properties of the states

    before and after the isentropic

    expansion and compression

    processes.

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    th of the ideal Otto cycle

    k=1.4

    The maximum

    feasible compressionratio is limited by

    engine knock. This is

    when the fuel and air

    mixture is compressedbeyond its autoignition

    temperature and

    premature ignition

    occurs.

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    MECH 351 PM Wood-Adams Fall 2006

    Specific heat ratio and th

    Air at room temperature

    smaller molecule, argon

    larger molecule, ethane

    Working fluid in real engines contains

    larger molecules and it is used at much

    higher temperatures. Both result in lower

    th. A typical value is about 25 to 30%.

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    Analysis of isentropic processes when

    specific heat varies with temperature

    Cannot use the isentropic ideal gas relations

    Instead we use Table A.17 and reduced pressure (Pr)or reduced volume (vr) to relate the properties of thestates before and after an isentropic process.

    We can also use ideal gas law to find temperature

    We find u from Table A.17

    1r

    2r

    ttanconss1

    2

    P

    P

    P

    P == 1r

    2r

    ttanconss1

    2

    v

    v

    v

    v ==

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    MECH 351 PM Wood-Adams Fall 2006

    Example 8-2 An ideal Otto cycle has a compression ratio of 8.

    At the beginning of the compression process, air

    is at 100 kPa and 17C, and 800 kJ/kg of heat istransferred during the heat addition process.

    Accounting for the variation in specific heats with

    temperature, determine (a) the maximum temperature and pressure that

    occur during the cycle,

    (b) the net work output,

    (c) the thermal efficiency and

    (d) the mean effective pressure for the cycle.

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    MECH 351 PM Wood-Adams Fall 2006

    Example 8-2