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    DEFINITIONDEFINITION

    Natural Gas is a naturally occurring gaseous mixtureNatural Gas is a naturally occurring gaseous mixture

    of hydrocarbon and non hydrocarbon gases found inof hydrocarbon and non hydrocarbon gases found in

    underground rock reservoirs either on its own as freeunderground rock reservoirs either on its own as free

    gas or in association with crude oil.gas or in association with crude oil.

    ** Hydrocarbon Components: CHydrocarbon Components: C11 C C77++

    ** Non Hydrocarbon ComponentsNon Hydrocarbon Components

    - Nitrogen (N- Nitrogen (N22))

    - Hydrogen Sulphide (H- Hydrogen Sulphide (H22S)S)

    - Carbon Dioxide (Co2)- Carbon Dioxide (Co2)

    - Water Vapour (H- Water Vapour (H220)0)

    o

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    TYPES OF NATURAL GAS DEPOSITTYPES OF NATURAL GAS DEPOSIT

    Associated GasAssociated Gas: Gas Co-exists in reservoir with Crude Oil.: Gas Co-exists in reservoir with Crude Oil.

    Non-Associated GasNon-Associated Gas: Gas exists without oil in the Reservoir.: Gas exists without oil in the Reservoir. Gas Condensates:Gas Condensates: Gases exists in gaseous form in the reservoir but liquefy onGases exists in gaseous form in the reservoir but liquefy on

    production due to reduction in pressure. Gas condensates are of higher qualityproduction due to reduction in pressure. Gas condensates are of higher quality

    and are therefore of more economic value.and are therefore of more economic value.

    Gases containing HGases containing H22S and CoS and Co22 are called acid gases because they form acids orare called acid gases because they form acids or

    acidic solution in the presence of water.acidic solution in the presence of water.

    A gas is called sour if it contains HA gas is called sour if it contains H22S in amounts above 4ppmS in amounts above 4ppm

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    Methane CH4 LNG

    Ethane C2H6

    Propane C3H8

    Butanes C4H10

    Pentanes and Heavier C5H12

    Non-Hydrocarbons

    NGLLPG

    NG

    LPG: Liquefied Petroleum Gas

    NGL: Natural Gas Liquids

    LNG: Liquefied Natural Gas

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    GAS PRODUCTION SCHEMATICGAS PRODUCTION SCHEMATIC

    Market

    Pipeline

    Compression

    Processing

    Production Tubing

    Inflow PerformanceReservoir

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    USES OF NATURAL GASUSES OF NATURAL GAS

    Current Use of Natural Gas and Future Options

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    PROPERTIES OF NATURAL GASPROPERTIES OF NATURAL GAS- Ideal Gases : the Ideal Gas LawIdeal Gases : the Ideal Gas Law

    PV = nRTPV = nRT

    Where:Where:

    P = Absolute Pressure (psia)P = Absolute Pressure (psia)

    V = Volume (ftV = Volume (ft33))

    n = No. of Moles of gasn = No. of Moles of gas

    R = Universal Gas ConstantR = Universal Gas Constant

    T = Absolute Temperature (T = Absolute Temperature (00

    R)R)If M = Mass of gas (Ib)If M = Mass of gas (Ib)

    And M = Molecular wt of the gas (Ibm/Ib-mol)And M = Molecular wt of the gas (Ibm/Ib-mol)

    M

    mn =

    M

    mn =

    RTMmPv =

    RTV

    mPM = = pRT

    gastheofdensity

    RT

    PMP ==

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    Gas Gravity (yGas Gravity (ygg): the specific gravity of a gas is defined as the ratio of): the specific gravity of a gas is defined as the ratio of

    the density of the gas to the density of dry air, at stp.the density of the gas to the density of dry air, at stp.

    29

    gg

    g

    M

    pair

    p

    y ==

    Apparent molecular weight: a gas mixture behaves as if were a

    pure gas with a definite molecular weight. This molecular weight isknown as an apparent molecular weight. It is defined as

    Where

    Ma = Apparent Molecular weight of Mixture

    yi = Mole fraction of component

    Mi = Molecular weight of component i

    Ma = yiMi

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    REAL GASESREAL GASES

    The assumption for ideal gas law do not hold for gases at pressures andThe assumption for ideal gas law do not hold for gases at pressures and

    temperatures that deviate from the ideal or standard conditions must be madetemperatures that deviate from the ideal or standard conditions must be made

    to account for the deviation from ideal behaviour.to account for the deviation from ideal behaviour.

    The most widely used correction method is the gas compressibility factor orThe most widely used correction method is the gas compressibility factor or

    the gas deviation factor or the Z-factor.the gas deviation factor or the Z-factor.

    Videal

    VactualZ=

    Z

    VactualVideal=

    For a certain quantity of gas, we write

    22

    22

    11

    11

    TZ

    VP

    TV

    VP

    =

    Where: Z1 = Gas deviation factor at condition 1

    Z2

    = Gas deviation factor at condition 2

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    Density of Real GasDensity of Real Gas

    RTM

    MZPV =

    ZRT

    PMP=

    At standard conditions (P = 14.73psia, T = 520R)

    ZT

    PyP

    g7.2=

    THE THEOREM OF CORRESPONDING STATES

    Reduced Temperature

    Reduced Pressure

    Reduced Volume

    Tc

    TTr=

    Pc

    P=Pr

    Vc

    VVr=

    Where:

    T = actual temperatureP = actual pressureV = critical temperatureTc = critical temperaturePc = critical pressure

    Vc = critical volume

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    DETERMINATION OF Z - FACTORDETERMINATION OF Z - FACTOR

    Using Standing and Kate CorrelationUsing Standing and Kate Correlation

    If Gas composition is givenIf Gas composition is given- Pseudo critical pressure: PPseudo critical pressure: Ppcpc == yy iiPPcici- Pseudo critical temperature: TPseudo critical temperature: Tpcpc == yy iiTTcici If Gas composition is not given but gas gravity is given:If Gas composition is not given but gas gravity is given:

    PPpcpc = 709.604 58.718y= 709.604 58.718ygg

    TTpcpc = 170.491 + 307.344 y= 170.491 + 307.344 ygg

    For a gaseous mixtureFor a gaseous mixture

    pc

    rp T

    TT =

    pcrp P

    PP =

    The interception of pseudo reduced pressure and pseudo reducedThe interception of pseudo reduced pressure and pseudo reduced

    temperature on standing and Katz chart gives the z factortemperature on standing and Katz chart gives the z factor

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    GAS FORMATION VOLUME FACTOR (BGAS FORMATION VOLUME FACTOR (Bg)g)

    Where:Where: V = volume at reservoir conditionV = volume at reservoir condition

    Vsc = volume at standard conditionVsc = volume at standard condition

    From the equation of stateFrom the equation of state

    sc

    g

    V

    VB =

    ( )VolStd

    vol

    PTZ

    PZT

    nRTZ

    Px

    P

    ZnRTB

    scsc

    sc

    scsc

    scg

    .=

    =

    At standard conditions: PAt standard conditions: Pscsc = 14.7psia and T= 14.7psia and Tscsc =520=52000R, ZR, Zscsc = 1= 1

    scfftP

    ZTBg /0283.0

    3=

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    VISCOSITY OF NATURAL GASVISCOSITY OF NATURAL GAS

    This is defined as a measure of resistance to flow exerted by the gas. The unit of viscosity is the centipaise.This is defined as a measure of resistance to flow exerted by the gas. The unit of viscosity is the centipaise.

    There are two ways of estimating viscosityThere are two ways of estimating viscosity Laboratory methodLaboratory method CorrelationsCorrelations

    By Lab MethodBy Lab MethodIf analysis of the gas mixture is known and the viscosities of the components are known, thenIf analysis of the gas mixture is known and the viscosities of the components are known, then

    ( )( )

    =ii

    ii

    My

    Myi

    2

    2

    By Correlations

    ( ) ( )rrTPfandTMf ==

    12 ,

    (a) Compute AMW of the gas yiMi

    (b) Determine the of the gas mixture at 1 atmosphere using chart. If the pressure of

    the mixture is above 1 atm then

    3. Calculate pseudo critical temperature/pressure

    4. Calculate reduced temperature/pressure

    5. Determine the viscosity ratio ( g/ gi ) from chart

    6. Calculate g

    7. If the gas contains non-HC components, then the should be corrected using chart.

    ig

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    ESTIMATION OF GAS RESERVESESTIMATION OF GAS RESERVES

    Three methods are availableThree methods are available

    1.1.Volumetric MethodVolumetric Method

    2.2.Material Balance MethodMaterial Balance Method3.3.Pressure Decline MethodPressure Decline Method

    Volumetric MethodVolumetric Method

    This is applied in a new field for rough estimates. No production history isThis is applied in a new field for rough estimates. No production history is

    required. We need only geological data like porosity, water saturation etc.required. We need only geological data like porosity, water saturation etc.

    ( )gi

    wi

    B

    SAhG 143560

    Where: A = Area of the reservoir (Acres)

    h = Formation thickness (ft)

    = PorositySwi = Water Saturation

    Bgi = Initial gas formation vol factor

    G = Gas initial in plae

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    Gas produced at any given condition (Gp) isGas produced at any given condition (Gp) is

    ( )

    =

    ggi

    wipBB

    SAhG11

    143560

    Recovery FactorRecovery Factor

    g

    gip

    gB

    B

    G

    GE == 1

    MATERIAL BALANCE METHODMATERIAL BALANCE METHOD

    This is used for reservoir that has produced long enough.This is used for reservoir that has produced long enough.

    There are two cases:There are two cases:

    - Without water production/influxWithout water production/influx

    - With water production/influxWith water production/influx

    Without water production/influxWithout water production/influx

    ( )g

    gig

    pB

    BBGG =

    With water production/influxWith water production/influx

    ( )

    g

    wpe

    g

    gig

    pB

    BWW

    B

    BBGG

    +

    =

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    PRESSURE DECLINE METHODPRESSURE DECLINE METHOD

    i

    i

    ibb

    pb

    Z

    P

    VTZ

    TGP

    Z

    P+=

    COMPRESSION OF NATURAL GASCOMPRESSION OF NATURAL GAS

    Add energy to the gasAdd energy to the gas

    TYPES

    (1)Positive Displacement Compressors

    - Reciprocating Compressors

    - Rotary Blowers

    (2)Continuous flow compressors- Centrifugal Compressors

    - Ejectors

    Reciprocating compressors are the most commonly used in

    gas industry

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    COMPONENTSCOMPONENTS

    - PistonPiston

    - CylinderCylinder

    - Suction/Discharge ValvesSuction/Discharge Valves

    - Connecting RodConnecting Rod

    - ImpellerImpeller

    - ShaftShaft

    - DiffuserDiffuser- VoluteVolute

    COMPRESSION CYCLECOMPRESSION CYCLE

    - Ideal CycleIdeal Cycle- Actual CycleActual Cycle

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    MULTISTAGE COMPRESSOR ARRANGEMENTMULTISTAGE COMPRESSOR ARRANGEMENT

    Compressor Ratio r =Compressor Ratio r =s

    d

    PP

    1 2 3Ps Pd

    For design purposesFor design purposes r < 6r < 6

    For practical purposesFor practical purposes rr 44

    - Optimum Number of stages is given by- Optimum Number of stages is given by

    n

    s

    d

    PP

    r

    1

    =

    Where:Where:

    Pd = discharge pressure (psia)Pd = discharge pressure (psia)

    Ps = suction pressure (psia)Ps = suction pressure (psia)

    n = No of stages requiredn = No of stages required

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    COMPRSSOR DESIGNCOMPRSSOR DESIGN

    This involvesThis involves

    1.1. The determination of compressor capacityThe determination of compressor capacity

    2.2. The determination of power requirementsThe determination of power requirements

    -- Determination of compressor capacityDetermination of compressor capacity

    4

    2

    vLSEdq

    =WhereWhere

    q = Flow capacity (scfd)q = Flow capacity (scfd)

    d = Piston diameter (ft)d = Piston diameter (ft)

    L = Stroke length (ft)L = Stroke length (ft)

    S = Compressor speed (rpm)S = Compressor speed (rpm)

    Ev = Volumetric efficiencyEv = Volumetric efficiency

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    The volumetric efficiency is calculated fromThe volumetric efficiency is calculated from

    ZZ11 = gas derivation factor at suction condition= gas derivation factor at suction condition

    ZZ22 = gas derivation factor at discharge condition= gas derivation factor at discharge condition

    K = Cp/Cv = Isentropic exponentK = Cp/Cv = Isentropic exponent

    = 11

    1

    2

    1 kv r

    Z

    ZCAE

    DETERMINATION OF COMPRESSOR HORSEPOWERDETERMINATION OF COMPRESSOR HORSEPOWERTheoretical HP is determined by 3 waysTheoretical HP is determined by 3 ways

    - Analytical methodAnalytical method

    - Mollier diagramMollier diagram

    - Quickie estimateQuickie estimate

    ANALYTICAL METHOD:ANALYTICAL METHOD:

    ( )( )

    = 11

    1

    027.31

    K

    KZr

    K

    KT

    T

    PW s

    b

    b

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    Where:Where:

    W = Power required HP/MNscfW = Power required HP/MNscf

    PPbb = Pressure at standard condition (psia)= Pressure at standard condition (psia)

    TTbb = Temperature standard condition (oR)= Temperature standard condition (oR)TT11 = Suction Temperature (oR)= Suction Temperature (oR)

    ZZ22 = Gas deviation factor at suction condition= Gas deviation factor at suction condition

    Mollier DiagramMollier Diagram

    W = 0.0432W = 0.0432 HH

    wherewhereW = Power required (HP/MNSIFD)W = Power required (HP/MNSIFD)

    H = Enthalpy change (BTU/Ib-mol)H = Enthalpy change (BTU/Ib-mol)

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    Quickie ChartsQuickie ChartsUsed for making quick estimates. They give higher values than otherUsed for making quick estimates. They give higher values than othermethods. Should not replace accurate methods.methods. Should not replace accurate methods.

    (Copy charts on Page 140).(Copy charts on Page 140).

    ( )MMcfdbHpT

    TVP

    b

    b /4.14

    1

    bHp =

    OR

    bHp =

    ( )

    ( )MMcfdbHpT

    TqP

    b

    b /

    104

    1

    Where

    V = Inlet capacity of compressor (mmcfd)

    q = Inlet capacity of compressor (cfm)

    Pb = Standard pressure (Psia)

    Tb = Standard temperature (oR)

    T1 = Inlet temperature of compressor (oR)

    (bHp/MMcfd) = Factor determined from chart

    bHp = Power requirement (HP)

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    GAS METERINGGAS METERING

    To determine volumetric flow ratesTo determine volumetric flow rates To determine pressure loss for a particular flow rateTo determine pressure loss for a particular flow rate

    EQUIPMENT USEDEQUIPMENT USED Orifice meterOrifice meter Turbine meterTurbine meter Pilot tubePilot tube

    Critical flow proverCritical flow prover

    ORIFICE METERINGORIFICE METERING Means of measuring the PD caused by a change in velocity of the gas as itMeans of measuring the PD caused by a change in velocity of the gas as it

    passes through a restriction placed in the pipe.passes through a restriction placed in the pipe. Gas flow rate in scf/hr is given asGas flow rate in scf/hr is given as

    fhwpCqsc =

    Where: qsc = gas flowrate scf/hr

    C = Orifice constants

    hw = differential press across the orifice (inches H2O)

    pf= flowing pressure (Psia)

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    C = FC = Fbb FFpbpb FFtbtb FFgg FFtftf FFrr FFpvpv**

    YFm

    Basic Orifice Factor (Fb): Dependends on the location of the differential taps and theDependends on the location of the differential taps and the

    internal pipe diameter and orifice diameter value is obtained from table.internal pipe diameter and orifice diameter value is obtained from table.

    Pressure Base Factor (Fpb ): for pressure correction if the pressure base used is notfor pressure correction if the pressure base used is not

    14.73psia.14.73psia.

    bpb PF 73.14=

    Temperature Base Factor (Ftb): for temperature correction if the base temperature is

    not 520R.

    520

    b

    tb

    TT

    =Specific Gravity Factor (Fg): For SG correlation if the gas SG is other than 1.00

    5.0

    =gYFg

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    5.0

    520

    =fT

    Ftf

    Reynolds Number Factor (Fr): It accounts for variation of the discharge

    coefficient with Reynolds number. Value obtained from chart

    Supercompressibility factor (Fpv ): It corrects the variation from the ideal

    gas law:

    ( ) 5.01

    =pvF

    Expansion Factor (Y): It accounts for change in gas density as the

    pressure changes across the orifice. The change is usually small and

    therefore ignored

    Manometer Factor (Fm): For correction when mercury-type manometer

    is used. It accounts for different heads of gas above the two legs of the

    manometer. Usually small value and therefore insignificant.

    Flowing Temperature Factor (Ftf): For flowing temperature correction

    if the flowing temperature of gas is other than 600F

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    Turbine MeterTurbine Meter

    A velocity responsive meter that is connected in the pipeline such thatA velocity responsive meter that is connected in the pipeline such that

    the entire gas stream passes through the meter.the entire gas stream passes through the meter.

    A propeller in the meter turns at a velocity which is proportional to theA propeller in the meter turns at a velocity which is proportional to the

    velocity of the fluid flowing through itvelocity of the fluid flowing through it A secondary element to sense and totalize the revolutions of theA secondary element to sense and totalize the revolutions of the

    propeller is connected.propeller is connected.

    Flow in WellsFlow in Wells

    Several methods are available for calculating static and flowing pressureSeveral methods are available for calculating static and flowing pressuredrop in gas wells. The most widely used method is that of cullender anddrop in gas wells. The most widely used method is that of cullender and

    smith.smith.

    The pressure gradient equation applicable to any fluid at any pipeThe pressure gradient equation applicable to any fluid at any pipe

    inclination angle is give asinclination angle is give as

    )1..(..........2

    2

    dLg

    vdv

    dg

    vfSing

    g

    dL

    dp

    ccc

    ++=

    )2..(..........accfel dL

    d

    dL

    d

    dL

    d

    dL

    dp

    +

    +

    =

    OR

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    Static Bottom Hole PressureStatic Bottom Hole Pressure

    For a vertical (For a vertical ( = 90= 9000, Sin, Sin = 1), shut in (v = 0) gas well, equation 1 becomes= 1), shut in (v = 0) gas well, equation 1 becomes

    =

    =

    =

    =

    H

    c

    ws

    ts

    c

    g

    c

    g

    dhTZRg

    gMd

    RZTg

    gMdhd

    ZRT

    PM

    g

    g

    dh

    dp

    0

    )3.......(..........

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    In oilfield unitIn oilfield unit

    ( )( )

    =

    TZ

    Hytsws

    g01875.0exp

    WhereWhere

    Pws = Static or shut in BHP (psia)Pws = Static or shut in BHP (psia)

    Pts = Static tubing pressure (psia)Pts = Static tubing pressure (psia)

    yg = Gas gravityyg = Gas gravity

    H = Well depth (ft)H = Well depth (ft)

    factorilitycompressibGasZ

    ORtubingtheinetemperaturAverageT

    ==

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    Cullender and Smith MethodCullender and Smith Method

    From equation (3), we can writeFrom equation (3), we can write

    HyR

    MHdhR

    Md

    TZg

    Hws

    ts 01875.00 ===

    This integral is written in short notation asThis integral is written in short notation as

    HyIddTZ

    g

    ws

    ts

    ws

    ts 01875.0==

    Using a series expansionUsing a series expansion

    ( ) ( ) ( )( )mswsmswstsMStsMS IIIIId ++= 2

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    Where

    ms = Pressure at mid point of well (H/s)

    Ims

    = I evaluated at ms

    , T

    Its = I evaluated at ts, Ts

    Iws = I evaluated at ws , Tf

    ssms

    gmsws

    tsms

    g

    tsms

    IIHy

    II

    Hy

    ++=

    ++=

    01875.0

    01875.0

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    FLOWING BOTTOM HOLE PRESUREFLOWING BOTTOM HOLE PRESURE

    ( )( ) ( )( )

    5

    2 1exp25exp

    2

    Sd

    SMDfZTqyS

    g

    wf tf

    +=

    Where

    Pwf = Flowing bottom hole pressure (psia)

    S = 0.0375yg (TVD)/TZ

    MD = Measure depth (ft)

    TVD = True vertical depth (ft)

    T = 0R

    q = MMScfd

    d = inches

    f = F(NRR,E/d) (Jain or Colebrook equation)

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    FLOW IN PIPELINESFLOW IN PIPELINES

    5.2

    5.022

    21 D

    LZTfyP

    CTq

    gb

    b

    =

    Value of C depends on the units used

    T d L q C

    Psia 0R in Mi scfd 77.54

    Psia 0R in ft scfd 56.38

    Psia 0R in ft MMscfd 5.638 x 10-3

    Kpa 0K M m M3/d 1.149 x 106

    Where

    f = friction factor

    D = Diameter of pipeline (inches)

    L = Length of Pipeline (miles)

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    Evaluation of friction factorEvaluation of friction factor

    Weymouth =

    Panhandle A =

    Panhandle B =

    3

    1032.0

    D

    147.0Re

    /085.0 Nf

    183.0

    Re

    015.0N

    Pipeline flow equation without f becomes

    [ ]51

    432

    21

    2

    1

    2

    1 a

    a

    g

    aa

    b

    b dyLZT

    TEaq

    =

    Where the values of as are

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    aa11 aa22 aa33 aa44 aa55

    Weymouth:Weymouth: 433.50433.50 1.0001.000 0.50000.5000 0.50000.5000 2.6672.667

    Panhandle A:Panhandle A: 435.87435.87 1.07881.0788 0.53940.5394 0.46040.4604 2.6182.618

    Panhandle B:Panhandle B: 737.00737.00 1.02001.0200 0.51000.5100 0.49000.4900 2.5302.530

    qq == ftft33/day/day

    TT == 00RR

    == psiapsiaLL == milesmiles

    dd == inchesinches

    Weymouth equation is used for pipeline diameter of dWeymouth equation is used for pipeline diameter of d 16 inches16 inches

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    Pipeline in SeriesPipeline in Series

    TT == 11 ++ 22 ++ 33

    =N

    i i

    ie

    dLdL

    1333.5

    333.5

    Pipeline in ParallelPipeline in Parallel

    qqTT = q= q11 + q+ q22 ++qq33

    ==

    N

    i

    aN

    i i

    iT diC

    f

    dCq

    1

    5

    1

    1

    5.0

    5.2

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    WELL PERFORMANCEWELL PERFORMANCE

    Two phase flow problem in flowing wells can be handled byTwo phase flow problem in flowing wells can be handled by

    1.1. Fluid gravity adjustmentFluid gravity adjustment2.2. Correlations Hagedorn & BrownCorrelations Hagedorn & Brown

    Gravity AdjustmentGravity Adjustment

    - Adjusting gas gravity to a mixture gravity to account for the added densityAdjusting gas gravity to a mixture gravity to account for the added density

    due to the liquid.due to the liquid.- The mixture gravity is given byThe mixture gravity is given by

    R

    Ryyy

    Lg

    m/11231

    4591

    ++

    =

    WhereWhere yymm == adjusted fluid gravityadjusted fluid gravity

    yygg == dry gas gravitydry gas gravity

    yyLL == liquid specific gravityliquid specific gravity

    RR == Producing gas liquid ratio (Scf/STB)Producing gas liquid ratio (Scf/STB)

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    Hagedorn and Brown Method:Hagedorn and Brown Method:

    Ignoring acceleration componentIgnoring acceleration component

    dg

    VfCos

    g

    g

    dh

    dp

    c

    mf

    m

    c 2

    2

    +=

    mm == LLHHLL ++ gg (1 H(1 HLL))

    L=L= Liquid densityLiquid density

    gg = gas density= gas density

    HHLL = Liquid holdup (fraction of pipe occupies by liquid)= Liquid holdup (fraction of pipe occupies by liquid)

    = angle of well segment from vertical= angle of well segment from vertical

    VVmm = V= VSLSL + V+ Vsgsg

    VVSLSL = Superficial liquid velocity = q= Superficial liquid velocity = qLL/A/AAA = area of flowing string= area of flowing string dd22/4/4d = flow string IDd = flow string ID

    ff == nn22// mm

    nn ==

    LL ++

    (1-(1-

    ))

    =V=V /V/V

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    The fraction factor is calculated Jain equation asThe fraction factor is calculated Jain equation as

    +

    =

    9.0

    25.21214.1

    1

    RENd

    Logf

    m

    mnm

    dVN

    =Re

    WhereWhere( )LH

    L g

    H

    Lm

    =

    1

    L = Liquid viscosity= Liquid viscosity

    g = gas viscosity= gas viscosity

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    To determine HTo determine HLL, we need to calculate, we need to calculate

    25.0

    3

    5.0

    25.0

    25.0

    0.115726.0

    872.120

    938.1

    938.1

    =

    =

    =

    =

    LLL

    Ld

    LsggV

    LSLLV

    N

    dN

    VN

    VN

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    WhereWhere VVSL,SL, VVSgSg = ft/Sec= ft/Sec

    LL = Ib/ft= Ib/ft33

    = dynes / cm= dynes / cmd = ftd = ft

    LL= centipoise= centipoise

    ThenThen

    1.1. Calculate NCalculate NLL

    2.2. Find CNFind CNLL from figure 4.7from figure 4.7

    3.3. Calculate XCalculate XHH

    ( ) 1.0575.01.0

    agvd

    LVH

    NNCNLNX

    =

    WhereWhere aa = 14.7psia= 14.7psia

    4.4. Find HFind HLL//b from figure 4.8b from figure 4.8

    5.5. Calculate XCalculate X

    14.2

    38.0

    d

    Lgr

    N

    NNX =

    6. Find from figure 4.9

    7. Calculate HL =

    LH

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    FIELD HANDLING OF NATURAL GASFIELD HANDLING OF NATURAL GAS

    A typical well stream is a high velocity, turbulent and constantlyA typical well stream is a high velocity, turbulent and constantly

    expanding mixture of gases, hydrocarbon liquids, water vapour,expanding mixture of gases, hydrocarbon liquids, water vapour,

    free water, solids and other contaminants. Field processing offree water, solids and other contaminants. Field processing of

    NG consists of four basic processes.NG consists of four basic processes.

    1.1. Separation of the gas from free liquids and entrained solidsSeparation of the gas from free liquids and entrained solids

    2.2. Processing the gas to remove condensable and recoverableProcessing the gas to remove condensable and recoverablehydrocabon vapoourshydrocabon vapoours

    3.3. Processing the gas to remove condensable water vapour to avoidProcessing the gas to remove condensable water vapour to avoid

    hydrate formation.hydrate formation.

    4.4. Processing the gas to remove other undesirable componentsProcessing the gas to remove other undesirable components

    such as hydrogen sulphide and carbon dioxidesuch as hydrogen sulphide and carbon dioxide

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    SEPARATORSSEPARATORS

    Separation of well stream gas from free liquids/solids isSeparation of well stream gas from free liquids/solids isaccomplished in a separatoraccomplished in a separator

    FUNCTIONS OF SEPARATORSFUNCTIONS OF SEPARATORS1.1. Causes of primary phase separation of the liquid hydrocarbonsCauses of primary phase separation of the liquid hydrocarbons

    from these that are mostly gas.from these that are mostly gas.

    2.2. Refine the primary separation by removing most of the entrainedRefine the primary separation by removing most of the entrainedliquid mist from the gas.liquid mist from the gas.

    3.3. Further refine the separation by removing the entrained gas fromFurther refine the separation by removing the entrained gas fromthe liquid.the liquid.

    4.4. Discharge the separated gas and liquid from vessel and ensureDischarge the separated gas and liquid from vessel and ensurethat no re-entrainment of one into the other.that no re-entrainment of one into the other.

    TYPESTYPES

    1.1. VerticalVertical

    2.2. HorizontalHorizontal

    3.3. Horizontal Double BarrelHorizontal Double Barrel

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    Each has specific advantages and selection is based on which one willEach has specific advantages and selection is based on which one will

    accomplish the desired results at the lowest cost.accomplish the desired results at the lowest cost.

    ACID GAS REMOVALACID GAS REMOVAL

    -- Maximum Allowable of HMaximum Allowable of H22S is sales Gas isS is sales Gas is

    (0.25gm per 100ft(0.25gm per 100ft33 or 4ppm/100ftor 4ppm/100ft33))

    Hydrogen sulphide and carbon Dioxide are removed by Absorption process:Hydrogen sulphide and carbon Dioxide are removed by Absorption process:

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    Chemicals used are:Chemicals used are:

    MEAMEA

    DEADEASulfinolSulfinol

    Molecular sieveMolecular sieve

    Iron SpongeIron Sponge

    GAS DEHYDRATIONGAS DEHYDRATION

    Removal of water vapour from natural gasRemoval of water vapour from natural gas

    Maximum allowable is 7Ib of HMaximum allowable is 7Ib of H220/Mcf of gas0/Mcf of gas

    Processes involvedProcesses involved1.1. AbsorptionAbsorption

    2.2. AdorptionAdorption

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    LIQUID HYDROCABON RECOVERYLIQUID HYDROCABON RECOVERY Products extracted from the gas in liquid recovery may include:Products extracted from the gas in liquid recovery may include:

    EthaneEthane

    PropanePropane

    IsobutaneIsobutaneNormal butaneNormal butane

    Natural GasolineNatural Gasoline

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    HYDROGEN SULPHIDE TREATMENTHYDROGEN SULPHIDE TREATMENT

    Clans processClans process

    Two stages involvedTwo stages involved

    Thermal step: HThermal step: H22S is partially oxidized in a furnance to S0S is partially oxidized in a furnance to S022

    Temperature 1000 1400Temperature 1000 140000cc

    Catalytic step: HCatalytic step: H22S reacts over VS reacts over V220055 catalyst with S0catalyst with S022

    002

    1

    03

    2031

    31

    03

    103

    102

    13

    1

    222

    222

    2222

    HSSH

    HSSSH

    HSSH

    ++

    ++

    ++

    GAS CONDENSATE SYSTEMSGAS CONDENSATE SYSTEMS

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    GAS CONDENSATE SYSTEMSGAS CONDENSATE SYSTEMS

    Gas at initial reservoir conditions but condenses to form same liquid atGas at initial reservoir conditions but condenses to form same liquid at

    some point in its path to the separator.some point in its path to the separator.

    They include both wet gas and retrograde condensate reservoirs.They include both wet gas and retrograde condensate reservoirs.

    - Wet gas Fluid initially exists as a gas in the reservior and remains in theWet gas Fluid initially exists as a gas in the reservior and remains in thegaseous phase as pressure declines at reservoir temperature. However, ingaseous phase as pressure declines at reservoir temperature. However, in

    being produced to the surface, the temperature drops, causingbeing produced to the surface, the temperature drops, causing

    condensation in the piping system and separator.condensation in the piping system and separator.

    - Retrograde gas fluid exists as a gas at initial reservoir conditions. AsRetrograde gas fluid exists as a gas at initial reservoir conditions. As

    reservoir pressure declines at reservour temperature, the dew point line isreservoir pressure declines at reservour temperature, the dew point line is

    crossed and liquid forms in the reservoir, piping system and separator.crossed and liquid forms in the reservoir, piping system and separator.

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    PHASE BEHAVIOURPHASE BEHAVIOUR

    The phase behaviour of a fluid can be described by determining its response toThe phase behaviour of a fluid can be described by determining its response to

    pressure and temperature changes.pressure and temperature changes.

    - Liquid: molecules are very close togetherLiquid: molecules are very close together

    - Gas: molecules are widely separatedGas: molecules are widely separated

    - Confining forces: Pressure and molecular attractionConfining forces: Pressure and molecular attraction

    - Dispersing forces: Kinetic energy (temperature) and molecular repulsion.Dispersing forces: Kinetic energy (temperature) and molecular repulsion.

    - The magnitudes of the confining and dispersing forces dictate whether theThe magnitudes of the confining and dispersing forces dictate whether the

    fluid is a liquid or a gas.fluid is a liquid or a gas.

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    For multicomponent systemFor multicomponent system

    The difference in molecule size and energy has influence on the phaseThe difference in molecule size and energy has influence on the phase

    change.change.

    - The locus of all the points where the first bubble of gas appears inThe locus of all the points where the first bubble of gas appears in

    liquid as pressure and temperature conditions are changed is calledliquid as pressure and temperature conditions are changed is called

    the bubble point here.the bubble point here.

    - The locus of all points where the first droplet of liquid appears in aThe locus of all points where the first droplet of liquid appears in a

    gas as the conditions are changed is called dew point line.gas as the conditions are changed is called dew point line.- The highest pressure at which a gas can exist is called theThe highest pressure at which a gas can exist is called the

    cricondenbar.cricondenbar.

    - The highest temperature at which a liquid can exist is called theThe highest temperature at which a liquid can exist is called the

    cricondenthermcricondentherm

    CALCULATION OF VAPOUR LIQUID EQUILIBRIACALCULATION OF VAPOUR LIQUID EQUILIBRIA

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    CALCULATION OF VAPOUR LIQUID EQUILIBRIACALCULATION OF VAPOUR LIQUID EQUILIBRIA

    From the relationship:From the relationship:

    iii

    i

    ii xKy

    x

    yK ==

    andand

    ZZiin = xn = xiiL + yL + yiiVV

    VKL

    nZx

    i

    ii +=

    xxii=1 and +=1 and + yyii = 1= 1

    HenceHence

    1=+

    =VKL

    nZx

    i

    ii

    andand

    1=+

    =i

    ii

    KLV

    nZy

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    WhereWhere

    nn == total No. of moles V in mixturetotal No. of moles V in mixture

    LL == total No. of moles V in liquidtotal No. of moles V in liquid

    VV == total no of moles V in vapourtotal no of moles V in vapour

    ZZii == mole fraction of component i in mixturemole fraction of component i in mixture

    KKii == equilibrium ratio of componentequilibrium ratio of component

    yy ii == mole fraction of component i in vapour phasemole fraction of component i in vapour phase

    xx ii == mole fraction of component i in liquid phasemole fraction of component i in liquid phase

    BUBBLE POINT PRESSUREBUBBLE POINT PRESSUREAt bubble pointAt bubble point

    VV 00LL nn

    HenceHence

    =

    +=

    10 VkL

    nZLimy

    i

    i

    Vi

    =1i

    i

    K

    ZOR

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    NOTENOTE

    IfIf ZZiiKKii > 1, the assumed pressure is below> 1, the assumed pressure is below bbIfIf ZZ

    ii

    KKii

    > 1, the assumed pressure is above> 1, the assumed pressure is above bb

    1ii K

    ZIf The assumed pressure is above d

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    DETERMINATION OF INITIAL OIL & GAS IN PLACEDETERMINATION OF INITIAL OIL & GAS IN PLACE

    Let:Let: R = Initial surface gas oil ratioR = Initial surface gas oil ratio

    yy00 = Specifi gravity of the tank oil= Specifi gravity of the tank oil

    MMoo = Molecular weight of the tank oil= Molecular weight of the tank oil

    yygg = Specific gravity of produced gas= Specific gravity of produced gas

    Standard conditions:Standard conditions: 14.7psia14.7psia

    606000FF

    379.4 Scf/mole379.4 Scf/mole

    Ome the basis of one bbl of tank oil/R Scf of gasOme the basis of one bbl of tank oil/R Scf of gas

    - The mass of total well fluid (MThe mass of total well fluid (Mww) is) is

    MMww = 0.07636RY= 0.07636RYgg + 350Y+ 350Y00

    - The total moles of fluid in one bbl of oil and R cubic feet of gas isThe total moles of fluid in one bbl of oil and R cubic feet of gas isnn tt = 0.002636R + 350 y= 0.002636R + 350 y00/M/Moo

    -- The molecular weight of the well fluid MThe molecular weight of the well fluid Mww

    0

    0

    0

    350002636.0

    35007636.0

    MY

    R

    yRy

    n

    MM

    g

    t

    ww

    +

    +==

    The specific gravity of the well fluid isThe specific gravity of the well fluid is

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    - The specific gravity of the well fluid is- The specific gravity of the well fluid is

    0

    0

    0

    800,132

    4584

    My

    R

    yRyy

    OR

    n

    My

    g

    w

    t

    ww

    +

    +=

    =

    5.131

    5.141

    9.56084

    03.129.44

    0

    0

    00

    +=

    =

    =

    APIy

    APIyyM

    nngg = No. of Mole of gas == No. of Mole of gas =

    NN00 = No of mole of oil == No of mole of oil =

    4.395R

    0

    0350M

    y

    Th f ti f th t t l th t i d d th f iThe fraction of the total gas that is prod ced on the s rface as gas is

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    The fraction of the total gas that is produced on the surface as gas isThe fraction of the total gas that is produced on the surface as gas is

    0nn

    nf

    g

    g

    g +=

    The total initial gas in place per acre foot of bulk reservoir rock isThe total initial gas in place per acre foot of bulk reservoir rock is

    ( )( )ftacreMcf

    ZRT

    SG w

    = /

    1664,528,16

    Hence:Hence:

    Initial Gas In Place = fInitial Gas In Place = fggGG

    Intial Oil in Place =Intial Oil in Place =R

    Gfg

    THERMODYNAMICS CONCEPTSTHERMODYNAMICS CONCEPTS

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    THERMODYNAMICS CONCEPTSTHERMODYNAMICS CONCEPTS

    Natural gas processing involves controlling the mass and energyNatural gas processing involves controlling the mass and energy

    transfer within, to or from the fluid/stream under consideration.transfer within, to or from the fluid/stream under consideration.

    The calculations in natural gas processing involve the prediction ofThe calculations in natural gas processing involve the prediction ofenthalpy, internal energy and entropy of the system.enthalpy, internal energy and entropy of the system.

    These functions are determined usingThese functions are determined using

    1.1.PVT dataPVT data

    2.2.Tables of dataTables of data3.3.Generalized correlations for H and SGeneralized correlations for H and S

    4.4.Figures showing H & S as functions of system PVTFigures showing H & S as functions of system PVT

    2

    2

    MVEK =

    Kinetic Energy

    Potential Energy

    MghE =

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    Internal Energy (U) energy of system by virtue of its state.Internal Energy (U) energy of system by virtue of its state.

    Enthalpy (H): H = U +Enthalpy (H): H = U + VV

    Heat (Q): energy in transition across the boundary of the systemHeat (Q): energy in transition across the boundary of the system

    Entropy (S):Entropy (S): S = Q/TS = Q/T

    Q = MCQ = MC tt

    Calculation UsingCalculation Using VT DataVT DataBoth enthalpy and entropy can be expressed in terms of otherBoth enthalpy and entropy can be expressed in terms of other

    thermodynamic properties.thermodynamic properties.

    ddT

    dv

    T

    dTCdS

    ddT

    dvTVdTCdH

    =

    +=

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    WhereWhere CC = S= S ht at constant pressureht at constant pressure , T = Pressure and Temperature (absolute units), T = Pressure and Temperature (absolute units)V = Corresponding volume of the systemV = Corresponding volume of the system

    Calculation using Table of Thermodynamic PropertiesCalculation using Table of Thermodynamic Properties

    The thermodynamic property of a two phase mixture is found fromThe thermodynamic property of a two phase mixture is found from

    the saturated tables as:the saturated tables as:

    t = (1 x) tg + x t f

    WhereWhere t = thermodyanmical property (h, S, V) of mixturet = thermodyanmical property (h, S, V) of mixture

    ttgg = thermodyanmical property of saturated vapour= thermodyanmical property of saturated vapour

    ttff = thermodyanmical property of saturated liquid= thermodyanmical property of saturated liquid

    X = composition of liquid in mixtureX = composition of liquid in mixture

    Calculation using Charts and FiguresCalculation using Charts and Figures

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    Calculation using Charts and FiguresCalculation using Charts and Figures

    The four useful chaarts areThe four useful chaarts are

    (1)(1) Enthalpy temperature (H.T)Enthalpy temperature (H.T)

    (2)(2) Enthalpy pressure (H.P)Enthalpy pressure (H.P)(3)(3) Enthalpy Entropy (H.S) Mollier diagramEnthalpy Entropy (H.S) Mollier diagram

    (4)(4) Temperature Endropy (T.S)Temperature Endropy (T.S)

    GAS UTILIZATION AND CONSERVATIONGAS UTILIZATION AND CONSERVATION

    - LNGLNG- GTLGTL

    - POWERPOWER

    - FEEDSTOCKFEEDSTOCK

    (Fig required)(Fig required)