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  • Introduction:Introduction:Solving Gas Well Solving Gas Well Liquid Loading

    P blLiquid Loading

    P blProblemsProblems

  • ObjectivesObjectives

    Understand: Concepts of Liquid Loading

    Fi ld S t Field Symptoms Critical Velocity/Rate Nodal Analysis Concepts Nodal Analysis Concepts

    2

  • U.S. Gas Well ProductionU.S. Gas Well Production

    U.S. Historical Gas Well Facts70 000 700

    60,000

    70,000

    F

    D

    600

    700

    M

    C

    F

    D

    /

    W

    e

    l

    l

    ProductionWell CountAvg Well Rate

    40,000

    50,000

    u

    c

    t

    i

    o

    n

    ,

    M

    M

    C

    F

    400

    500

    g

    G

    a

    s

    R

    a

    t

    e

    ,

    M

    20,000

    30,000

    v

    g

    D

    a

    i

    l

    y

    P

    r

    o

    d

    u

    200

    300

    t

    ,

    0

    0

    0

    '

    s

    o

    r

    A

    v

    g

    10,000

    A

    v

    100

    W

    e

    l

    l

    C

    o

    u

    n

    t

    3

    J F Lea PLTech LLC 3

    01965 1970 1975 1980 1985 1990 1995 2000 2005 2010

    0

    Source: EIA

  • Canadian Gas Well Production No CBMCanadian Gas Well Production No CBM

    Canadian Historical Gas Well Facts25,000 250 2,500

    20,000

    25,000

    D

    200

    250ProductionWell CountAvg Well Rate

    ,

    2,000

    W

    e

    l

    l

    15,000

    c

    t

    i

    o

    n

    ,

    M

    M

    C

    F

    D

    150

    o

    u

    n

    t

    ,

    0

    0

    0

    '

    s

    1,500

    R

    a

    t

    e

    ,

    M

    C

    F

    D

    /

    W

    10,000

    G

    a

    s

    P

    r

    o

    d

    u

    c

    100

    W

    e

    l

    l

    C

    o

    1,000

    500

    A

    v

    g

    G

    a

    s

    R

    0

    5,000

    0

    50 500

    0

    4

    J F Lea PLTech LLC 4

    1970 1980 1990 2000 2010

    YearSource: HPDI

  • Canadian Gas Well Production With CBMCanadian Gas Well Production With CBM

    Canadian Historical Gas Well Facts25,000 250 2,500

    20,000

    25,000

    D

    200

    250ProductionWell CountAvg Well Rate

    ,

    2,000

    W

    e

    l

    l

    15,000

    c

    t

    i

    o

    n

    ,

    M

    M

    C

    F

    D

    150

    o

    u

    n

    t

    ,

    0

    0

    0

    '

    s

    1,500

    R

    a

    t

    e

    ,

    M

    C

    F

    D

    /

    W

    10,000

    G

    a

    s

    P

    r

    o

    d

    u

    c

    100

    W

    e

    l

    l

    C

    o

    1,000

    500

    A

    v

    g

    G

    a

    s

    R

    0

    5,000

    0

    50 500

    0

    5

    J F Lea PLTech LLC 5

    1970 1980 1990 2000 2010

    YearSource: HPDI

  • Canadian Gas Well LocationsCanadian Gas Well Locations

    S

    6

    J F Lea PLTech LLC 6

    Source: HPDI

    MS Streets & Trips

  • USA-Canada Gas Well LocationsUSA-Canada Gas Well Locations

    S

    7

    J F Lea PLTech LLC 7

    Source: HPDI

    MS Streets & Trips

  • USA-Canada Gas Well Locations (Post 2000 Production)USA-Canada Gas Well Locations (Post 2000 Production)

    S

    8

    J F Lea PLTech LLC 8

    Source: HPDI

    MS Streets & Trips

  • Shale: New Shale finds also

    9

    J F Lea PLTech LLC 9

  • Horizontal WellHorizontal Well

    Horizontals Horizontal Well Ideal CaseHorizontal Well Ideal Case

    10

    J F Lea PLTech LLC 10

  • Complex Horizontal Well ProfilesComplex Horizontal Well Profiles

    Complex Horizontal Well Profiles10 10010,100

    10,150

    Well 1Well 2Well 3Well 4

    10,200

    10 250

    c

    a

    l

    D

    e

    p

    t

    h

    ,

    f

    t

    Well 5Well 6Well 7Well 8Well 910,250

    10,300

    T

    r

    u

    e

    V

    e

    r

    t

    i

    c

    Well 9

    10,350

    10 400

    11

    J F Lea PLTech LLC 11

    10,4000 1,000 2,000 3,000 4,000 5,000 6,000 7,000

    Departure, ft

  • Complex Horizontal Well Profiles: SPE 149477Complex Horizontal Well Profiles: SPE 149477

    Paper shows:

    Updip gives most recoverable reserves

    Undulating wellbore worse gthan downdip for recoverable reserves

    12

    J F Lea PLTech LLC 12

  • Hydrostatic/Friction loss in Horizontal Hydrostatic/Friction loss in Horizontal

    What would impact the back pressure the pmost Vertical hydrostatic head or horizontal frictional

    Assume ~ 500 ft of hydrostatic

    horizontal frictional loss?

    head

    Assume ~ 2000 ft of

    How length of horizontal frictional Assume 2000 ft of

    fricitional loss due to bubble flow loss would be

    equivalent to 500 ft of hydrostatic head

    13

    hydrostatic head (~200psi)?

    13

  • Horizontal well complexitiesHorizontal well complexities

    Horizontal does not mean straight/constant. Inclination and azimuth varyInclination and azimuth vary

    Gravity affects velocities, fluid collection, and flow regimesFrac ports liners and other IDFrac ports, liners, and other ID changes. Introduces friction, turbulence,

    flow restrictionsflow restrictionsCased vs Open hole. Friction, corrosion, further flow

    t i tirestrictionsSand production and accumulation.

    14

    Introduces friction, turbulence, flow restrictions

    14

  • Horizontal Fluid AccumulationHorizontal Fluid Accumulation

    This and following:

    15

    This and following:

    Courtesy of BP-Calgary/ EPTG Noel15

  • Horizontal Two-phase Flow (cont.)Horizontal Two-phase Flow (cont.)

    Flow regimes are very complicated. Flow has multiple variables Stratified Smooth Flow has multiple variables. Changes with angle, rate,

    gas/fluid densities, temperature

    Stratified Smooth

    Stratified Wavy Flowp

    Multiple flow types exist across all parts of well (horizontal and vertical)

    Plug Flow

    Slug FlowAlso two-phase flow has an negative influence on production rate.

    Pressure lost due to friction

    Slug Flow

    Annular Flow

    Pressure lost due to friction Changes to critical flow rate Changes in flowing gas

    d it d t i t

    Dispersed Bubble Flow

    16

    density due to moisture.

    16

  • Simplified ModelSimplified Model

    Pressure Loss

    Figure 8: Gas-Liquid Flow Simplified Model

    17

    Figure 8: Gas Liquid Flow Simplified Model

    17

  • Progression of Liquid Loading Progression of Liquid Loading

    Gas Flow

    Mist Annular Slug Bubble

    Flow

    Decreasing Gas Velocity

    18

  • Topics CoveredTopics Covered

    Introduction

    1. Introduce, Recognize Loading

    2. Introduce Solution Methods

    3. Velocity string y g

    4. Compression

    5. Plunger

    6 Beam P mping6. Beam Pumping

    7. Gaslift

    8. Hydraulic Pumping

    9. Foaming

    10. Injection Systems

    11. Field Examples

    19

    p

    12. New Techniques

  • Flow Regimes in Gas Well with timeFlow Regimes in Gas Well with time

    HOLDUP (LIQUID) BUILDS WITH TIME

    20

    HOLDUP (LIQUID) BUILDS WITH TIME AND LOWER PRODUCTION

  • Flow Regimes in Gas/Liquid Flow Flow Regimes in Gas/Liquid Flow

    Bubble Flow The tubing is almost completely filled with liquid. Free gas is present as small bubbles, rising in the liquid. Liquid contacts the wall surface and the bubbles serve only to reduce the density.

    Slug Flow - Gas bubbles expand as they rise and coalesce into larger bubbles, then slugs. Liquid phase is still the continuous phase. The li id fil d th l f ll d d B th d li idliquid film around the slugs may fall downward. Both gas and liquid significantly affect the pressure gradient.

    Slug Annular Transition The flow changes from continuousSlug-Annular Transition The flow changes from continuous liquid to continuous gas phase. Some liquid may be entrained as droplets in the gas. Gas dominates the pressure gradient, but liquid is still significantsignificant.

    Annular-Mist Flow - Gas phase is continuous and most of liquid is entrained in the gas as a mist. The pipe wall is coated with a thin film of

    21

    entrained in the gas as a mist. The pipe wall is coated with a thin film of liquid but pressure gradient is determined predominately from the gas flow.

  • Flow Regimes with Time and DepthFlow Regimes with Time and Depth

    22

  • Flow Regimes with Time and DepthFlow Regimes with Time and Depth

    23

  • Effects of Liquid LoadingEffects of Liquid LoadingGas velocity in the tubing has dropped below the minimum required to move liquids up and out of the wellbore.

    Liquids are settling in the bottom of the tubing

    Gas flow is beginning to flowing heads (slug flow) where it has not before onset of liquid loading.

    There are other symptoms as well

    24

  • Problems from Liquid LoadingProblems from Liquid Loading

    Less or no production. Less means production drops below the decline curve trendPossible damage or a water/condensate block onPossible damage or a water/condensate block on formation.More corrosion with more liquids resident in the tubingRequires artificial lift or other remedial measures and associated expenseand associated expense.

    25

  • Source of LiquidsSource of Liquids

    Produced along with gas

    P d d f t tProduced from separate water zone

    Condensed from the saturated gasCondensed from the saturated gas

    Coned into gas zone with timeg

    Other

    26

  • Wet GasWet Gas

    27

  • View of Condensation in Gas WellView of Condensation in Gas Well

    ONE SOURCE OF LIQUIDS: WATER CONDENSING IN TUBING DOWNHOLE

    28

    CONDENSING IN TUBING: DOWNHOLE CAMERA

  • Other Sources of LiquidsOther Sources of LiquidsW t b d i f bWater may be coned in from an aqueous zone above or below the producing zone.

    If the reservoir has aquifer support, the encroaching water will eventually reach the wellbore.

    Water may enter the wellbore from another producing zone which could be separated some distance from the pgas zone

    Free formation water may be produced with the gasFree formation water may be produced with the gas

    Water and/or hydrocarbons may enter the wellbore in the vapor phase with the gas and condense out as

    29

    in the vapor phase with the gas and condense out as a liquid in the tubing

  • Effects of Loading on DeclineEffects of Loading on Decline

    Normal Decline

    Rate, MCFDMCFD

    Loading

    30

    LoadingTime After Phillips & Listiack; SWPSC

  • Effects of Loading on DeclineEffects of Loading on Decline

    Normal Decline

    Rate, MCFD Goal ofMCFD Goal of

    Artificial Lift

    Loading

    31

    Time

    Loading

    After Phillips & Listiack; SWPSC

  • Well Loaded: Being cycled before lift addedWell Loaded: Being cycled before lift added

    Sh t i

    32

    Shut inAfter Phillips & Listiack; SWPSC

  • Cycle to Liquid LoadingCycle to Liquid Loading

    Fl iSh t i

    33

    FlowingShut in

  • Cycle to Liquid LoadingCycle to Liquid Loading

    Flowing L diSh t i

    34

    Flowing Loading upShut in

  • z Flow Rate Declines (see Turner Curve)

    Cycle to Liquid LoadingCycle to Liquid LoadingFlow Rate Declines (see Turner Curve)

    z Velocity in Tubing Dropsz Settling Fluid Creates Back Pressure and Continues to Drop Flow Rate

    High LinePPressure

    Friction

    Fl i L d OffL diSh t i

    35

    Flowing Logged OffLoading upShut inA well loads up when it is FLOWING at LOW gas rates!.

  • Shut-In WellShut-In Well

    L d d

    36

    Loaded Shut inA well DOES NOT load up when it is shut in.

    After Phillips & Listiack; SWPSC

  • Tubing / Casing Pressures Tubing / Casing Pressures

    After Phillips & Listiack; SWPSC

    100 PSI

    130 PSI

    100 PSI

    100 PSI

    100 PSI

    220 PSI

    100 PSI

    80 PSI130 PSI 100 PSI

    x

    220 PSI

    x

    T bing

    37

    Normal Tubing Leak

    Loaded Casing Leak

  • Pressures with a Packer in PlacePressures with a Packer in Place

    0 PSI

    100 PSI

    0 PSI

    130 PSI

    0 PSI

    100 PSI 101 PSI

    0 PSI0 PSI 0 PSI 0 PSI 0 PSI

    After Phillips & Listiack; SWPSC

    38

    Flowing Unloaded

    1-MinuteShut-in

    Flowing Loaded

    1-Minute Shut-in

  • Loading & Well IPRLoading & Well IPRLoading & Well IPRLoading & Well IPR

    IPR = Inflow Performance Relationship

    39

  • Typical IPR for Gas WellTypical IPR for Gas Well

    800

    s

    i

    a

    500600700

    s

    s

    u

    r

    e

    ,

    p

    s

    After Phillips & Listiack; SWPSC

    300400500

    n

    g

    P

    r

    e

    s

    100200

    F

    l

    o

    w

    i

    00 50 100 150 200 250 300

    40

    Rate, mcfd

  • Hi/Lo Shut-In Pressures for Gas WellHi/Lo Shut-In Pressures for Gas Well

    700800

    p

    s

    i

    a

    Higher Pressure Gas Well

    400500600

    r

    e

    s

    s

    u

    r

    e

    ,

    Higher Pressure Gas Well

    200300400

    o

    w

    i

    n

    g

    P Lower Pressure Gas Well

    0100

    0 50 100 150 200 250 300

    F

    l

    41

    0 50 100 150 200 250 300

    Rate, mcfd

  • Effects of Loading on IPREffects of Loading on IPR

    100 PSI

    130 PSI

    100 PSI

    300 PSI

    After Phillips & Listiack; SWPSC

    N l L d d

    42

    Normal Loaded

  • IPR: Reacting to Hi/Lo pressures IPR: Reacting to Hi/Lo pressures

    350400

    e

    ,

    p

    s

    i

    a

    200250300

    P

    r

    e

    s

    s

    u

    r

    e

    100150200

    F

    l

    o

    w

    i

    n

    g

    P

    050

    0 50 100 150 200 250 300

    F

    43

    0 50 100 150 200 250 300

    Rate, mcfd

  • Single Phase Radial Flow Gas EquationSingle Phase Radial Flow Gas Equation

    44

  • Gas Well Back Pressure EquationGas Well Back Pressure Equation

    n22Mscf/D )PwfC(PrQ, =

    Exponent n reflects total turbulence effects- reservoir and completionand completion For low turbulence n ~ 1 For high turbulence n ~ .5

    C and n are determined from multipoint flow tests

    Flow after Flow Isochronal Modified Isochronal

    45

  • Recognizing Liquid LoadingRecognizing Liquid Loading

    Producing Symptoms

    C iti l V l itCritical Velocity

    Nodal AnalysisNodal Analysis

    46

  • Slugs of Liquid through Gas Measure DeviceSlugs of Liquid through Gas Measure Device

    Production of slugs of liquid g q

    when previously not present.

    Charts may not be used still look for slugging throughslugging through DP transducer?

    47

  • Slugs still present but reduced Slugs still present but reduced

    L li ?Lower line pressure?Reduced tubing size?Added heat??

    48

  • Drop off decline curve indicates loadingDrop off decline curve indicates loading

    Could be tubing leak Could be salting or sand over perforations

    Decline w/wo Liquid Loading

    But if not other problems then indicates liquid loading

    Expected

    Decline w/wo Liquid Loading

    Actual with L dio

    n

    R

    a

    t

    e

    Loading

    P

    r

    o

    d

    u

    c

    t

    i

    o

    49

    Time

  • Increase in CP minus TP: Loading likelyIncrease in CP minus TP: Loading likely

    Tubing Pressure

    Increase in Casing minus Tubing Pressure

    ti i di t

    C i

    vs. time indicates loading

    Casing Pressure

    g Ps

    iC

    sg

    Tbg

    Time

    50

  • Tubing survey or Echometer shot: LoadingTubing survey or Echometer shot: Loading

    Results of Pressure Survey

    Pressure

    hD

    epth

    Gas

    Liquid

    51

  • Tubing Pressure Profile: What is Happening?Tubing Pressure Profile: What is Happening?

    Tubing Pressure

    Dep

    Condensation

    Gradient

    Gas & liquid vapor

    pth

    Gas & liquid vapor gradient

    Liquid over the perforations

    52

    Pressure

  • Loading Prediction: Critical Velocity or RateLoading Prediction: Critical Velocity or Rate

    Buoyant weight of

    Droplet in flowing gas

    gdroplet in gas

    Drag from flowing gasflowing gas tending to lift the droplet

    53

  • Turner used Droplet model Not film modelTurner used Droplet model Not film model

    ( ) 3dgF ( )6g

    gF GLC

    Gravity =

    2, )(2

    1dGdDG

    CUPDrag VVACg

    F = Cg

    Whereg = gravitational constant = 32.17 ft/s2gC = 32.17 lbm-ft/lbf-s2d = droplet diameterrL = liquid densityrG = gas densityCD = drag coefficientAd = droplet projected cross-sectional areaV = gas velocity

    54

    VG = gas velocityVd = droplet velocity

  • Equate Weight of Droplet to Uplift on DropletEquate Weight of Droplet to Uplift on Droplet

    DG FF =

    ( ) 232

    16 CdDGGL

    VACdg =( )26 CdDGC

    GLC gg

    Substituting A = d2/4 and solving for V givesSubstituting Ad = d /4 and solving for VC gives,

    ( )GL dgV 4 ( )DG

    GLC C

    gV =

    3

    55

  • Hinze AICHE Journal Sept 1955 shows that droplet diameter dependence

    Literature Correlation Predicts Droplet SizeLiterature Correlation Predicts Droplet SizeHinze, AICHE Journal Sept 1955, shows that droplet diameter dependence

    can be expressed in terms of the dimensionless Weber number

    302

    == GCWE gdVN

    Cg

    Solving for the droplet diameter gives

    g230CG

    C

    Vgd

    =and substituting into Equation A-1 gives

    ( )2303

    4

    CG

    C

    DG

    GLC V

    gCgV

    =

    or

    4/14/140

    = GLCggV

    56

    2

    = GDC CV

  • Substitute values of Cd and Surface TensionSubstitute values of Cd and Surface TensionTurner assumed a drag coefficient of CD = .44 that is valid for fully turbulent conditions. Substituting the turbulent drag coefficient and values for g and gC gives:

    fV GL /514174/1

    sftVG

    GLC /514.17 2

    =

    WhereWhererL=liquid density, lbm/ft3rG=gas density, lbm/ft3s=surface tension, lbf/ftWritten for surface tension in dyne/cm units

    i th i lbf/ft 00006852 d / iusing the conversion lbf/ft = .00006852 dyne/cm gives:

    sftV GLC /59314/1

    = sftV

    GC /593.1 2

    WhererL=liquid density, lbm/ft3r =gas density lbm/ft3

    57

    rG=gas density, lbm/ft3s=surface tension, dyne/cm

  • Calculate Gas Density: Real Gas LawCalculate Gas Density: Real Gas Law

    Evaluating Equation A-4 for typical values ofGas gravity G 0.6Temperature T 120FTemperature T 120FGas deviation factor Z: 0.9gives:

    3/0031.9)120460(

    6.715.2 ftlbmPPG =+= 9.)120460( +

    Typical values for density and surface tension areTypical values for density and surface tension areWater density 67 lbm/ft3Condensate density 45 lbm/ft3Water surface tension 60 dyne/cmCondensate surface tension 20 dyne/cm

    58

    Condensate surface tension 20 dyne/cm

  • C l l (E )

    Field Equations: Turner & ColemanField Equations: Turner & Coleman

    ( ) fPPV /0031.674344600031.675931 4/14/1

    Coleman, et al., (Exxon)

    ( )( )

    ( ) sftPPV waterC /0031.434.4600031.593.1 2/12, ==

    ( )PP 003145003145 4/14/1 ( )( )( ) sftP

    PP

    PV condC /0031.0031.45369.320

    0031.0031.45593.1 2/12,

    =

    =

    Turner et al (with 20% adjustment)

    ( ) sftPV /0031.673215 4/1=Turner et al., (with 20% adjustment)

    ( ) sftPV waterC /0031.321.5 2/1, =( ) sftPV /0031.450434 4/1

    59

    ( )( ) sftPV condC /0031.043.4 2/1, =

  • Use Critical Velocity to find Critical RateUse Critical Velocity to find Critical Rate

    Turner et al., (with 20% adjustment)

    ( )( ) sftP

    PV waterC /0031.0031.67321.5 2/1

    4/1

    ,=

    ( )( ) sftP

    PV condC /0031.0031.45043.4 2/1

    4/1

    ,=

    2/1

    4/12

    , )0031(.)0031.45(

    )460(0676.

    )/(P

    PZT

    dPDMMscfq ticondensatet

    +=

    2/1

    4/12

    , )0031(.)0031.67(

    )460(0890.

    )/(P

    PZT

    dPDMMscfq tiwatert

    +=

    60

  • View Comparing Turner/ Coleman WHP DataView Comparing Turner/ Coleman WHP Data

    61

  • Results from Shell Paper Results from Shell Paper

    Evaluating Liquid LoadingField Data & Remedial MeasuresField Data & Remedial Measures

    By Kees Veeken & Eelco Bakker, NAMNAM

    Paul Verbeek, ShellThe NetherlandsThe Netherlands

    2002 Denver Forum

    62

  • Comparing to TurnerComparing to Turner

    Turner Ratio vs Best Fit Combination of A and FTHP

    4.00

    3.00

    3.50

    y = 3.4441x-0.1717

    R2 = 0 2085

    2.00

    2.50

    T

    R

    (

    -

    )

    R = 0.2085

    1.00

    1.50

    0.00

    0.50

    0 100 200 300 400 500 600 700 800 900 1000

    63

    A0.5 x FTHP

  • Example of Using Shell CorrelationExample of Using Shell Correlation

    Turner Ratio (TR) is ratio between actual and TurnerBest fit TR = 3.77 (A0.5 x FTHP) -0.172

    Inflow resistance A ~ (Pdd / Q)xPr [ bar2 / 1000 m3/d ]

    OR:TR = 3.77 (A0.5 x FTHP, psi/ 14.5) -.172

    Example:

    A = (0.1678)(Pwf,psi)(Pr,psi) / (Mscf/D)

    Example:

    Pwf=500Pr=3000Mscf/D = 2000Example:

    Pwf = 300 psiPr = 800 psiMscf/D = 300

    Mscf/D 2000A=12FTP = 1500TR 1 37A = 134

    FTP = 100 psiTR = 3.77(134^.5 x 100/14.5) -.172 = 1.77 ... or actual predicted crit vel

    TR = 1.37

    64

    velis 1.77 times the Turner value...

  • Critical Rates at Low PressuresCritical Rates at Low Pressures

    CRITIAL RATE VS. FTP, DIA=1.995

    1.4

    1

    1.2

    1.4

    A=1 TURNER

    0 6

    0.8

    1

    M

    M

    S

    C

    F

    /

    D

    A=100A=200A=50

    A l

    0 2

    0.4

    0.6

    M

    COLEMAN

    A values denote using Shell-Nam model

    0

    0.2

    0 200 400 600 800 1000

    FTP PSI

    Nam model

    65

    FTP, PSI

  • Conclusions on Critical Rate at Low PressureConclusions on Critical Rate at Low Pressure

    Depending on the A parameter, Shell Nam predicts different degrees of rate in addition to either Turner or Exxon at low pressuresor Exxon at low pressures

    A Stripper Well Consortium Project will examine critical velocity requirements at low pressure and compare the data to existing methods

    66

  • Critical Rate with assumptions includedCritical Rate with assumptions included

    Using Turner s simplified assumptions of 20 and 60 dynes/cm surface tensions for condensate and water, 45 and 67 lbm/cu.ft. densities, gas gravity of 0.6 and 120 F for temperature gives:

    4/1

    2/1

    4/1

    )0031()p0031.( = Cv criticalgas 2/1, )p0031(.criticalgas

    Turner: C= 5.34 water, or 4.02, condensate, p >1000 psiColeman: C= 4.43, water, or, 3.37, condensate, p < 1000 psi

    67

    , , , , , p p

  • Critical Velocity Cast as Critical RateCritical Velocity Cast as Critical Rate

    AvpDMM fQ criticalgas ,

    06.3)/(

    zTDMMscfQ criticalgascritg +=

    ,, )460(

    )/(

    ftareaAwhere= 2

    :

    psiapftareaA

    == ,

    FTpp

    =o

    68

    factorilitycompressibz =

  • Turner Critical RateTurner Critical Rate

    DMM fAPVg /

    067.3DMMscf

    ZTq gg /)460( +=

    2/1

    4/12 )0031.45(0676.)/( PdPDMMscfq ticondensatet= 2/1, )0031(.)460()/( PZTDMMscfq condensatet +

    4/12 )003167(0890 PdP2/1, )0031(.)0031.67(

    )460(0890.

    )/(PP

    ZTdPDMMscfq tiwatert

    +=

    69

  • Divide rate by 1 2 for

    Turner Critical Rate: Water: SimplifiedTurner Critical Rate: Water: SimplifiedDivide rate by 1.2 for Exxon correlation which is really better for pressures lower than 1000 psi

    P is psia in below

    Turner Unloading Rate for Well Producing Water

    30004-1/2 OD 3.958 ID

    2000

    2500

    )

    3-1/2 2.992

    2-7/8 2.441

    2-3/8 1.995

    2-1/16 1.751

    1000

    1500

    R

    a

    t

    e

    (

    M

    c

    f

    d

    0

    500

    70

    0 50 100 150 200 250 300 350 400 450 500

    Flowing Pressure (psi)

  • Example: Critical-2 3/8s, 100 psia, 320 Mscf/DExample: Critical-2 3/8s, 100 psia, 320 Mscf/D

    Turner Unloading Rate for Well Producing Water

    2500

    30004-1/2 OD 3.958 ID

    3-1/2 2.9922-7/8 2 441

    2000

    M

    c

    f

    d

    )

    2 7/8 2.441

    2-3/8 1.995

    2-1/16 1.751

    1000

    1500

    R

    a

    t

    e

    (

    M

    0

    500

    71

    00 50 100 150 200 250 300 350 400 450 500

    Flowing Pressure (psi)

  • Problem One: Critical Velocity Problem: Concept: Critical velocity charts like the below are usually used with the surface tubing pressure and may indicate if the well is above or below critical flow. However it can also be used to indicate what you might consider as severalHowever it can also be used to indicate what you might consider as several approaches to solve the problem, if it exists.

    Turner Unloading Rate for Well Producing Water

    1500

    2000

    2500

    3000

    e

    (

    M

    c

    f

    d

    )

    4-1/2 OD 3.958 ID

    3-1/2 2.992

    2-7/8 2.441

    2-3/8 1.995

    2-1/16 1.751

    0

    500

    1000

    0 50 100 150 200 250 300 350 400 450 500

    Flowing Pressure (psi)

    R

    a

    t

    e

    Given 3 tubing and Pwh = 300 psi and a 1 MMscf/D rate.

    1 - Would 2 7/8s tubing put the well above critical flow?2 - To what pressure would you have to lower the wellhead pressure in order to

    obtain above critical flow (with a compressor and 3 inch tubing)3 - If foam reduces the critical flow rate by a factor of 2/3rds. Leaving 1/3 of

    original critical rate for 3 at 1 MMscf/D would you then be above critical

    72

    original critical rate for 3 at 1 MMscf/D would you then be above critical flow?

  • Critical: Canadian Units Critical: Canadian Units

    73

    Weatherford

  • Problem One: Critical Velocity Problem: Canadian Version: Concept: Critical velocity charts like the below are usually used with the surface tubing pressure and may indicate if the well is above or below critical flow. However it can also be used to indicate what you might consider as severalHowever it can also be used to indicate what you might consider as several approaches to solve the problem, if it exists.

    Given 3 tubing and Pwh = 689 kPa and a 28.3 E3m3/day rate.

    1 - Would 2 7/8s tubing put the well above critical flow?2 - To what pressure would you have to lower the wellhead pressure in order to

    obtain above critical flow (with a compressor and 3 inch tubing)3 - If foam reduces the critical flow rate by a factor of 2/3rds. Leaving 1/3 of

    original critical rate for 3 at 28 3 E3m3/day would you then be above

    74

    original critical rate for 3 at 28.3 E m /day would you then be above critical flow?

  • Coleman Critical Rate: WaterColeman Critical Rate: Water

    Coleman Unloading Rate for Well producing Water2500

    2000 4-1/2 OD 3.958 ID3-1/2 2.9922-7/8 2.441

    1000

    1500

    R

    a

    t

    e

    (

    M

    c

    f

    d

    )

    2-3/8 1.9952-1/16 1.751

    500

    00 50 100 150 200 250 300 350 400 450 500

    Flowing Pressure (psi)

    75

  • Coleman: Water: Coiled TubingColeman: Water: Coiled Tubing

    Coleman Unloading Rate for Well Producing WaterCoiled Tubing

    800

    900

    1000

    2.875 OD 2.499 ID

    2.375 2.063

    2.00 1.732

    1 50 1 25

    400

    500

    600

    700

    R

    a

    t

    e

    (

    M

    c

    f

    d

    )

    1.50 1.25

    1.25 1.06

    100

    200

    300

    400

    R

    0

    100

    0 50 100 150 200 250 300 350 400 450 500

    Flowing Pressure (psi)

    76

  • Turner: WaterTurner: Water

    Turner Unloading Rate for Well Producing Water3000

    2000

    2500

    4-1/2 OD 3.958 ID3-1/2 2.9922-7/8 2.4412-3/8 1.9952-1/16 1.751

    1500

    2000

    R

    a

    t

    e

    (

    M

    c

    f

    d

    )

    500

    1000

    00 50 100 150 200 250 300 350 400 450 500

    Flowing Pressure (psi)

    77

  • Turner: Water: Coiled TubingTurner: Water: Coiled Tubing

    Turner Unloading Rate for Well Producing WaterCoiled Tubing

    1000

    1200

    2.875 OD 2.499 ID2.375 2.0632.00 1.732

    600

    800

    e

    (

    M

    c

    f

    d

    )

    1.50 1.251.25 1.06

    400

    R

    a

    t

    e

    0

    200

    0 50 100 150 200 250 300 350 400 450 500

    Fl i P ( i)

    78

    Flowing Pressure (psi)

  • Above Critical at Surface: Below Surface? Above Critical at Surface: Below Surface?

    Critical Flow Rate - Pressure with GrayCritical Flow Rate - Pressure with GrayCritical Flow Rate - Pressure with Gray0

    1

    2

    Depth (1000 ft MD)Depth (1000 ft MD)Depth (1000 ft MD)Critical Flow Rate Pressure with GrayCritical Flow Rate Pressure with GrayCritical Flow Rate Pressure with Gray

    Pfwh 312 psigFormation Gas Rate 2153 MscfdCondensate .0 bbl/MMscfWater .5 bbl/MMscf

    2

    3

    4

    5

    Tubing String 1

    5

    6

    7

    8

    ACTUAL

    800 1000 1200 1400 1600 1800 2000 2200 2400 2600 2800 3000 3200 3400 3600

    8

    9

    Gas Rate (Mscfd)Gas Rate (Mscfd)Gas Rate (Mscfd)prob2prob2prob2

    79

  • Problem 2: Critical with DepthProblem 2: Critical with Depth

    Background: Usually the critical rate is evaluated at the top of the tubing. However the formulas for critical rate can apply at any point in the tubing. Program PRODOP calculates the required critical rate vs. depth and shows the user if the actual rate is above or below the critical over the entire tubing string.

    WHT 100F (37 8 C) BHT 245 F (118 3 C)WHT: 100F (37.8 C) BHT: 245 F (118.3 C) Gas Rate: 555 Mscf/D (15.7 E3m3/d or 15700 m3/d) Condensate rate: 7.7 bbl/MMscf ( 43.26 m3/MMm3/d)Water rate: 111 bbl/MMscf (623.6 m3/MMm3/d)( )GG: .65 API: 43.3 WG: 1.03Tubing Pressure: 100 psi (689.4 kPa)2 3/8s to 9450 feet (60.325mm to 2881 meters) 1.8530 (47.066mm) ID Roughness: smooth pipe 0018 ( 04577mm)Roughness: smooth pipe .0018 (.04577mm)

    Run on PRODOP and determine the critical rate required over the tubing depth vs. the actual rate.

    80

    tubing depth vs. the actual rate.

    Note: you can adjust Prodop to SI units. Same for Snap

  • Problem 8: Critical in Casing and Tubing?Problem 8: Critical in Casing and Tubing?P bl Ei ht C iti l Fl ith D th d C i Fl t B tt f W llProblem Eight: Critical Flow with Depth and Casing Flow at Bottom of Well Concept: Tubing set a little above the perforations. Some casing flow above the

    perforations. Check critical flow vs. actual flow for flow in the casing and in the tubing.

    Run on PRODOP:Run on PRODOP:WHT: 100F (37.8 C)BHT: 245 F (118.33 C)Gas Rate: 444 Mscf/D (12.57 E3m3/d or 12565 m3/d) Condensate rate: 7.7 bbl/MMscf (43.26 m3/MMm3)Condensate rate: 7.7 bbl/MMscf (43.26 m /MMm )Water rate: 307 bbl/MMscf (1724 m3/MMm3)GG: .65API: 43.3WG: 1.03WG: 1.03Tubing Pressure: 100 psi (689 kPa)1.3151 to 9450 (33.4 mm to 2881meters) 0.9570 ID ( 24.3 mm ID)5 casing to 10,000 (139.7 mm casing to 3048.78 meters)Roughness: smooth pipe 0.0018 (.0457 mm)Roughness: smooth pipe 0.0018 (.0457 mm)Is well loaded at surface of tubing?Is well loaded at bottom of the tubing?Is well loaded in the casing? What is critical rate for the casing flow? Average rate?

    81

    What is critical rate for the casing flow? Average rate?

  • Problem: Casing or Tubing Flow:Problem: Casing or Tubing Flow:Problem Ten: Tubing or Casing Flow? 2 3/8 tubing 1.995 ID (60.325mm tubing 50.673mm ID)4 casing 3.958 ID (114.3 mm casing 100.533 mm ID)6000 depth (1829.3 meters)22 bbl/MMscf condensate (123 m3/MMm3)22 bbl/MMscf water (123 m3/MMm3)WG 1.03Condensate: 40 APIGG: .65Pwh: 100 psi (689 kPa)BHT: 150F (65.56 C)WHT: 100F (37.78 C)( )Rate: 1400 Mscf/D (39620 M3/D)Compare in PRODOP or SNAP the calculated flowing BHPs for

    tubing and casing flow and critical rates and stable rates in

    82

    each.

  • Problem 12: Tapered Tubing StringProblem 12: Tapered Tubing Stringt t bi i d th d th f h P bl T l T d T bi St itwo tubing sizes and the depths of each. Problem Twelve: Tapered Tubing String: Background: Usually the critical rate is evaluated at the top of the tubing. However

    the formulas for critical rate can apply at any point in the tubing. Program PRODOP calculates the required critical rate vs. depth and shows the user if the actual rate is above or below the critical over the entire tubing string. g g

    WHT: 100F (37.78 C)BHT: 245 F (118.3 C)Gas Rate: 375 Mscf/D ( 10618 M3/d)Condensate rate: 7.7 bbl/MMscf (43.26 m3/MMm3)( )Water rate: 111 bbl/MMscf (623.6 m3/MMm3)GG: .65API: 43.3WG: 1.03Tubing Pressure: 100 psi or 689.4 kPa2 3/8s to 9450 1.8530 ID (60.325mm tubing to 2881m ) 47.066 mm ID Roughness: smooth pipe .0018 (.04572mm)If the bottom of the string has current flow blow critical, then insert a new string of g , g

    tubing in PRODOP so that flow will be above critical flow for the bottom of the string as well as the top of the string. Insert the largest but still smaller string to cover the bottom of the string (and little more depth for safety factor) such that flow over the entire depth of the well is above critical flow.

    Report the tapered string you determine and the

    83

    Report the tapered string you determine and the

  • Turner Critical: Smaller Tubing SizesTurner Critical: Smaller Tubing Sizes

    1000

    700800900

    1000

    t

    e

    ,

    m

    c

    f

    d

    400500600700

    d

    i

    n

    g

    R

    a

    t 2.3752.0161.90

    100200300400

    n

    U

    n

    l

    o

    a

    d

    1.66

    0100

    0 200 400 600 800

    M

    i

    n

    84

    Surface Pressure, PSIA

  • Critical Changes with InclinationCritical Changes with Inclination

    85

  • Critical Changes with InclinationCritical Changes with Inclination

    ( ) ( )( )[ ]907.1sin59341 38.025.025.0 glweNv ( )( )[ ]740767.0305934.1 2 = ggwe

    cv

    86

  • Question? Question?

    Does well liquid load when: Flowing? Shut-in?

    87

  • Question? Question?

    Does well liquid load in the: Casing? Tubing?

    88

  • Tubing size: Large-Loading, Small-FrictionTubing size: Large-Loading, Small-Friction

    There must be a balance between liquid loading and friction. You need enough velocity to be above critical velocity but not so much as to have too much frictiontoo much friction.

    89

  • Critical Questions: Which are 100% True?Critical Questions: Which are 100% True?Producing below the Critical Rate will cause the well to load up and quit flowing.Producing below the Critical Rate will cause the gwell to continue to flow but at a lower rate.Producing below the Critical Rate will damage the formationformation. Producing below the Critical Rate will not affect the production.Producing below the Critical Rate will create a higher pressure loss in the tubing and the well will either produce at a lower rate or could load up and die.

    90

  • Does well quit flowing when below critical? Does well quit flowing when below critical? Exxon said on average with their data, production was 40% lessSutton, et al., Marathon, SPE 80887 modeled flow with gas bubbling through static liquid column.

    91

  • Nodal Analysis: A Model of the Well Nodal Analysis: A Model of the Well

    92

  • Inflow to the node

    Nodal Analysis: TM of SchlumbergerNodal Analysis: TM of SchlumbergerInflow to the node

    PR P (upstream components press drops) = PnodeOutflow from the node

    Inflow

    Psep + P (downstream components press drops) = Pnode

    InflowOutflow

    P

    r

    e

    s

    s

    u

    r

    e

    93

    Rate

    P

  • Reservoir: Gas Inflow CurveReservoir: Gas Inflow Curve

    Reservoir Inflow curve often represented by:

    Inflow

    Q = C ( Pr2 Pwf2)n . (back pressure equation)

    Inflow

    P

    r

    e

    s

    s

    u

    r

    e

    94

    Rate

    P

  • Well Testing to Obtain Reservoir Inflow Well Testing to Obtain Reservoir Inflow

    Objective is to calculate reservoir inflow at varying flowing wellbore pressures (the IPR)

    Pr = average reservoir pressurePr = average reservoir pressurePwf = flowing well pressure at mid - perf depth or top of perforations

    PR

    PWF

    95

    Q

  • Well TestingWell Testing

    Desirable to have 3 or more flow rates with pressure and rates recordedUsually short duration hours or daysUsually short duration - hours or daysReservoir is often in transient flow during testingNeed to be able to evaluate short term tests toNeed to be able to evaluate short term tests to accurately predict long term (years) behavior

    96

  • Well TestingWell Testing

    Flow after FlowIsochronalM difi d I h lModified IsochronalLaminar Inertia Turbulence (LIT) MethodJones Blount & Glaze Method (SPE 6133)Jones, Blount & Glaze Method (SPE 6133)

    97

  • Pseudo Steady State Radial Flow for GasPseudo Steady State Radial Flow for Gas

    qsc= 703 x 10-6 kgh (PR2-Pwf2)/ gZT {ln(.472re/rw) + (st+Dq) }(2-44) Golan p 2-9 WPM

    qsc = gas flow rate, Mscfd,

    kg = permeability to gas, md,gh = reservoir thickness, ft.

    PR = average reservoir pressure, psia,

    g = gas viscosity at T, P=.5 (PR + Pwf), cpZ = gas compressibility factor at T, P

    T=reservoir temperature, R,

    re=drainage radius, ft, and,

    98

    rw=wellbore radius, ft.

    (st+Dq) =total skin plus pseudo skin due to turbulence

  • Deliverability Equations for GasDeliverability Equations for Gas

    Jones et al - DArcy pseudo-steady solution for turbulence effects

    P2R - P2WF = A qSC + B q2SC

    Rawlins and Schellhardt postulated that the it ff t ld b t d i thcomposite effect could be represented in the

    familiar gas well equation: q = C (P2 P2 )nqSC = C (P2R - P2WF)n

    99

  • Gas Well Back-Pressure EquationGas Well Back-Pressure Equation

    Gas Well Backpressure EquationqSC = C (p2R - P2WF)n

    Exponent n reflects total turbulence effects-reservoir and completion-For low turbulence n ~ 1-For low turbulence n ~ 1 -For high turbulence n ~ .5 C and n are determined from multipoint flow tests

    Flow after Flow IsochronalIsochronal Modified Isochronal (tests solve for constants in deliverability expressions)

    100

  • Flow After Flow TestFlow After Flow Test

    Start from shut - in condition Open choke and flow until gas rate and PWF stabilizeR d t d PRecord gas rate and PWFRepeat for at least three additional choke settings For best results P should be measured directlyFor best results, PWF should be measured directly with pressure bomb PWh can be used to calculate PWF but results are less reliable

    101

  • Conduct of Flow After Flow Tests Conduct of Flow After Flow Tests

    q1q2

    q3q4

    qsc

    q1

    Pr

    time

    P

    Pwf1

    Pwf3Pwf2

    102

    time

  • Flow After Flow Test CommentsFlow After Flow Test Comments

    Must have stabilized flow for all rates (less than .1 psi change is surface pressure in 15 min.

    Pseudo - stabilization (surface pressures stabilize before BHP fully stabilized) may occur

    If a well is tubing limited (high tubing friction)

    May be able to use static casing annulus pressure to determine stabilized flowdetermine stabilized flow

    103

  • Time to Pseudo Steady StateTime to Pseudo Steady State

    The time required for attain flow stabilization a circular drainage reservoir can be estimated fromcircular drainage reservoir can be estimated from

    950 C (1 - Sw ) r2etS =

    t =stabilization time, hoursit

    kS

    = porosity = viscosity k = perm , md

    C = is total compressibility 1/psi C = is total compressibility, 1/psi re= radius of drainage, ft

    Takes a long time for low k in the denominator

    104

  • Analysis of Flow after Flow Tests: OilAnalysis of Flow after Flow Tests: Oil

    Rewrite backpressure equation by taking log of both sides and rearranginglog (P 2 P 2) = (1/n) log (q ) (1/n) log(C)log (PR2 PWF2) = (1/n) log (qO) - (1/n) log(C)

    Plot log (PR2- PWF2) vs log (qO) -slopePlot log (PR PWF ) vs log (qO) slope = 1/n - intercept = log (C)/n

    105

  • Analysis of Flow After Flow Tests: GasAnalysis of Flow After Flow Tests: Gas

    Rewrite backpressure equation by taking log of both sides and rearranging

    log ( P2R - P2WF)=(1/n) log (qSC) - (1/n)log(C)

    Plot log (P2R - P2WF) vs log (qSC) slope = 1/n intercept = log (C) /n

    106

  • Flow After Flow Test Plot: GasFlow After Flow Test Plot: Gas

    10,000 Reflects a zero sandface pressure

    Reflects the

    1,0002 )

    sandfacepressure related to a particular back pressure0

    Absolute open flow

    (

    P

    r

    2

    -

    P

    w

    f

    2 pressure

    Slope = 1/n

    Sandface potential at

    1 10 10

    100

    Absolute open flow potential

    Sandface potential at the particular back pressure

    qsc

    107

    1 10 100

    qsc

  • Flow After Flow ExampleFlow After Flow ExampleDuration pwf, psia MMscf/D

    0 201 0.0

    3 196 2 733 196 2.73

    2 195 3.97

    2 193 4 44

    Back Pressure Plot0.01

    2 193 4.44

    4 190 5.5

    1 10

    w

    f

    ^

    2

    )

    /

    1

    0

    ^

    6

    0 001

    (

    P

    r

    ^

    2

    -

    P

    w

    108

    0.001

    MMscf/D

  • Back Pressure PlotBack Pressure Plot

    You should do a least squares curve fit of the points but you can just do a best straight line as shown previously. Once line is drawn, you can use any two

    )l ()l (

    previously. Once line is drawn, you can use any two points on the line to calculate n and C:

    )log()log()log()log(

    21

    222

    212

    wfrwfr PPPPqqn

    =ff

    qC = nwfR PP

    C)( 22

    109

  • Flow After Flow Example Flow After Flow Example

    Sample calculation: )log()log()log()log(

    21

    222

    212

    ff PPPPqqn

    =)log()log( 12 wfrwfr PPPP

    n=(ln(5.5)-ln(4.44)/ {ln(2012-1902) ln(2012-1932)}( ( ) ( ) { ( ) ( )}

    = (1.7-1.49)/ (8.36-8.06)=.2141/0.3108= .6888

    C = 5 5/(2012-1902)0.688 = 0173 MMscf/D/ psi2C = 5.5/(201 190 ) = .0173 MMscf/D/ psi

    So: q = .0173(Pr2 Pwf2)0.6888

    Check: q=.0173(2012-1902)0.688=.0173(4301).6888

    = 5 5 MMscf/D So equation duplicates

    110

    = 5.5 MMscf/D .. So equation duplicates point!!

  • 200

    Enter C and n to Nodal Program for Inflow

    150

    200

    g

    50

    100

    P

    r

    e

    s

    s

    u

    r

    e

    ,

    p

    s

    i

    g

    0 5000 10000 15000 20000 25000 300000

    Gas Rate, Mscf/DInflow @ Sandface (1) Not Used Inflow (1) Outflow (A) Not Used Not Used Not Used Not Used

    11

    Not Used Not Used Not Used Not Used Not Used Not Used Cond Unloading Rate Water Unloading Rate Max Erosional Rate Reg: james f lea - ttu

    111

    Q aof=.01573(2012)0.7= 26.37 Mscf/D

  • Problem 18: Find C and n from test dataProblem 18: Find C and n from test dataP bl Ei ht (18)Problem Eighteen (18):

    Gas Back Pressure Equation: Normally we want a four point test for determining the gas flowNormally we want a four point test for determining the gas flow

    equation and the AOF. Assume we have only the below 2 points.

    What is C, MMscf/D/psi2n ? (or in m3/D / (kPa2n)What is nDoes this well exhibit any turbulence or is it all Darcy Flow? What is the AOF in MMscf/D? (Q when Pwf=0)F i d th b k ti iFor a reminder the back-pressure equation is:Remember to separate variables:

    Pwf, psia MMscf/D or Pwf, kPa E3m3/D201 0 13485 6 0201 0 13485.6 0193 4.44 1330.5 125.6190 5.5 1309.86 155.6

    Data: two point test

    112

    Data: two point test

  • Tubing Outflow Curve:Tubing Outflow Curve:

    At low rates, liquid builds up in the tubing and requires more pressure to flow

    s

    s

    u

    r

    e

    Tubing J-Curve(Use various correlations, Gray, etc. )

    FrictionLiquidho

    l

    e

    p

    r

    e

    s

    FrictionLiquidBuildup

    D

    o

    w

    n

    -

    h

    113

    Rate

  • Nodal Analysis: StabilityNodal Analysis: Stability

    114

  • Liquid Loading in Casing Below EOTLiquid Loading in Casing Below EOT

    Critical Gas Rate Pressure with GrayC iti l G R t P ith GCritical Gas Rate Pressure with Gray

    0

    1

    Depth (1000 ft MD)Depth (1000 ft MD)Depth (1000 ft MD)

    Critical Gas Rate - Pressure with GrayCritical Gas Rate - Pressure with GrayCritical Gas Rate - Pressure with Gray

    Pfwh 125 psigGas Rate 2000 mscf/dCond 0 bbl/MMscf

    2

    3

    4

    5

    Cond .0 bbl/MMscfWater 15.0 bbl/MMscf2.375" at 10000 ftGray Correlation

    Unloading

    5

    6

    7

    8Loading

    Current Rate

    0 800 1600 2400 3200 4000 4800 5600 6400 7200

    9

    10

    11

    Rate (mscf/d)Rate (mscf/d)Rate (mscf/d)

    Loading

    115

    Rate (mscf/d)( )( )

  • J-Curve Tubing PerformanceJ-Curve Tubing Performance

    Liquid Loading J-Curve with GrayLiquid Loading J-Curve with GrayLiquid Loading J-Curve with Gray

    820860900

    Flowing BHP (psig)Flowing BHP (psig)Flowing BHP (psig) Tbg - Critical Rate (Min BHP) = 547 mscf/dPfwh 125 psigCond .0 bbl/MMscfWater 15.0 bbl/MMscf2.375" at 10000 ft

    Liquid loading occurs when gas rate is too low to

    620660700740780

    2.375 at 10000 ft

    Stable flowHigh frictionMay have some liquid buildup

    Unstable flowHigh liquid buildup

    efficiently remove the produced liquidsThis results in unstable flow behavior and

    460500540580620 behavior and

    potential logging off of the well

    0 200 400 600 800 1000 1200 1400 1600 1800 2000340380420460

    Gas Rate (mscf/d)Gas Rate (mscf/d)Gas Rate (mscf/d)

    Optimal Operation

    116

    Gas Rate (mscf/d)Gas Rate (mscf/d)Gas Rate (mscf/d)

  • Liquid Loading Liquid Loading

    Liquid loadingLiquid loading occurs when gas rate is too low to

    1600

    1800 PSIAPSIAPSIANodal PlotNodal PlotNodal Plot

    S1 - Tubing Flow - Ptbg = 500 psigS2 - Tubing Flow - Ptbg = 500 psigS3 - Tubing Flow - Ptbg = 500 psigPbar = 1450 psiaPbar = 1250 psia Pbar = 1050 psiaStable Flow

    Cond .0bbl/MMscfWater 15.0bbl/MMscf

    efficiently remove the produced liquids 1000

    1200

    1400

    1600S1 - 2.375" at 10000 ft S2 - 1.9" at 10000 ft S3 - 1.66" at 10000 ft Gray Correlation

    liquidsThis results in unstable flow b h i d 200

    400

    600

    800

    behavior and potential logging off of the well

    0 100 200 300 400 500 600 700 800 900 1000 1100 1200 13000Gas Rate (mscf/d)Gas Rate (mscf/d)Gas Rate (mscf/d)

    117

  • Nodal Analysis: Tubing Size and Flow RateNodal Analysis: Tubing Size and Flow Rate

    118

  • Predictions of Tubing Turnup: Biggest ErrorPredictions of Tubing Turnup: Biggest Error

    119

  • Nodal Analysis Summary: Can Study Below:Nodal Analysis Summary: Can Study Below:

    Effects of diameter sizeEffects of surface pressure (compression)Eff t f h t l d th t biEffects of where to land the tubingEffects of flow line pressure dropEffects of adding artificial lift such as gaslift orEffects of adding artificial lift such as gaslift or pumping methodsEffects of completion such as Shots-Per-Foot for a perforation jobEtc.

    120

  • Problem 11 Problem 11

    121

  • Problem 11 Continued: Duplicate below? Problem 11 Continued: Duplicate below?

    122

  • Problem 13: Inflow with no well testsProblem 13: Inflow with no well testsP bl Thi t D t i P f ith NO W ll T tProblem Thirteen: Determine Performance with NO Well Tests: Use PRODOP use Modified Gray for multiphase flow gradient. Although it is best to have flow-after-flow tests or for tighter wells, Isochronal and for still tighter (lower

    permeability) , modified Isochronal tests, and yet tighter analyze reservoir performance using reservoir models, and type curves, it is possible to estimate reservoir performance using numbers from our tubing flow correlations to build a reservoir expression for q=C(Pr^2-Pwf^2)^n. The accuracy of this method depends on the correlation used in the tubing but in many cases is sufficient to allow modeling of a gasdepends on the correlation used in the tubing but in many cases is sufficient to allow modeling of a gas well or liquid loaded gas well.

    Tubing ID: 1.867No casing flow. Depth: 5000Use GrayWell is flowing @ 552 Mscf/D(15621 m3/D) The Pr is 785 psia (5441 kPa) given here and always required

    either guess, measured, or from P vs. time decline curve. Pwh: 200 psigGG: .7WG: 1.02100% water100% water50 bw/MMscfTwh: 100BHT: 150 FWhat is the value of Pwf calculated using 552 Mscf/D (the current flow point). What is value of C in back pressure equation for N=1?p qWhat is value of C in back pressure equation for N=0.5What is AOF for N=1 in back pressure equation?What is AOF for N=0.5 in back pressure equation?If surface pressure reduced to 50 psia from compression, what is rate for N=1?If surface pressure reduced to 50 psia from compression what is rate for N=0.5? Thi h ld b k t th fl t f th d d P h i i d d t d ll t t f C

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    This should bracket the flow rate for the reduced Pwh using compression and you do not do well tests for C and N using flow-after-flow or any tests. But you do rely on the flowing BHP at the given rate to be calculated or measured correctly.

    You can do same to evaluate different tubing sizes or different WHPs or other conditions.

  • QuestionQuestion

    Based on the unloading curve, should you choke a well to prevent loading?

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  • Effects of ChokeEffects of Choke

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  • Choke Gas Wells for Help With Loading? Choke Gas Wells for Help With Loading?

    However more recent evidence shows a choke may t d t bl fl b l iti l flextend stable flow even below critical flow

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  • Select Solution to Loaded Well: Problem 7Select Solution to Loaded Well: Problem 7St bilit C iti l Fl P bl P blStability or Critical Flow Problem Problem: Concept: Dewatering can be solved by several approaches. Here you are asked to investigate some possibilities to see if

    the Nodal Predications can be made to show stable flow although it may still be below critical.GG: 0.7230 bbls total /MMscf25% WC1.05 WG52 condensate APITubing: 9000 , 2 3/8sPwh: 1000 psiBHT 190 FBHT: 190 FTwh: 95FWell Test Data: Pr: 3600psiRates, Mscf/D Pwfs, psi225 3000225 3000275 2790325 2350390 1910Simulations Requested: Run as isRun with compression, with Pwf 800,600,400,200,100 and 50 psiRun with smaller tubing 1.095 IDRun with 12/64s choke at surfaceComment on each situation with respect to the fact it is solution or not depending on whether or not the

    minimum in the tubing curve is to the left of the intersection of the tubing and reservoir curve or not?? Also note where a Turner Critical Rate would be

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    Also note where a Turner Critical Rate would be.

  • Inflow for Liquids (Oil and Water)Inflow for Liquids (Oil and Water)

    For reference at this point two commonly used equations for liquid inflow, BPD are introduced.PI is for liquids coming into the well in absence ofPI is for liquids coming into the well in absence of any gasThe Vogel IPR is for the inflow of liquids, BPD, along with gas flowThe equation for PI and IPR are shown on the next two slidestwo slides We will use the liquid inflow equations when dealing with pumps and other lift techniques.p p q

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  • Productivity Index (PI) BPD FlowProductivity Index (PI) BPD Flow

    Simplest and most widely used relationship

    Straight Line PI

    1000

    1200

    1400

    1600

    s

    i

    )relationshipStraight linePI often called J in

    0

    200

    400

    600

    800

    1000

    P

    r

    e

    s

    s

    u

    r

    e

    (

    p

    s

    some text booksUnits stbpd/psiN t li bl t

    0 200 400 600 800 1000 1200

    Rate (STBLPD)Test Point PI Test Point

    Not applicable to gas wells )(Pr Pwf

    QPI =

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  • Vogels Equation for Liquid Production when some gas is also flowing: Flow belowis also flowing: Flow below the bubble point

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  • Composite IPR: Vogel/PI matched at PbComposite IPR: Vogel/PI matched at Pb

    Vogel

    Pb=Pr

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    Progression from PI to Vogel as in put Pb changes

  • Vogel: BPD Flow Vogel: BPD Flow

    As watercut increases the IPR may approach PI modelPI model becomes straight line

    rather than curved

    Similarl skin effects orSimilarly skin effects or additional gas may cause the IPR to move to

    the left become more curved

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