lesson 14 air, gas, mist cont

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  • 8/13/2019 Lesson 14 Air, Gas, Mist Cont

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    ATMPETE 625ATM

    ATM ATMHarold Vance Department of

    Petroleum Engineering

    Lesson 14

    Air, Gas, and Mist Drilling

    Read: UDM Chapter 2.1 - 2.4

    pages 2.1-2.74

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    ATMPETE 625ATM

    ATM ATMHarold Vance Department of

    Petroleum Engineering

    Circulating Pressures

    Calculating

    standpipe pressure

    starts withpredicting the

    pressure just below

    the bit, and workingyour way back to

    the surface

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    ATMPETE 625ATM

    ATM ATMHarold Vance Department of

    Petroleum Engineering

    Bit Pressure Drop

    As air flows through the jets, it expands in

    response to the decrease in pressure and its

    velocity increases

    Once the pressure drop exceeds a certain

    level, the air velocity reaches the prevailing

    speed of sound.

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    ATMPETE 625ATM

    ATM ATMHarold Vance Department of

    Petroleum Engineering

    Bit Pressure Drop

    At this point, the air cannot expand any

    faster and the upstream pressure becomes

    independent of the downstream pressure.

    This implies that under sonic discharge

    conditions the standpipe pressure is

    independent of the annular pressure

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    ATMPETE 625ATM

    ATM ATMHarold Vance Department of

    Petroleum Engineering

    Bit Pressure Drop

    b

    k

    k

    b

    a

    P

    kP

    P

    89.1Pand

    1.4kair,For

    olumeconstant vatthattopressure

    constantatheatspecificofratiok

    pressuredownstreamP

    psiaflow,sonicofonsetat thepressureupstreamP

    1

    2

    :isgasesidealinflowsonicofonsetfor theconditionThe

    a

    b

    a

    1

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    ATMPETE 625ATM

    ATM ATMHarold Vance Department of

    Petroleum Engineering

    Bit Pressure Drop

    If the upstream pressure is more than 1.89

    times the annulus pressure beneath the bit,

    flow through the bit will be sonic.

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    ATMPETE 625ATM

    ATM ATMHarold Vance Department of

    Petroleum Engineering

    Upstream bit pressure - sonic

    flow

    2

    a

    n

    5.0

    1

    1

    ft/s32.17constant,nalgravitatiog

    air)for(1gravitygasS

    airforRlbf/lbm-ft53.3constant,gasuniversaltheR

    Rbit,theaboveatureair temperT

    sq.in.nozzles,bittheofareatotalA

    lbm/sinairofrateflowmassG

    1

    2

    k

    k

    a

    n

    akSgk

    RT

    A

    GP

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    ATMPETE 625ATM

    ATM ATMHarold Vance Department of

    Petroleum Engineering

    Upstream bit pressure

    sub-sonic flow

    1

    22

    2

    a2

    11P

    :bybitebeneath thpressureannulus

    theandrateflowmassthetorelatedisbit

    theabovepressurethesonic,-subremains

    jetsethrough thvelocityflowairtheIf

    k

    k

    bn

    bb

    PgkSATGkRP

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    ATMPETE 625ATM

    ATM ATMHarold Vance Department of

    Petroleum Engineering

    Upstream bit pressure

    sub-sonic flow

    lbm/cu.ft.STP,at0.0764

    lbm/cu.ftSTP,atdensitygas

    Rbit,thebelowretemperatu

    60

    236.01P

    :becomesair thisfor

    air

    g

    5.3

    22

    2

    a

    b

    g

    bn

    bb

    T

    QG

    PA

    TGP

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    ATMPETE 625ATM

    ATM ATMHarold Vance Department of

    Petroleum Engineering

    Upstream bit pressure

    sub-sonic flow

    sonicisjetsthe

    throughflowifbittheabovethatlower than

    17%elyapproximatbebit willthebenow

    atureair temperabsolutethat theIndicating

    T

    :fromestimatedbecandecrease

    retemperatuthebehavior,idealAssumingbit.the

    throughexpandsitascoolsairgcirculatinThe

    1

    b

    k

    k

    a

    baP

    PT

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    ATMPETE 625ATM

    ATM ATMHarold Vance Department of

    Petroleum Engineering

    Standpipe pressure

    ft.g,drillstrintheofdiameterinternal

    10625.1

    3.53

    1

    333.5

    26

    /2

    /222

    i

    i

    Th

    Th

    avas

    D

    D

    Q

    S

    e

    eTPP

    av

    av

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    ATMPETE 625ATM

    ATM ATMHarold Vance Department of

    Petroleum Engineering

    Steps to predicting standpipe

    pressure Assess whether flow through bit is sonic or

    sub-sonic

    If sonic, the pressure above the bit is

    determined with equation 2.21

    This value is used in equation 2.25 to

    predict standpipe pressure

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    ATMPETE 625ATM

    ATM ATMHarold Vance Department of

    Petroleum Engineering

    Steps to predicting standpipe

    pressure If flow is sub-sonic, the annulus pressure

    below the bit must be first predicted

    (Angels analysis, etc) using equation 2.12. The pressure above the bit is determined by

    equation 2.23

    This value is used in Equation 2.25 todetermine standpipe pressure

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    ATMPETE 625ATM

    ATM ATMHarold Vance Department of

    Petroleum Engineering

    Important point

    When air drilling, large changes in annulus

    pressure may result in smaller changes in

    standpipe pressure, or in the case of sonicflow through the bit, no change in standpipe

    pressure at all.

    Hole problems that lead to an increase inannulus pressure may be indicated by small

    changes in standpipe pressure.

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    ATMPETE 625ATM

    ATM ATMHarold Vance Department of

    Petroleum Engineering

    Important point

    It is very important to monitor the standpipe

    pressure closely and react promptly to

    unanticipated changes.It is important to know if flow through the bit

    is sonic or not.

    If flow is sonic, standpipe pressure will notchange with changes in annulus pressure

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    ATMPETE 625ATM

    ATM ATMHarold Vance Department of

    Petroleum Engineering

    Example

    8.1/2 hole at 6000 drilled with 4 1/2

    drillpipe air rate is 1400 scfm. Penetration

    rate ranges up to 300 ft/hr. Bit has nonozzles in one example and 3- 14s in the

    other.

    TPETE 625T

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    ATMPETE 625ATM

    ATM ATMHarold Vance Department of

    Petroleum Engineering