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PETE 689 Underbalanced Drilling UBD

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PETE 689. Underbalanced Drilling (UBD) Harold Vance ... KOP = 2250 m. 120.6mm PDM. Elkton: Gas. BHP = 7.0 MPa. BHT = 80oC. Drilling Fluid. Water = 1000 kg/m3 ... – PowerPoint PPT presentation

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Title: PETE 689 Underbalanced Drilling UBD


1
PETE 689 Underbalanced Drilling (UBD)
Lesson 4 Air, Gas and Mist Drilling.
  • Read UDM - Chapter 2.1 - 2.4

Harold Vance Department of Petroleum Engineering
2
Air, Gas, and Mist Drilling
  • Gases used in UBD.
  • Dry air drilling.
  • Nitrogen drilling.
  • Natural gas drilling.
  • Mist drilling.
  • Optimized hole cleaning.

Harold Vance Department of Petroleum Engineering
3
Gases for UB Drilling
  • Air.
  • Cryogenic Nitrogen.
  • Membrane Nitrogen.
  • Engine Exhaust.
  • Natural gas.

Harold Vance Department of Petroleum Engineering
4
Gases for UB Drilling
Compressed Air
  • 79 N2 , 21 O2.
  • Corrosion.
  • Fire.
  • US3,000 Day.
  • Mod and Demob.

Harold Vance Department of Petroleum Engineering
5
Cryogenic Nitrogen
  • 40 year old technology.
  • Made as a by product of liquid oxygen
    manufacture.
  • Air replacement.
  • No corrosion.
  • No downhole fires.
  • 99.9 pure N2
  • 7K-40K US/day.

Harold Vance Department of Petroleum Engineering
6
Delivery
Cryogenic Nitrogen
  • Bottled gas.
  • Truck.
  • Storage tank on
  • a ship.

Harold Vance Department of Petroleum Engineering
7
Cryogen Nitrogen-Pumping Equipment
Stainless Steel
Carbon Steel
Vaporizer
Liquid Nitrogen (-320OF)
Pump
Gaseous Nitrogen to well 80OF, 0-10,000 psi
Harold Vance Department of Petroleum Engineering
8
Procedure
  • Determine Gas Volume Required.
  • Convert from Liquid Volume.
  • 1 gallon liquid nitrogen produces 93.12 ft3 of N2
    at SCP.
  • 1 m3 of N2 liquid produces 698 m3 of gas at SCP.

Harold Vance Department of Petroleum Engineering
9
Nitrogen Conversion Factors
  • 1 gal of liquid nitrogen is93.12 ft3 at STC.
  • 1 gal of liquid nitrogen is0.1333 ft3.
  • 1 liter of liquid nitrogen is698 litres of gas
    at STC.

Harold Vance Department of Petroleum Engineering
10
Cryogenic Nitrogen Cost
  • World-wide
  • 1-3 US /gal.
  • 0.10 US /scf.
  • Canada
  • 0.02 US /scf.
  • South America
  • 1.00 US /m3.

Harold Vance Department of Petroleum Engineering
11
UB Drilling Gas Alternatives
  • Nitrogen Membranes
  • 95 N2 , 3-5 O2.
  • Corrosion considerations.
  • Combustion considerations.
  • Approximately 15,000 US /day.
  • Mob/demob costs.

Harold Vance Department of Petroleum Engineering
12
Membrane Nitrogen
  • On site manufacture.
  • Dependent on concentration.
  • Directly proportional to pressure and rate.
  • Inversely proportional to gas partial pressure.
  • Driven by dissolution and diffusion.

Harold Vance Department of Petroleum Engineering
13
Individual Hollow Polmeric Gas Separation Fiber
Harold Vance Department of Petroleum Engineering
14
Individual Hollow Polmeric Gas Separation Fiber
Nitrogen Oxygen Water Vapor
Nitrogen
Oxygen and Water Vapor are Fast Gases which
quickly permeate the membrane, allowing Nitrogen
to flow through the fiber bores as the product
stream.
Harold Vance Department of Petroleum Engineering
15
N2 Generating Unit A Bundle Of Fibers
OXYGEN- ENRICHED AIR
FEED AIR
Harold Vance Department of Petroleum Engineering
16
Equipment Required
  • Compressor.
  • Filters-fibers will plug if the air is not
    filtered.
  • NPU or NGU.
  • Controller.
  • Booster(s).

Harold Vance Department of Petroleum Engineering
17
Membrane Nitrogen Production Unit
Filter and Air Separation Membrane System
Optional Booster Compressor
Feed Air Compressor
Drilling Rig
Harold Vance Department of Petroleum Engineering
18
1997 Nitrogen Unit.
  • N2 units with coolers.
  • 8x30x8 high
  • 23,000 psi
  • 1200 scfm N2 at 5 02

Harold Vance Department of Petroleum Engineering
19
Skid-Mounted Nitrogen Producing Unit (NPU)1998
Harold Vance Department of Petroleum Engineering
20
Weatherford 2000Nitrogen Generation Unit.
  • 1. N2 500-600 scfm.
  • 2. 2000 psi comp.
  • 3. 27 gph diesel.
  • 4. 8x20x16 high.
  • Nominal O2 5

1.
3.
2.
4.
Harold Vance Department of Petroleum Engineering
21
Nitrogen Membrane System 1999
2
3
5
1
Harold Vance Department of Petroleum Engineering
22
Procedure
  • Determine volume requirement.
  • Determine maximum oxygen concentration.
  • Determine effective volume from units.
  • Determine pressure requirement.

Harold Vance Department of Petroleum Engineering
23
Oxygen Concentration
  • Oxygen is only partially a valid concept for
    fire.
  • Ignition temperatures and water content play a
    big part.
  • Oxygen is important for corrosion.

Harold Vance Department of Petroleum Engineering
24
Recent Combustion Work
  • Testing
  • Alberta Research Council.
  • Counter claims of increased corrosion and
    combustion with membrane generated N2

Harold Vance Department of Petroleum Engineering
25
Minimum Oxygen for Combustion (with Methane)
Oxygen Required for Combustion
0 500 1000 1500
2000 2500 3000
Pressure (psia)
Harold Vance Department of Petroleum Engineering
26
Nitrogen Source SelectionCryogenic vs. Membrane
  • Location.
  • Job duration.
  • Volume requirement.
  • Pressure requirement.
  • Purity requirement.

Harold Vance Department of Petroleum Engineering
27
Operating Cost
  • Canada
  • USA
  • Crossover between cryogenic costs and membrane
    costs is generally about three days of operation.
  • Transportation and mobilization are big items.

Harold Vance Department of Petroleum Engineering
28
Cryogenic Nitrogen Operating Cost
  • Canada
  • 10,000 US /day minimum.
  • 40,000 US /day maximum.
  • (500-1800 scfm for 20 hrs/day).

Harold Vance Department of Petroleum Engineering
29
Flow Path
Harold Vance Department of Petroleum Engineering
30
Exhaust Gas Generating Unit 1980
Harold Vance Department of Petroleum Engineering
31
Exhaust Gas System
Harold Vance Department of Petroleum Engineering
32
Natural Gas for UB Drilling
  • Available.
  • No downhole fires.
  • No corrosion.
  • Low cost, long term contracts.

Harold Vance Department of Petroleum Engineering
33
Pressure
  • Determine requirement as for air, but allow for
    lesser specific gravity.
  • Delivery pressure set at source.

Harold Vance Department of Petroleum Engineering
34
Fuel Gas Group Gas Pipeline
Harold Vance Department of Petroleum Engineering
35
Natural Gas Pipeline Hook Up(Lyons, 1984)
Main Pipeline.
Auxiliary line to rig.
500 Psig
Flow to rig.
Choke/Controller
Pipeline Flow
Harold Vance Department of Petroleum Engineering
36
Natural Gas Concerns
  • May be pressure limited.
  • Heavier hydrocarbons repress foam so be sure that
    they are stripped out.

Harold Vance Department of Petroleum Engineering
37
  • Amoco Crossfield
  • Gas Recovery Project

Harold Vance Department of Petroleum Engineering
38
Amoco Crossfield 9-12 Well
88.9 mm Drill Pipe
Drilling Fluid Water 1000 kg/m3 Viscosity 1cP
KOP 2250 m
2350 m
177.8 mm Casing _at_ 2403 m
155.6 mm Openhole
120.6mm PDM
Elkton Gas BHP 7.0 MPa BHT 80oC
778 m
Target TMD 3181 m
Harold Vance Department of Petroleum Engineering
39
CrossfieldGas Recovery Project
  • Why it was done
  • Increasing public concerns over flaring.
  • Increasing EUB requirements for public
    consultation and notification.

Harold Vance Department of Petroleum Engineering
40
CrossfieldGas Recovery Project
  • Perfect fit with Amocos goal of
  • reducing greenhouse gas
  • emissions.
  • Try out new idea and technology.
  • Great plumbing setup.

Harold Vance Department of Petroleum Engineering
41
Gas Recovery Project
RBOPTM
Gas Flare System
Drilling Rig
Choke Manifold
Flare Knockout Vessel
Horizontal Separator
Feed Gas Compressors
Produced Gas Compressors
Gas Processing Unit
Feed Gas Line
Gas Gathering Line
Harold Vance Department of Petroleum Engineering
42
Compression Scrubber/Filter Units
Recovery Gas Compressors
Feed Gas Compressors
Scrubber/Filter Unit
Harold Vance Department of Petroleum Engineering
43
Flow Control Manifold
Harold Vance Department of Petroleum Engineering
44
Gas Scrubber Filter Unit
Harold Vance Department of Petroleum Engineering
45
Gas Recovery Summary
Harold Vance Department of Petroleum Engineering
46
Gas Recovery Summary
Gas Conserved
Gas Flared
16
  • Conserved 92.
  • Inc. Cost 170k US .
  • No need to optimize GLRs.
  • 75 MMCFD well.

14
12
10
8
6
4
2
0
10-Jul
12-Jul
14-Jul
16-Jul
18-Jul
20-Jul
22-Jul
24-Jul
26-Jul
Harold Vance Department of Petroleum Engineering
47
Crossfield Gas Recovery Project
  • Results
  • Estimated costs were 250k US , actual cost was
    170k US .
  • Conserved 92 of flow from the well.
  • Eliminated need to optimize the gas/liquid
    ratios.
  • 75 MMCFD storage well.

Harold Vance Department of Petroleum Engineering
48
Hole Cleaning
  • Optimizing hydraulics with gasses is primarily
    concerned with hole cleaning - getting the
    cuttings that are generated by the bit out of the
    hole.
  • With gas, rheological properties have very little
    to do with hole cleaning.
  • Hole cleaning with gasses is almost entirely
    dependent on the annular velocity.

Harold Vance Department of Petroleum Engineering
49
Drag and Gravitational Forces
  • Flowing air exerts a drag force on cuttings.
  • Gravitational force on the cuttings
  • Therefore there is a threshold velocity in which
    the cuttings will be lifted from the wellbore.
  • Threshold velocity increases with size of
    cuttings.

Harold Vance Department of Petroleum Engineering
50
Hole Cleaning
  • Compressibility of air (or gas) complicates
    matters.
  • Frictional pressure increases downhole pressure -
    decreases velocity downhole.
  • Suspended cuttings increase the density of the
    air, increasing downhole pressure.

Harold Vance Department of Petroleum Engineering
51
Hole Cleaning
  • Temperature has an effect on
  • volumetric flow rate.
  • We must pump at a velocity
  • high enough to remove the
  • cuttings, but not too high
  • where we waste energy.

Harold Vance Department of Petroleum Engineering
52
Hole Cleaning Criteria
  • Terminal Velocity Criteria.
  • Minimum Energy Criteria.
  • Minimum BHP Criteria.

Harold Vance Department of Petroleum Engineering
53
Terminal Velocity Criteria
  • Gray determined that the minimum velocity of the
    gas must be at least as high as the terminal
    velocity of the cutting in order to lift the
    cutting from the wellbore.
  • Vc Vf - Vt

Harold Vance Department of Petroleum Engineering
54
Terminal Velocity
?c ?f 3Cd ?f
Vt
4gdc

g gravitational acceleration, 32.17
ft/sec2 dc characteristic particle diameter,
ft. Cd drag coefficient. ?c density of
cuttings, lbm / ft3 ?f density of fluid, lbm/
ft3
Harold Vance Department of Petroleum Engineering
55
Terminal Velocity
dcT?c P
Vt 3.369
For flat cuttings
dcT?c P
Vt 4.164
For sub-round cuttings, T and P are at bottom
hole conditions in 0R and psia.
Harold Vance Department of Petroleum Engineering
56
Terminal Velocity
  • Terminal velocity in air drilling is determined
    mainly by
  • cutting diameter, shape, and density.
  • bottom hole temperature and pressure.

Harold Vance Department of Petroleum Engineering
57
Factors Effecting Vt
  • Shape (roundness).
  • Increased Size.
  • Increased Temperature.
  • Increased Density.
  • Increased Pressure.
  • Increases.
  • Increases.
  • Increases.
  • Increases.
  • Decreases.

Harold Vance Department of Petroleum Engineering
58
Terminal Velocity
  • As pressure increases Vt decreases.
  • As pressure increases Air velocity decreases.
  • If the mass flow rate of gas remains constant the
    local air velocity decreases with increasing
    pressure.
  • The air flow rate required to lift the cuttings
    increases with increasing BHP.

Harold Vance Department of Petroleum Engineering
59
Friction Pressure
?m
Eq. 2.5
fm Friction factor of the mixture
of air and cuttings. ?m Mixture density,
lbm/cu.ft. Vm Mixture velocity, ft/s. g
Acceleration due to gravity. Dh
Hole diameter, ft. Dp Pipe diameter, ft.
Harold Vance Department of Petroleum Engineering
60
Friction Pressure
fm a c
Weymouth quation.
0.14 ( Dh Dp) 0.333
a




Gou argued that Nikuradse is more correct.
1 a
2? Dh - Dp
1.14 0.86ln
? absolute roughness of the pipe.
Harold Vance Department of Petroleum Engineering
61
Friction Pressure
  • Mixture density of air and cuttings in the
    annulus is determined by the mass of the cuttings
    and the density of the air.
  • Air density is a function of the pressure.
  • Mass of the cuttings in the wellbore is a
    function of
  • ROP
  • Hole cleaning efficiency.

Harold Vance Department of Petroleum Engineering
62
Friction Pressure
  • Pressure drops down the drillstring and through
    the bit play a part in BHP due to temperature
    effects.
  • Temperature is also effected by
  • Formation temperature.
  • Influx of formation fluid (expansion of gas into
    the wellbore).
  • Mechanical friction.
  • Pressure.

Harold Vance Department of Petroleum Engineering
63
Required injection rates?
  • Relating downhole air velocities to surface
    injection rates is quite complex.
  • We need cuttings shape and size to determine
    terminal velocity.
  • Methods required knowledge of the cutting shape
    and size.

Harold Vance Department of Petroleum Engineering
64
Minimum Energy Criteria
  • Probably the most widely used criteria was
    developed by Angel in 1957.
  • Angel assumed that, for efficient cuttings
    transport downhole, the kinetic energy of the air
    striking each cutting should be the same as that
    of air giving efficient cuttings transport at
    standard pressure and temperature.

Harold Vance Department of Petroleum Engineering
65
Minimum Energy Criteria
1 2
1 2
?min V 2min
? stp V 2stp
Pmin Density of air (or gas) at the minimum
required downhole injection rate,
lbm/cuft. Vmin Air (or gas) velocity downhole,
ft/min. Pstp Density of air (or gas) at
standard temp and pressure, lbm/cuft. Vstp
Air (or gas) velocity at standard Temp and
pressure, ft/min.
Harold Vance Department of Petroleum Engineering
66
Minimum Energy Criteria
Pstp Pmin
Vmin Vstp
Harold Vance Department of Petroleum Engineering
67
Minimum Energy Criteria
  • Experience from shallow blast holes, drilled in
    limestone quarrying operations, indicated that
    cuttings were transported efficiently if the air
    velocity equaled or exceeded 3,000 feet per
    minute.
  • This is equivalent to Grays terminal velocity
    for flat cuttings with a diameter of 0.46 in. and
    for sub-rounded particles of 0.26 in.

Harold Vance Department of Petroleum Engineering
68
Minimum Energy Criteria
Angel computed the downhole air pressure with eq.
2.5
m ? m V 2m 2g (Dh Dp)
dP dL
?m
Wc Wa
?m ?a
1
Wc Mass of cuttings generated in a given
time the mass flow rate of cuttings,
lbm/min. Wa Mass of air flowing past any
point in the well in given time the mass flow
rate of air, lbm/min.
Harold Vance Department of Petroleum Engineering
69
Minimum Energy Criteria

2aG
abTs2 T abT2 G a Ts
G - a

Pb P2s-
Ps Surface air pressure, lbf/sq.ft,
absolute. Ts Surface temperature, 0F. G
Annular temperature gradient, 0F/100. T
Downhole temperature TsGh h Hole depth.
Harold Vance Department of Petroleum Engineering
70
Minimum Energy Criteria
SQ 28.8 . ROP . Dh2 53.3Q
a
S Gas specific gravity (air1) Q
Gas flow rate, scf/m ROP Penetration rate,
ft/hr
1.625 x 10-6Q2 (Dh Dp) 1.333 (Dh2
Dp2)2
b
Dh Hole diameter, ft. D2 Drillpipe
diameter, ft.
Harold Vance Department of Petroleum Engineering
71
Minimum Energy Criteria
This was combined with the cuttings transport
criterion defined in Eq 2.10 to deduce the
minimum air flow rate as a function of hole
depth, annular geometry, and penetration rate.
? stp ? min
Vmin Vstp
Eq. 2.10
Harold Vance Department of Petroleum Engineering
72
Minimum Energy Criteria
To simplify, the average downhole temperature can
be used to calculate BHP.
Harold Vance Department of Petroleum Engineering
73
Minimum Energy Criteria
This was solved numerically for the gas injection
rate required to give an annular velocity
equivalent in cuttings lifting power to air with
a velocity of 3000 ft/min. A series of charts was
generated for different combinations of hole
size, drillpipe diameter and penetration rates
Harold Vance Department of Petroleum Engineering
74
Minimum Energy Criteria
  • Qmin can be approximated by
  • Qmin Qo NH
  • Qo Injection rate (scfm) at zero
    depth that corresponds to an annular
    velocity of 3000 ft/min
  • N Factor dependent on the
    penetration rate (Appendix C)
  • H Hole depth, (thousands of feet).

Harold Vance Department of Petroleum Engineering
75
Appendix C
Data for calculating approximate circulation
rates required to produce a minimum annular air
velocity which is equivalent in lifting power to
standard air velocity of 3.000 ft/min. (Angel,
1957).
Harold Vance Department of Petroleum Engineering
76
250
200
150
Bottomhole Pressure (psia)
100
50
0
0 2000 4000 6000
8000 10000 12000
Depth (feet)
Harold Vance Department of Petroleum Engineering
77
80
70
60
50
Bottomhole Pressure (psia)
40
30
20
10
0
0 2000 4000 6000
8000 10000 12000
Depth
(feet)
Harold Vance Department of Petroleum Engineering
78
7-7/8 hole 3-1/2 drillpipe 6 drill
collars 3800 hole depth
Annular Bottomhole Pressuresin An Air Drilled
Hole-comparison Of Predictions And Measurements
Made While Circulating Off-bottom
Harold Vance Department of Petroleum Engineering
79
45
40
35
Bottomhole Pressure (psia)
30
25
20
  • 600 700 800 900
    1000 1100 1200 1300

  • Flow Rate (scfm)

Harold Vance Department of Petroleum Engineering
80
34
32
30
28
Bottomhole Pressure (psia)
26
24
22
20
  • 600 700 800 900
    1000 1100 1200 1300

  • Flow Rate (scfm)

Harold Vance Department of Petroleum Engineering
81
3.5
3
2.5
2
Required Rate of Air (scfm)
1.5
1
0.5
0
0 2000 4000 6000 8000 10000
12000 14000 16000 18000
Depth ( feet)
Comparison of air rates recommended by several
different cuttings transport analyses (after Guo
et al, 199412).
Harold Vance Department of Petroleum Engineering
82
Minimum BHP Criteria
Angel analysis does not predict a minimum BHP,
but gives a pressure that decreases monotonically
with decreasing air flow rate.
Annulus Pressure Drop
Annulus Pressure Drop
Annulus Air Velocity
The influence of air flow rate on annular
pressure drop (after Supon and Adewumi, 19915).
Harold Vance Department of Petroleum Engineering
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