1_2_acoustic liquid level measurement 2014
TRANSCRIPT
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Acoustic Liquid LevelMeasurement
Fundamentals
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TWM Computes
Distance to Fluid LevelFluidLevel
Gaseous Liquid
Flowing BHP
Gas
Liquid
Pump
Static
Reservoir
Pressure
Casing head pressureMicrophone
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1898
Batcheller
Patent
Locating stuck tubes
in pneumatic mailsystems.
Used Blank Pistol
Timed Round TripTravel Time to a
Stuck Tube
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Gas Gun Patent 1936 (Lehr and Wyatt)
Relation between
acoustic velocity, gas
composition, density
and pressure.
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DeptographC. P. Walker 1937
Objective: determine if there is liquid above the pump
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DeptographC. P. Walker 1937
Photographic Recording of Trace
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Walker Patent,
1937
Methods to Calculate
Depth to Liquid level:
1-Time to tubing catcher
and to liquid echoes.
2-Count collar echoes to
liquid level
3-Measure echo time andacoustic velocity in gas
with resonant tube.
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Sound Waves Basics
Sound waves are caused by a pressure change(increase or decrease) in a gas or liquid.
Sound waves propagate through the fluid at a speedcalled Acoustic Velocity.
Sound propagating in gas is reflected by solids or
liquids in the path of the wave. Sound propagating inside a tube is reflected by
changes in area (increase or decrease) of the tube.
The greater the change in area the larger is the
amplitude of the reflected wave and the smaller theamplitude of the transmitted wave.
The pressure of two waves arriving at the same timeat the microphone will add or subtract depending ontheir polarity.
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Traveling Surface Wave
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Echoes from Diameter (cross section area) Changes
Restrictions
inside tubing
Enlargements
in annulus
Acoustic trace
Acoustic trace
Time
Time
0 ft 4300 ft 5000 ft3000 ft
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Echoes due to Wellbore Area Changes
Hole Enlargement Liquid Flow Through Perfs Open Perfs
Enlargementscauseinversionof pulse echo polarity
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Liquid Leaking from Tubing @ 4056 feet
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Liquid Leaking from Tubing @ 4056 feet
Pump On
Pump Off
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Explosion
PulseGeneration
1. Gas gun chamber is charged to a pressure in excess of
the well pressure. Then the valve is opened quickly to
release gas into well.2. The increase in well pressure generates the pulse.
3. Utilizes an external gas supply to generate the acoustic
pulse.
Pressure Increases
5 psi during a short
time then pressure
wave propagates in
tube.Quick
opening
valve
300 psi 100 psi
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Remote Fired Gas Gun
Detailedschematics and
part numbers at
back of TWM
manual
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12 Volt
250 psi
50 psi
50 psi
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Implosion
PulseGeneration
1. Gas gun chamber pressure is bled to a pressure lower than the wellpressure. Then the valve is opened to quickly admit gas from well.
2. Uses the reduction in wells pressure to generate the sound pulse. Well
pressure should be greater than 100 PSI.
3. External gas supply not necessary.
Pressure
Decreases 5 psi
during a short
time thenpressure wave
propagates in
tube.
Quick
opening
valve 300 psi
100 psi
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Acoustic Pulse
Generators
Modern Acoustic Gas Guns:
1. Compact gas gun
2. Remote-fired gas guns
2aWired, 2b-Wireless
1. 5000 psi gas gun
2. 15000 psi gas gun
Obsolete Acoustic PulseGenerators Include:
dynamite cap
45 caliber blank
10 gauge black powder blank
Comparison of Energy fromGas Gun:
1. 45 caliber = 150 psi
2. 10 gauge = 300 psi
13
42b
2a
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TWM Explosion vs. Implosion Example
Data collected
on a shut-in gaswell JW-131using CompactGas Gun.
Compact GasGun charged to400 Psig togenerate thecompressionacoustic pulse.
Wells casingpressure of 205Psig used togenerateimplosion pulse.
400 Psig Explosion
205 Psig Implosion
RTTT
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Normal WellLiquid Level Echo
Polarity of echo same as polarity of pulse generated by gas gun
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Liquid Level Echo Round Trip Travel Time
RTTT = time for sound to travel from gun to LL and back
Question: what is the Distance to the Liquid Level ??
RTTT
A ti V l it i Ai
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Acoustic Velocity in Air
Speed of sound
1100 FT/Sec
Sound in air travels 1100 feet per second. If a person sees the flash and
hears the BOOM 5 seconds later, then the lightning struck 5500 feet away.
Lightning
See Flash
then, hear
BOOM.
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Acoustic Velocity of GasesDepends on P, T and Specific Gravity: (Charts for hydrocarbon gases)
Velocity = 1400 ft/sec Velocity = 785 ft/sec
400 psi
108 F
Distance to Echoes Calculated from a Known
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Distance to Echoes Calculated from a Known
Average Acoustic Velocity
Restrictions
Acoustic trace
0 ft
0 sect1= 6.000sec
L1= 6 x 1000/2
L1= 3000 ft
t2=8.6 sec
L2= 8.6 x 1000/2
L2= 4300 ftIn Wellbore:
P=100 psi
T=188 F
1.2 gravity
V=1000 ft/sec
A ti V l it d G G it C l l t d f
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Acoustic Velocity and Gas Gravity Calculated from a
Known Distance to Cross-sectional Area Changes
Restrictions
Acoustic trace
0 ft
t2=16 sec
V=8000 x 2/16
V = 1000 ft/sec
P=100 psi
T=188 F
V=1000 ft/sec
5000 ft 8000 ft
Gas gravity = 1.2
0 sec t1=10 sec
V=5000 x 2/10
V = 1000 ft/sec
E l i
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Shot
Liquid
Collar
Collar
Collar
Collar
Collar
Bang!
Explosion
PulseImplosion
Pulse
Change in cross-sectional
area at tubing
couplings cause
sound waves to
partially reflect back
to microphone
Number of collar echoes
per unit time is a
measure of the
acoustic velocity of
the gas in that section
of the well.
Echoes in Well
1 second sec/)/(*sec)/( ftJtftJts
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Count Echoes from
Tubing Collars Ideally should count all
echoes from surface toliquid level and givedepth to liquid asnumber of tubing
joints.
In practice need toextrapolate collarcount since the
amplitude of echoesdecreases to wellnoise level and collarechoes becomeindistinguishable from
noise.
E l i
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Shot
Liquid
Collar
Collar
Collar
Collar
Collar
Bang!
Explosion
PulseImplosion
PulseTWM Adjusts
Echo Polarity
For consistency with
established practice
TWM always showsrestr ic t ions as
down kicks and
enlargements as
up
kicks provided
the shot type:
Explosion or
Implosion is
enteredin data file.
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Processing of Acoustic Reflections in TWM
Reflected Pulsecaused byDECREASE in thecross-sectionalarea IS displayedas an downwardkick on theacoustic trace.
Shot fired
Reflected Pulse
caused byINCREASE in thecross-sectionalarea IS displayedas an upward kickon the acoustic
trace.
Depth scale computed from average acoustic velocity from collar count
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Processing of Acoustic Reflections in TWM
Reflected Pulsecaused by LiquidLevel
RTTT= 14.877 sec
LL @ 293.7 joints
Initial Acoustic Pulse
Reflected Pulsecaused byINCREASE in thecross-sectionalarea at 4017 feetas tubing tapers
down.
End of collar echoescounted by processing
record automatically.
Number of Collar
Echoes from 1.5 to 2.5seconds = 19.53 per
second
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Summary
Sound pressure pulse is generated at surface and pressure
wave travels down the wellbore. Changes in cross sectional area cause sound to be reflected
causing echoes that are recorded vs. time at the surface.
Reflected signal polarity indicates restrictions (down kick) orenlargements (up kick) encountered by the acoustic wave.
Round trip travel time (RTTT) is measured very accuratelyfrom shot to any echo flagged by the dashed vertical marker.
If present, the echoes from the tubing collars are counted asfar as possible down the acoustic record.
A depth scale is defined using the average sound speed forthe gas in the well computed from the collar echoes or fromknown downhole markers.
When tubing collars or known depth reflectors are notpresent the acoustic velocity for the gas is estimated fromgas properties, pressure and temperature.
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Questions ?