[0001] This invention relates to a method and apparatus for detecting a pressure pulse in
a flowing mud stream, and is particularly useful in measurement while drilling processes.
[0002] Measurement while drilling (MWD) is a technique whereby data collected at the bottom
of a borehole are transmitted to the surface by some form of telemetry. This results
in a major reduction in drilling time compared to other techniques in which drilling
has to be stopped to permit instrumentation to be lowered down the hole on a wireline.
[0003] MWD is widely used in drilling for oil and gas. Parameters measured include direction
and inclination of the drill string, and geological data such as gamma radiation,
resistivity, porosity and density. Various telemetry methods have been tried, the
most widely used at present being mud pulse transmission.
[0004] Drilling for oil and gas is carried out by means of a string of drill pipes, at the
downhole end of which is the drill bit. The pipes are rotated either by a drive device
on the surface or by a downhole motor or turbine. Drilling mud is pumped at high pressure
down the drill pipes to emerge through jets in the bit. The mud then travels back
up the hole via the annulus between the drillpipe and the hole wall, to be cleaned
and recirculated. The functions of the drilling mud are to lubricate the bit, carry
the cuttings back up to the surface, and balance the hydrostatic pressure in the rock
formation.
[0005] Mud is pumped downhole by a positive displacement pump, usually with three cylinders.
The pump pressure is up to 3000 psi (20.7 MPa) and the flow rate up to 1400 US gallons
(5.3m³) per minute. The pumps can develop several hundred horsepower. (1hp is 746W.)
A hydraulic accumulator, generally referred to as a de-surger in this application,
is installed in the pipeline to absorb the pressure fluctuations from the pump. These
would otherwise cause undue noise and vibration. The de-surger consists of a pressure
vessel in which an elastomeric diaphragm separates a volume of nitrogen from the mud
which fills the rest of the vessel. As will be seen, the de-surger affects the efficiency
of mud pulse transmission.
[0006] Mud pulses can be generated by opening and closing a valve between the drillpipe
and the annulus near the bottom of the drill string. When the valve is open, the pressure
drop across the bit jets is bypassed to some extent, and the pressure in the drill
pipe is reduced. A device operating in this way is generally referred to as a negative
pulser. Alternatively, a valve in the drill pipe can be partially closed, causing
a pressure increase or positive pulse. A third type of device produces a train of
pulses which are phase modulated to transmit data. This is really a special case of
a positive pulser.
[0007] Whatever type of pulser is employed, detection of the pulses is a major problem due
to attenuation of the signal and the presence of noise from the pump and elsewhere.
The signal to noise ratio is typically less than unity, necessitating the use of sophisicated
electronic signal processing techniques to improve detection. Even with these, detection
can be unreliable or impossible in some circumstances.
[0008] British patent specification no. 2160565A describes a way of overcoming at least
some of these problems. According to this specification, the mud flow rate, rather
than the mud pressure, is monitored at the surface using a flow meter downstream of
the de-surger. The mud flow rate at the surface responds more sharply to a downhole
mud pulse than does mud pressure and, in addition, signal to noise ratios for mud
flow rate are much higher than for mud pressure. According to GB 2160565A, suitable
flow meters are magnetic flow meters such as the Foxboro Series 2800 magnetic flowmeters
manufactured by The Foxboro, Massachusetts, USA. Other types of commercially available
flow meters, such as insertion type flow meters, can also be employed. Magnetic flow
meters operate by establishing a magnetic field through which the slightly conductive
drilling mud flows, thereby creating an electric potential. This potential, which
is proportional to the rate of flow, is measured and electronically amplified and
then transmitted to a recorder or data processor.
[0009] As a result of our own investigations, we also have found that surface measurement
of mud flow instead of mud pressure gives a number of advantages. However, the use
of sophisticated flow meters as envisaged in GB 2160565 is in itself disadvantageous
since they are expensive and can be costly to install and use.
[0010] We have now found that the use of these flow meters is unnecessary, and that good
results can be obtained by a different technique which does not necessitate the use
of such sophisticated and expensive equipment.
[0011] It is an object of the invention to provide a new, effective and simple method of
detecting mud pulses in a flowing stream of mud contained in a conduit.
[0012] According to one aspect of the present invention, mud pulses can be detected in a
flowing stream of mud in a conduit by monitoring the pressure change as the pulse-containing
stream passes between two regions of the conduit of different cross-sectional area.
In accordance with this aspect of the invention, the flowing mud will show a pressure
change as it passes from one region to the other. This difference in pressure will
change as a mud pulse flows into one of the regions. This change in the difference
in pressure between the two regions can be used very effectively to detect mud pulses
in the mud stream.
[0013] It is thus possible, by the present invention, to provide very effective and low
cost surface detection of mud pulses generated downhole while drilling. Apart from
the simplicity and lower cost overall, the method of the invention has other advantages
too. For example, because it monitors the difference in pressure between the two regions,
the background "noise" is of very little importance or effect. Furthermore, the change
in pressure due to the arrival of a pulse in one region can be a greater percentage
of the normal pressure difference between the regions, than is the change in flow
rate with the GB 2160565 arrangement or the pressure change in conventional prior
art procedures. These features give the present invention greater sensitivity and
accuracy as compared with prior art procedures.
[0014] In accordance with the invention, the two regions of different cross-sectional area
are preferably adjacent so that mud flows directly from one region into the other.
The pressure in each region can be measured independently, and then compared (normally
electronically) with the pressure in the other region. Alternatively, a differential
pressure transducer can be connected to the two regions to give direct information
as to the pressure difference.
[0015] In one highly preferred arrangement, a bypass conduit is tapped into a main conduit,
and a venturi for example is provided in the bypass conduit, the pressure changes
being measured in the bypass conduit this avoids having to interfere significantly
with the main mud flow conduit on site (which can be difficult on a working drilling
rig).
[0016] The invention also includes apparatus for detecting pulses in a stream of flowing
mud, which comprises a body for connection into the mud flow path, a through bore
in the body, the bore being of smaller cross-sectional area in the first region than
in a second region, and means for sensing the difference in pressure between mud in
the two regions.
[0017] Other objects and advantages of the invention will become apparent from the following
specification taken in conjunction with the accompanying drawings.
Figure 1 is a simplified schematic view of a drill string mud circuit;
Figure 2 is a diagram depicting a mud pulse in the circuit;
Figure 3 is a schematic view of one arrangement in accordance with the present invention;
Figure 4 is a schematic cross-sectional view of one embodiment of an apparatus of
the invention;
Figure 5 is a trace of pulse detections made by conventional processes (A) and by
the method of the invention (B);
Figure 6 is a schematic cross-sectional view of an alternative embodiment of an apparatus
of the invention; and
Figure 7 is a schematic plan view of another embodiment of apparatus according to
the invention.
[0018] Referring to the drawings, a simplified mud circuit is shown in Figure 1. A mud pump
1 drives mud through a drill string 2. A de-surger 3 contains a diaphragm 4 and a
volume of gas 5. A pressure transducer 6 is fitted downstream of the de-surger. The
mud pulser is represented by a valve 7 and the bit jets by a restriction 8.
[0019] The pulser 7 effectively has two settings, one of which will create a higher pressure
drop across the pulser than the other. The following discussion will relate to a positive
pulser i.e. the pressure upstream will rise when a pulse is created. The invention
is however equally effective with a negative pulser.
[0020] When the pulser is activated, the pressure immediately upstream increases and the
velocity decreases. These changes do not occur instantaneously throughout the drill
string, but propagate along it at the speed of sound in the fluid - approximately
4000 feet (1219m) per second. If the pressure transducer is 8000 feet (2438m) from
the pulser, its reading will remain unchanged for two seconds after the pulser is
activated.
[0021] The volume of mud produced by the pump can be assumed to be substantially unaffected
by the increased pressure of the pulser signal. If the pulse were of sufficient duration
for transients to die away, pressure at the transducer would stabilise at a higher
value determined by the various losses in the system including the pulser restriction,
and velocity at the transducer would return to its previous value.
[0022] In practice, the pulse is too short for stabilisation to occur, and the transient
signal must be detected. This can best be visualised as a region in the drill pipe
in which mud pressure is increased and velocity decreased. This is shown diagrammatically
in Figure 2.
[0023] The region 9, which will be referred to as the pulse, moves upstream at the velocity
of sound in the fluid. At the leading edge of the pulse there will be a transition
area 10 in which the transition between lower pressure/higher velocity and higher
pressure/lower velocity will occur. The length of the transition area will depend
on the speed of operation of the pulser, the degree of diffraction due to changes
in drill pipe section, and the effects of viscous friction. Similarly, there will
be a second transition area 11 at the trailing edge of the pulse in which the opposite
changes in pressure and velocity take place.
[0024] When the leading edge of the pulse 9 reaches the pressure transducer 6, an increase
in pressure will be detected. However, when the leading edge reaches the desurger
3 the pressure will immediately be reduced to its previous value. This reduction in
pressure will be reflected back down the drill pipe. When it passes the transducer,
the indicated pressure will return to its normal value. The transducer will therefore
register a short duration signal whose duration is twice the distance between the
transducer and the de-surger divided by the speed of sound in the fluid. These short
duration signals are usually referred to as 'sonics', and are not always detected
in practice.
[0025] The velocity of the fluid in the pulse is not similarly cancelled out by the presence
of the de-surger. The reduced pressure at the upstream end of the pulse results in
a further reduction in velocity, so while the pressure component in the pulse is removed,
the velocity component is enhanced.
[0026] In practice, a pressure signal may still be detected in the absence of sonics, but
its amplitude depends on the duration of the pulse. This can be illustrated by a numerical
example:
[0027] Suppose a pump is supplying 300 US gallons per minute at a pressure of 1500 psi,
and that a mud pulser at the bottom of the drill string can create an additional pressure
drop of 200 psi. Total pressure difference when the pulser is activated is therefore
1500 + 200 = 1700 psi.
[0028] Assuming a drill pipe bore above the pulser of 3.5 inches, cross sectional area is
3.5² x Pi/4/144 = 0.067 square feet.


[0029] Assuming that the change in velocity is proportional to the square root of the change
in pressure difference:

[0030] When the pulse reaches the de-surger, there is going to be a surplus of mud produced
by the pump over that going downhole, proportional to the ratio of the two velocities.
That surplus can only go into the de-surger.
[0031] The initial flow into the de-surger is:

[0032] Assuming that the initial charge of gas in the de-surger is equivalent to a volume
of 1l gallons at 1500 psi, the volume would reduce in one second to 11 - 0.3 = 10.7
gallons.
[0033] The pressure in the de-surger would increase to:

[0034] The initial rate of pressure change is only 42 psi per second. A pulse of 0.1 seconds
duration would only give a pressure rise, sonics apart, of 4.2 psi. This would be
extremely hard, if not impossible to detect.
[0035] It can be seen from the foregoing that it would be preferable to detect the velocity
component of a pulse rather than the pressure component. The invention to be described
provides a method of doing this.
[0036] Figure 3 shows two pressure transducers 30, 31 installed in sections 32, 33 of pipe
having different diameters. Since the sum of pressures and kinetic energies remains
constant, the pressure in the smaller diameter pipe will be lower. This effect is
well known in fluid mechanics and can be expressed as:

Where:
- P1
- = pressure in the larger diameter
- P2
- = pressure in the smaller diameter
- V1
- = velocity in the larger diameter
- V2
- = velocity in the smaller diameter
- D
- = density in pounds per cubic foot
- 144
- = square inches/square foot
- 32.2
- = acceleration due to gravity ft/sec²
[0037] Taking density as 78 pounds per cubic foot, assuming a reduction in pipe diameter
from 3.5 to 2.5 inches, and taking the original value of 10 ft.sec for V1.


[0038] When V1 reduces to 9.4 ft/sec due to the arrival of a pulse,


[0039] If the signals from the two transducers are subtracted electrically, the remaining
difference signal will give an accurate indication of velocity. Alternatively, a differential
pressure transducer may be connected between the two pressure tappings to give a direct
indication of velocity.
[0040] The distance between pressure tappings should be kept to a minimum for optimum detection
of short pulses. Figure 4 shows a device designed for mud pulse velocity detection.
It consists of a body 12 preferably having screw threads 13, 14 at each end to permit
fitting in the pipeline from the de-surger to the drill pipe. The body has an internal
constriction 15 with a pressure tapping 16. A second tapping 17 is provided in the
larger diameter of the body. A differential pressure transducer 18 is connected across
the two tappings. The constriction may optionally be faired by two tapered sections
19, 20 to reduce erosion due to turbulent mud flow.
[0041] As an additional refinement, the cross sectional area at the constriction may be
adjustable by means of a plunger operated by a screw thread or hydraulic ram in order
to accommodate the range of mud flow rates encountered in practice.
[0042] Figure 5 is an example of unprocessed pressure (A) and velocity (B) traces obtained
from a positive pulser at a depth of 4500 feet, using the detection device described
above for velocity. The greater amplitude and clarity of the velocity signal are obvious.
Pulse width is 0.5 seconds.
[0043] Figure 6 shows an alternative device for mud pulse velocity detection. The device
as shown is adapted to fit into a standard pressure transducer tapping 40 which may
already exist on rig pipework 41 by means of screw threads 42 in the tapping. Alternatively,
the device may be provided within a screw-threaded body for fitting into a pipeline
in a manner similar to that described with respect to the Figure 4 embodiment.
[0044] The device of Figure 6 comprises a plunger 43 slidably supported within a sleeve
44. The sleeve 44 is provided with screw threads 45 which cooperate with screw threads
42 in the tapping 40. A shoulder 46 on a plunger 43 separates a first portion 47 of
the plunger from an end portion 48 of the plunger having a larger diameter than the
first portion 47. The shoulder 46 limits the distance by which the plunger 43 is permitted
to slide within the sleeve 44. An annular recess 49 is provided in the first portion
47 of the plunger and a screw-threaded hole 50 is provided in the sleeve 44. A locking
screw 51 fits through the hole 50 and cooperates with the annular recess 49 to permit
fixing of the plunger 43 within the sleeve at the correct depth and alignment, as
will be described in more detail below. O-ring seals 60 are provided between the plunger
and the sleeve to prevent leakage of the drilling mud from the pipework 41.
[0045] A high pressure tapping or aperture 52 is formed in the plunger 43, and is connected
via a through-passage 53 and a connecting loop 54 with one side of a differential
pressure transducer 55. A low pressure tapping or aperture 56 is also formed in the
plunger 43, and is connected via a through-passage 57 and a connecting loop 58 with
the other side of the differential pressure transducer 55. The low pressure aperture
56 is oriented at right angles to the high pressure aperture 52.
[0046] As shown in Figure 6, the drilling mud is flowing through the pipework 41 in the
direction of arrow 59. In order to use the device of Figure 6 to detect mud pulse
velocity, the device is positioned in the tapping 40 and the location of the plunger
43 within the sleeve 44 is adjusted, such that the end portion 48 of the plunger protrudes
into the fluid flow by a selected amount in order to cause a restriction in the flow.
The plunger is oriented with the high pressure aperture 52 facing upstream, as shown,
and the depth and orientation of the plunger are set by means of the locking screw
51.
[0047] In the position shown in Figure 6, the high pressure aperture 52 is exposed to the
stagnation pressure in the flow, since the restriction in the flow caused by the end
portion 48 of the plunger 43 creates a stagnation point immediately upstream of the
plunger. The low pressure aperture 56 is exposed to the static pressure of the fluid
near the minimum cross-section of the restriction in the flow.
[0048] The sensitivity of the device of Figure 6 is therefore higher than that of the device
of Figure 4 since it senses the high pressure at a stagnation point in the flow.
[0049] A further advantage of the device shown in Figure 6 is that it can be fitted to the
standard transducer tappings already provided on rig pipework, thus facilitating installation.
[0050] The end portion 48 of the plunger 43 may be provided with a streamlined shape, or
with an aerofoil.
[0051] In the embodiment of Figure 7, a main mud flow conduit 70 (the direction of flow
being shown by arrow 71) is tapped to provide a bypass passage 72 in parallel to the
main flow 71. A venturi 73 is provided in the bypass and a pressure sensor 74 is provided
connected at one side to the venturi and at the other side upstream of the venturi.
This arrangement enables the invention to be used without carrying out major interfering
work on the main flow conduit 70.
[0052] It must be understood that the foregoing description has been given only by way of
example and that it in no way limits the scope of the invention. Clearly various modifications
and changes may be made by those skilled in the art without departing from the spirit
and scope of the invention.
1. A method of detecting mud pulses in a flowing stream of mud in a conduit comprising
comparing pressure signals from two regions of the conduit of different cross sectional
area.
2. A method according to Claim 1, wherein the pressure signal from each of the two regions
is measured independently, and the pressure signals are then compared.
3. A method according to Claim 1 or 2, wherein a differential pressure transducer is
connected to the two regions and a direct comparison of the pressure signals is provided.
4. A method according to Claim 1,2 or 3, wherein the two regions are adjacent.
5. A method according to Claim 1,2,3 or 4, wherein the stream of mud is in a bypass parallel
to a main mud flow conduit.
6. A mud pulse detection device comprising a body (12) defining a through bore for passing
drilling mud therethrough; a first region in the bore; a second region in the bore
having a greater cross-sectional area than said first region; and means (18) for sensing
the difference in pressure between the mud in the first and second regions.
7. A mud pulse detection device according to Claim 6, wherein means (13,14) are provided
on said body for connection of said body (12) in a drilling mud circuit.
8. A mud pulse detection device according to Claim 6 or 7, wherein said first region
is provided by an internal constriction (15), and wherein said device additionally
comprises a first pressure tapping (16) exposed to pressure in the first region, a
second pressure tapping (17) exposed to pressure in the second region, and a means
for measuring and transmitting the difference in pressure between the first and second
tappings.
9. A mud pulse detection device according to Claim 8, wherein streamlined fairings (19,20)
are provided on the constriction (15).
10. A mud pulse detection device according to Claim 8 or 9, wherein the cross-sectional
area at the constriction (15) is adjustable by means of a plunger.
11. A mud pulse detection device according to Claim 10, wherein the plunger is operable
by means of a locking screw.
12. A mud pulse detection device according to Claim 10, wherein said first and second
pressure tappings are provided within the plunger, and wherein said second pressure
tapping is exposed to the pressure at a stagnation point upstream of said plunger.