TECHNICAL FIELD OF THE INVENTION
[0001] The present invention relates to a subsea compression system for well stream boosting
by compression of gas and pumping of liquid in subsea hydrocarbon production. More
precisely, the present invention refers to arrangements on a compressor station forming
part of a subsea compression system.
BACKGROUND AND PRIOR ART
[0002] Offshore gas production involves installations on the seabed which are controlled
and powered from a land-based or sea-based terminal or host facility. Well fluid is
transported via pipelines from a subsea production system to the receiving terminal
to be further processed before the products are supplied to market. In the initial
phases of production, the fluid reservoir pressure is usually sufficient for feeding
the hydrocarbon fluids through the pipeline. Later in production, or in the case of
very long distance between the well fluid reservoir and the receiving terminal, boosting
of fluid pressure and flow may be required at one or more compression stations along
the feed line in order to maintain flow rate and production level.
[0003] Compressors used in subsea compression stations are adapted to process wet gas containing
a certain ratio of liquid. Above such a ratio, liquid pumps will be required. In the
compression station, well fluid containing gas and liquid enters a separator or scrubber
in which liquid is separated from the well stream and fed to the pump, providing predictable
operating points for both the compressor and the pump with respect to liquid volume
fraction. The pump is operated to pump the liquid downstream, typically by injecting
the liquid into the compressed gas that is discharged from the compressor, whereby
a re-mixed multiphase well fluid leaves the compression station at a raised pressure
level and flow. Nevertheless, the subsea compression station may optionally be arranged
for discharge of boosted gas and liquid flows via separate export lines.
[0004] Conventionally, each compressor and pump is driven by a dedicated electrical motor
respectively which is supplied operating and control power via an umbilical connecting
the compression station with its host facility. Each compressor or pump motor in the
compression station requires for its operation an individual setup of power and control
gear for a variable speed drive, such as subsea switchgear, wet-mate electrical connectors,
high voltage electrical jumpers and electrical control system components, cooling
and lubricating circuits including valves and flow or pressure control, etc.
SUMMARY OF THE INVENTION
[0005] The present invention aims to reduce the number of components required in a subsea
compression station configured for boosting a well stream containing gas and liquid.
[0006] The object is met in a subsea compression station comprising a separator, a compressor
and a pump, wherein the compressor is operable for compression and discharge of gas
separated from a well stream fed into the separator, and the pump is operable for
pumping liquid that is separated from the well stream. An electrical motor is drivingly
connected to a compressor rotor having a compressor rotor shaft, the compressor rotor
shaft being connectable to a pump rotor via a speed reduction device bringing the
pump rotor in co-rotation with the compressor rotor at reduced speed.
[0007] Thus, the dedicated pump motor and associated components such as power supply components,
operation control, lubrication and cooling components etc., can be omitted which substantially
reduces cost and complexity of the compression station.
[0008] The speed reduction device can be realized in alternative ways. A speed reduction
ratio of about 4-5:1 can be assumed appropriate for a majority of subsea compressor/pump
combinations.
[0009] For example, a mechanical clutch and gear reduction may be used as coupling and speed
reduction device. A mechanical clutch coupling would however require slowing down
the drive motor and compressor in order to connect the pump rotor to the compressor
rotor, which revolves at considerably higher speed than the pump rotor in normal operating
conditions.
[0010] In order to provide smooth acceleration of the pump it is preferred to connect the
pump rotor to the compressor rotor shaft via a variable speed hydrodynamic torque
converter, or alternatively, via an electrical hysteresis powered clutch, both of
which provide torque transfer without physical contact between the driving compressor
rotor shaft and the driven pump rotor.
[0011] In one preferred embodiment of the present invention, the compressor rotor shaft
is fixedly connected to a housing of a fill-controlled hydrodynamic torque converter,
and the pump rotor is fixedly connected to a turbine of the fill-controlled torque
converter.
[0012] In another preferred embodiment, the compressor rotor shaft is fixedly connected
to an impeller of a variable vane hydrodynamic torque converter, and the pump rotor
is fixedly connected to a turbine of the variable vane torque converter.
[0013] In yet another preferred embodiment, the compressor rotor shaft is fixedly connected
to a rotor of an electrical hysteresis powered clutch, and the pump rotor is fixedly
connected to a hysteresis disk of the electrical clutch.
[0014] The present invention thus provides a common-drive and individual control concept
wherein adjustable amount of torque can be transferred without physical contact from
a compressor motor to a pump rotor in a subsea compression station, bringing the pump
rotor in co-rotation with the compressor rotor at reduced speed. Connecting in and
connecting out of the pump can be accomplished as required with respect to a liquid
content in the supplied well stream, either by controlling the filling of a fill-controlled
hydrodynamic coupling, or by adjusting the attack angle of vanes in a variable vane
hydrodynamic coupling, or by regulation of electrical power supplied to an electromagnet
of an electrical hysteresis powered clutch.
[0015] The present invention is advantageously applied to a subsea compression station wherein
a centrifugal wet gas compressor and a positive displacement liquid pump are commonly
driven and independently controlled.
[0016] Further advantages, advantageous features and embodiments of the invention will appear
from the dependent claims and from the following detailed description of preferred
embodiments.
SHORT DESCRIPTION OF THE DRAWINGS
[0017] The invention will be further explained below with reference made to the accompanying,
schematic drawings. In the drawings,
Fig. 1 is a diagram illustrating schematically the setup of a prior art subsea compressions
station;
Fig. 2 is a diagram corresponding to Fig. 1, illustrating the setup of a subsea compression
station according to the present invention;
Fig. 3 is sectional view showing one preferred embodiment of the present invention;
Fig. 4 is a corresponding sectional view showing another preferred embodiment;
Fig. 5 is a sectional view showing yet another preferred embodiment, and
Fig. 6 is a simplified diagram illustrating an implementation of the present invention.
DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS
[0018] An overview of the main modules and parts of a subsea compression station for well
stream boosting is illustrated schematically in the diagram of Fig. 1. The compression
station receives bi-phase or multi-phase well fluid from at least one subsea production
system and feeds boosted well fluid into one or several export pipe lines for further
transport to a receiving terminal. The compression station comprises a compressor
module including one or more compressors 1, a pump module including at least one pump
2, and a separator/scrubber module including a separator 3. The separator 3 is designed
for liquid/gas separation and may additionally be structured for dissolving liquid
slugs, for hydrate prevention and for sorting out solid particles entrained in the
well stream, for gas scrubbing etc., so that compressible gas (wet gas) mainly is
delivered to the compressor intake. The compressor(s) 1 is designed for raising the
pressure of the gas and discharging the gas at an elevated pressure into the export
pipeline. The pump(s) 2 is designed for injecting the excess liquid, at an elevated
pressure, to the gas flow discharged from the compressor.
[0019] High voltage power, low voltage power, hydraulic, control and utilities are supplied
from the host facility via an umbilical connected to the subsea compression station.
Utility and control power is distributed to consumers on the subsea compression station
via transformers, high voltage cables and wet-mate electrical connectors, switchgear,
electrical jumpers, circuit breaker modules, etc. Since the compressor(s) and pump(s)
are individually driven by dedicated variable speed drive (VSD) electrical motors
4 and 5, respectively, utility and control power equipment need to be individually
installed for each motor. In the drawings, the dedicated utility and control power
equipment is schematically represented through VSD-blocks 6.
[0020] In addition, each motor requires separate flexible couplings, guiding and landing
devices, valves and fluid lines for cooling, lubrication and barrier pressure, on
the subsea compression station.
[0021] Fig. 2 is an overview of a subsea compression station which is setup in utilization
of the present invention. A noticeable difference in the architecture of Fig. 2 is
the significantly reduced number of VSD-blocks 6, which can be reduced by 50 % as
the result of driving the pump(s) 2 with the compressor motor(s) 4, via the compressor
rotor shaft 7 and an interconnected speed reduction device 8 effective for bringing
the pump rotor in co-rotation with the compressor rotor at reduced speed.
[0022] Naturally, the reduction in number of components required in the subsea compression
station applies to all components that would otherwise have been involved in the operation
of the omitted motor.
[0023] Fig. 3 illustrates a first preferred embodiment of the invention, relying on a speed
reduction device in the form of a variable speed, hydrodynamic torque converter 9.
[0024] In the embodiment of Fig. 3, the compressor rotor shaft 7 is fixedly connected to
a housing 10 of a fill-controlled hydrodynamic torque converter, and the pump rotor
11 is fixedly connected to the turbine 12 of the fill-controlled torque converter.
The amount of torque and output speed that is transferred from the compressor rotor
shaft to the pump rotor depends on the fill level of hydraulic fluid in the housing,
which can be controlled and modified during operation. For a slow start of the pump,
acceleration of pump rotor can be controlled through the speed by which the housing
is filled, and the appropriate speed reduction is achieved through a corresponding
fill level in the housing.
[0025] Alternatively, and illustrated in Fig. 4, the compressor rotor shaft 7 may be fixedly
connected to an impeller 13 of a variable vane hydrodynamic torque converter 14, whereas
the pump rotor 11 is fixedly connected to the turbine 15 of the variable vane torque
converter. The amount of torque and output speed that is transferred from the compressor
rotor shaft to the pump rotor depends on the angle of attack of guide vanes 16 arranged
adjustable on a stator 17 in which the impeller is housed, and can be controlled and
modified during operation through actuation of a vane angle shifting mechanism 18
supported on the stator.
[0026] Fig. 5 illustrates another preferred embodiment of the invention, relying on a speed
reduction device in the form of an electrical hysteresis powered clutch 19.
[0027] In Fig. 5, the compressor rotor shaft 7 is fixedly connected to a rotor 20 of the
electrical hysteresis powered clutch, and the pump rotor 11 is fixedly connected to
a hysteresis disk 21 of the electrical clutch. The hysteresis disk 21 passes an annular
gap in the rotor 20 without physical contact between disk and rotor. The rotor 20
rotates in a magnetic field created as current/voltage is applied to an electromagnet
22 near the rotor. As the rotor rotates, the hysteresis disk is pulled in rotation
in result of magnetic drag between the rotor 20 and the hysteresis disk 21. Since
the hysteresis disk becomes magnetized in relation to the strength of the magnetic
flux created by the electromagnet, the amount of torque and output speed that is transferred
from the compressor rotor shaft to the pump rotor depends on the amount of current/voltage
that is applied to the electromagnet, which can be controlled and modified during
operation.
[0028] A subsea compression station laid out in accordance with the common-drive and individual
control concept provided by the present invention is illustrated schematically in
Fig. 6.
[0029] Without explicitly being explained in detail with reference to Fig. 6, a fully equipped
and operative subsea compression station typically comprises import and export well
stream manifolds and valves, flow and pressure meters, re-circulation lines and valves,
anti-surge control circuit and valves, lubrication and barrier fluid circuits and
valves, umbilical head end, transformers, coolers, sand trap etc., and other equipment
which is conventionally found on a subsea compression station. For reasons of clarity,
the detailed structure and organization of modules and units which are of subordinated
significance in this connection have been excluded from Fig. 6.
[0030] In a subsea compression station implementing the invention, well fluid F is fed into
a separator and slug catcher 3 configured for separation of gas and liquid. The separator
houses a mixer pipe 23 wherein gas and remaining liquid are evenly distributed before
delivery to the intake of compressor 1 via wet gas fluid line 24. The level of liquid
in the separator 3 is controlled through drain pipe 25 from which excess liquid is
withdrawn and delivered to pump 2 via self-filling liquid line 26. The compressor
1 and pump 2 are commonly driven by a single, variable speed electrical motor 4, the
output torque and speed of which is reduced by means of a speed reduction device 8
interconnected between the pump and the compressor.
[0031] Utility and control power is supplied to the motor 4 via VSD-block 6 and umbilical
head end block 27 representing the necessary high and low voltage circuits, wet mate
connectors, switchgear, circuit breakers, etc. Operating fluid or pressure for the
fill-controlled torque converter, or control power for the variable vane torque converter,
or magnetizing current/voltage for the electrical hysteresis clutch, as required in
each respective embodiment, is supplied to the speed reduction device 8 from the host
facility/top side terminal via power supply line 28. Control of power supply for actuation
of the speed reduction device 8, i.e. coupling and de-coupling with the compressor
rotor shaft, is accomplished in response to a detected liquid fraction or level in
the separator 3 and communicated to actuator valves or actuator switches in the speed
reduction device via pilot line 29.
[0032] The compressor(s) used in the subsea compression station is designed for a substantial
elevation of the gas pressure, such as from about 40 bar at compressor intake to about
120 bar at compressor discharge, e.g. Heavy duty centrifugal wet gas compressors are
generally used in this connection, typically operating at a power range of one or
several tens of megawatt and at rotational speeds in the order of 8-12,000 rev per
min.
[0033] The pump(s) used in the subsea compression station is designed for boosting the liquid
stream up to a pressure required for introduction into the gas discharged from the
compressor. Positive displacement pumps are useful in this connection, operating at
a power range of hundreds of kilowatt and at rotational speeds of about 1,500-4,000
rev per min. Thus in most compressor/pump combinations a speed reduction ratio of
about 4-5:1 will be appropriate. However, positive displacement pumps or centrifugal
pumps rotating at other operational speeds may alternatively be used, requiring different
speed reduction ratios. Nevertheless, the present invention provides great freedom
in the choice of pump/compressor combination since both the fill-controlled or variable
vane hydrodynamic torque converters as well as the electrical hysteresis clutch can
be controlled between zero and 100 % lockup between driving and driven components,
depending obviously on the output torque required.
[0034] Although referred to as a compressor rotor shaft 7 in the description and appended
claims, the element 7 shall be understood to include any shaft or axle that is connectable
to or constitutes an integrally formed extension from the compressor rotor and which
co-rotates with the compressor rotor.
[0035] Although referred to as a pump rotor 11 in the description and appended claims, the
element 11 shall be understood to include any shaft or axle that is connectable to
or constitutes an integrally formed extension from the pump rotor and which co-rotates
with the pump rotor.
[0036] The invention is not limited to the in-line, co-axial assembly which is schematically
illustrated in the drawings. Instead, the pump and compressor may alternatively be
arranged on parallel axes, or even on crossing axes, with intermeshing gears or bevel
gears transmitting torque and rotation from the compressor motor to the pump rotor.
[0037] The invention is not in any way restricted to the embodiments described above. On
the contrary, many possibilities to modifications thereof will be apparent to a person
skilled in the art without departing from the basics of the invention such as defined
in the appended claims.
1. A subsea compression station comprising a separator (3), a compressor (1) and a pump
(2), wherein the compressor is operable for compression and discharge of gas separated
from a well stream ingested into the separator, and the pump is operable for pumping
liquid that is separated from the well stream, and further comprising an electrical
motor (4) drivingly connected to a compressor rotor having a compressor rotor shaft
(7), characterized in that the compressor rotor shaft is connectable to a pump rotor (11) via a speed reduction
device (8) bringing the pump rotor in co-rotation with the compressor rotor at reduced
speed.
2. The compression station of claim 1, wherein the speed reduction device is a variable
speed hydrodynamic torque converter (9; 14).
3. The compression station of claim 2, wherein the compressor rotor shaft (7) is fixedly
connected to a housing (10) of a fill-controlled hydrodynamic torque converter (9),
and the pump rotor (11) is fixedly connected to a turbine (12) of the fill-controlled
torque converter.
4. The compression station of claim 2, wherein the compressor rotor shaft (7) is fixedly
connected to an impeller (13) of a variable vane hydrodynamic torque converter (14)
and the pump rotor (11) is fixedly connected to a turbine (15) of the variable vane
torque converter.
5. The compression station of claim 1, wherein the speed reduction device is an electrical
hysteresis powered clutch (19).
6. The compression station of claim 5, wherein the compressor rotor shaft (7) is fixedly
connected to a rotor (20) of the electrical hysteresis powered clutch and the pump
rotor (11) is fixedly connected to a hysteresis disk (21) of the electrical clutch.
7. The compression station of any of claims 1-6, wherein the speed reduction device has
a speed reduction ratio of about 4-5:1.
8. The compression station of any of claims 1-7, wherein a centrifugal wet gas compressor
and a positive displacement liquid pump are commonly driven and independently controlled.