[0001] The present invention relates to a method for providing pressurized gas from a source
of liquefied gas to a consumer. The invention also relates to a compressor arrangement
for providing pressurized gas from a source of liquefied gas to a consumer and to
a ship for transporting liquefied gas comprising a compressor arrangement according
to the invention.
[0002] The invention is of particular relevance to the supply of fuel gas from a source
of liquefied natural gas (LNG), especially in ocean-going tankers and is primarily
described herein with the reference to this application. It is, however, to be understood
that it is also applicable to other cryogenic liquids or liquid mixtures.
State of the Art
[0003] While natural gas is conveniently stored and transported in liquid state, it is generally
used, however, in the gaseous state, e.g. for propulsion of the tanker. To this end,
a flow of LNG can be vaporized and/or boil-off gas, i. e. evaporated LNG from the
ullage space of the container can be used. Such vaporized gas is supplied from the
source of liquefied gas through a main input line to a compressor for pressurizing
the vaporized gas. Over the past decades, fuel gas supply to LNG carrier propulsion
has namely being achieved using multi-stage compressors (stage number ranging from
2 to 6 stages), in which typically each stage is integrated in one single gearbox
including several highspeed shafts. For example, 4-stage compressors have progressively
replaced 2-stage compressors for DFDE (Dual Fuel Diesel Electric) 4-stroke propulsion,
since 4-stage compressors are able to maintain the required fuel gas (FG) pressure
(6 bara) even with warm boil off gas (BOG) at suction. Recently, 6-stage compressors
have been developed to cope with 2-stroke dual fuel propulsion requirements for 17
Bara fuel gas pressure level (XDF). A 2-stage compressor is mainly used in laden voyage
when BOG is cold (typically -90°C). However, when the BOG temperature warms-up (especially
during ballast voyage), performance limitations are reached and it becomes difficult
to maintain the required fuel gas pressure. 4-stage compressors can be used either
in cold (laden) or in warm (ballast and heel-out) BOG conditions. Thus, different
BOG conditions (laden, ballast or heel-out) and different consumers (2 or 4-stroke
dual fuel engines) require different multi-stage compressors leading to a cumbersome
and costly compressor arrangement.
[0004] Very often, a standard approach selected during ship design is to provide one fuel
gas (FG) compressor (with a spare one) sized to supply gas to the consumers with the
most constraining suction conditions. At fixed discharge pressure dictated by the
FG consumer, the variability of suction conditions (pressure, temperature and composition)
can lead to a FG compressor design, which is not optimized in all possible operating
cases.
[0005] Typical temperature levels met at compressor suction are ranging from 40°C to -140°C
(covering heel-out to laden operations) which has a great impact on fuel gas density.
The compressor design features required to cope with this fuel gas density range often
leads to a lower compressor efficiency at cold temperature. This is because, in cold
suction conditions, the required head of the overall compressor is lower. The technical
term "compressor head" basically corresponds to the pressure of the pressurized fluid,
more specifically to the pressure divided by the product of fluid density and the
gravitation constant. This corresponds to the height of a column of the fluid exerting
said pressure on its bottom.
[0006] Typical FG compressor suction pressure levels met on LNG carriers are ranging from
1.03 to 1.7 Bara, which has even a greater impact on compressor performance than the
suction temperature range. At fixed discharge pressure, the poorest performances are
met at high suction pressure since it leads to a lower required head of the compressor.
Often low temperature and high-pressure conditions at compressor suction are combined.
[0007] The typical composition of BOG is ranging from pure methane to a C1/N2 mixture containing
up to 20 % mol N2. BOG from the tanks is usually found in the range of 40/-140°C.
40°C BOG is met when the tanks are operated with very few liquid (dead heel). -140°C
is often met after tank loading when BOG flow is high. Intermediate temperature levels
(-50/-80°C) can be found in ballast operations. The pressure ranges from 1.03 to 1.7
Bara. Typical LNG carriers have tank operating pressure levels ranging from 1.03 to
1.26 bara whereas vessels with reinforced tank containments have operating pressures
reaching 1.6 bara or slightly above.
[0008] LP (Low Pressure) consumers usually require FG at around 6 Bara and 20/40°C. MP (Medium
Pressure) consumers usually require FG at pressure levels of 15 and 40 Bara and 20/40°C.
HP (High Pressure) consumers usually require FG at a pressure above 100 bar (up to
400 Bara) and a temperature range 40/20°C.
[0009] It is therefore an object of the present invention to provide an efficient method
for providing pressurized gas from a source of liquefied gas to a consumer, especially
providing the possibility of using vaporized gas of different temperature and/or pressure
and/or mass flow levels and/or of varying composition and/or supplying different consumers
requiring pressurized gas at different temperature and/or pressure levels, with pressurized
gas, especially with fuel gas from an LNG source.
Summary of the present invention
[0010] The object is solved by a method for providing pressurized gas from a source of liquefied
gas to a consumer according to claim 1, a compressor arrangement for providing pressurized
gas from a source of liquefied gas to a consumer according to claim 7 and a LNG carrier
comprising a compressor arrangement according to claim 14.
[0011] According to the present invention there is provided a method for providing pressurized
gas from a source of liquefied gas to a consumer, wherein vaporized gas is supplied
via a first line from the source of liquefied gas to a compressor arrangement for
pressurizing the vaporized gas, the compressor arrangement comprising a first screw
compressor module and a second screw compressor module which are designed according
to the redundancy concept each comprising an own screw compressor and an own motor
for driving the screw compressor, wherein the first screw compressor module, being
arranged at the first line and being fed with vaporized gas via the first line, is
arranged in parallel to the second screw compressor module, the second compressor
module being arranged at a bypass-line, the bypass-line branching off the first line
upstream of the second screw compressor module, wherein the compressor arrangement
is operated such that in a first mode of operation the vaporized gas is fed through
the first line to the first screw compressor module and through the bypass-line to
the second screw compressor module and the first screw compressor module and the second
screw compressor module are in operation, and in a second mode of operation, the bypass-line
is closed with a valve at a position upstream of the second screw compressor module
and the second screw compressor module is not in operation.
[0012] The terms first and second do not indicate the arrangement with regards to the flow
of compressed gas but are merely used for clarity of enumeration.
[0013] The redundancy concept means that each screw compressor module design includes its
own screw compressor and all own equipments, like valves, electrical motor for driving
the compressor and instruments as an independent screw compressor system. As the screw
compressor within each screw compressor module is driven by its own electrical motor,
each screw compressor can then be separately driven from the screw compressor of another
screw compressor module. Therefore each screw compressor module is able to be independently
operated from any other screw compressor module of the compressor arrangement, which
is particularly advantageous if one of the compressor modules must be stopped for
example for maintenance because the other compressor module can still be operated
and purveying compressed gas to the consumer.
The second compressor module can also be deactivated and bypassed when not needed.
With such a compressor train modularization, it is not necessary to run all the screw
compressors modules when only a part of them is required. As an example, the first
screw compressor module could be operated only in cold suction conditions whereas
the additional screw second compressor module could be started in case of warm suction
conditions in order to maintain the required fuel gas pressure. This is an improvement
in terms of power consumption of the compressor arrangement.
[0014] To keep the efficiency of the compressor arrangement near the optimum point of best
efficiency, the motor driving the screw compressor of at least one of the screw compressor
modules is an electrical motor whose speed of rotation can be adjusted, when the screw
compressor module is in operation, with a variable frequency drive depending on at
least one of pressure level, temperature level, mass flow and composition of the gas
to be provided to the consumer, hence adjusting the speed of rotation of the screw
compressor of at least one of the screw compressor modules to the gas conditions.
As at least one of the screw compressors is driven by a variable speed electrical
motor, the speed of rotation of at least one of the screw compressor can be permanently
adjusted to the conditions of the gas to be compressed, without wasting energy in
recycling gas around the compressor.
[0015] In a preferred embodiment, a third screw compressor module is connected in series
downstream the first and/or the second screw compressor module.
The terms "upstream" and "downstream" means about the direction of flow of the compressed
gas through the compressor arrangement.
[0016] In another preferred embodiment, the speed of rotation of the electrical motor driving
the screw compressor of the third screw compressor module is adjusted with a variable
frequency drive, depending on at least one of pressure level, temperature level, mass
flow and composition of the gas to be provided to the consumer.
[0017] In a further embodiment, boil-off gas from the ullage space of the container/source
of liquefied gas where the stored liquefied gas changes its stage from liquid to vapor
can be used as the vaporized gas.
[0018] Additionally, the gas compressed by one of the screw compressor modules can be cooled
by conducting the gas through a cooling unit arranged at an outlet of at least one
screw compressor, i.e. downstream of the at least one screw compressor.
[0019] The proposed approach according to the present invention is to provide a modular
compressor train philosophy with a limited footprint. Compressor efficiency is maintained
over the whole range of suction conditions. Optimization of gas compressor efficiency
is achieved by selecting the numbers of screw compressor modules put in operation
according to the required load (mass flow), pressure level head and/or temperature
of the gas that is provided to the consumer. The possibility of bypassing one or more
of the screw compressor modules of the compressor arrangement allows for a flexible
operation depending on the suction conditions to reach the required gas pressure level.
At the same time, it is possible to deactivate compressor modules that are presently
not needed. Furthermore, the compressor arrangement according to the present invention
allows for spare screw compressor modules what be used as redundancy is case one of
the screw compressors modules had to be stopped, for example for maintenance.
[0020] According to a second aspect, the present invention relates to a compressor arrangement
for providing pressurized gas from a source of liquefied gas to a consumer, wherein
vaporized gas is supplied from the source of liquefied gas to a compressor arrangement
for pressurizing the vaporized gas, the compressor arrangement comprising a first
screw compressor module and a second screw compressor module which are designed according
to the redundancy concept each comprising an own screw compressor and an own motor
for driving the screw compressor, wherein the first screw compressor module, being
arranged at the first line and being fed with vaporized gas via the first line, is
arranged in parallel to the second screw compressor module, the second screw compressor
module being arranged at a bypass-line, the bypass-line branching off the first line
upstream of the second screw compressor module, wherein the compressor arrangement
is operable such that in a first mode of operation the vaporized gas is fed through
the first line to the first screw compressor module and through the bypass-line to
the second screw compressor module and the first screw compressor module and the second
screw compressor module are in operation, and in a second mode of operation, the bypass-line
is closed with a valve at a position upstream of the second screw compressor module
and the second screw compressor module is not in operation..
[0021] Additionally, at least one of the screw compressor modules comprises a variable frequency
drive for adjusting the speed of rotation of the electrical motor driving the screw
compressor when the screw compressor module is in operation, depending on at least
one of pressure level, temperature level, mass flow and composition of the gas to
be provided to the consumer.
[0022] In a preferred embodiment, the compressor arrangement comprises a third screw compressor
module connected in series downstream the first and/or the second screw compressor
module.
[0023] To adjust the capacity of the third compressor module to the operation of the upstream
first and / or second compressor module, the third compressor module can comprise
a variable frequency drive for adjusting the speed of rotation of the electrical motor
driving the screw compressor of the third screw compressor module, depending on at
least one of pressure level, temperature level, mass flow and composition of the gas
to be provided to the consumer.
[0024] To simplify maintenance, it is also possible that all screw compressor modules use
screw compressors having identical actual inlet volume flows.
To reduce spare parts inventory, it is also possible to uses identical electrical
motors of identical power rating
[0025] Additionally, at least one of the screw compressor modules comprises a cooling unit
at an outlet downstream the screw compressor for cooling the compressed gas. Preferably,
all the screw compressor modules have identical motors of identical power.
[0026] Optionally, at least one of the screw compressor modules comprises a cooling unit
downstream the screw compressor for cooling the compressed gas, thus removing the
heat of compression of the compression stage and thus further improving the efficiency
of the compression arrangement.
[0027] A third aspect for which protection is sought, but which also represents an embodiment
of the present invention according to the first and second aspects, is directed to
ship for transporting liquefied gas comprising a compressor arrangement according
to the invention.
[0028] Regarding further explanations as to the advantages of the compressor arrangement
and its embodiments, reference is explicitly made to the statements in connection
with the method according to the present invention above.
[0029] Further advantages and preferred embodiments of the invention are disclosed in the
following description and figures.
[0030] It is understood by a person skilled in the art that the preceding and the following
features are not only disclosed in the detailed combinations as discussed or showed
in a figure, but that also other combinations of the features can be used without
exceeding the scope of the present invention.
[0031] The invention will now be further described with reference to the accompanying drawings
showing preferred embodiments.
Brief description of the drawings
[0032]
- Fig. 1
- schematically shows a first embodiment of a compressor arrangement for implementing
the method according to the present invention
- Fig. 2
- schematically shows a second embodiment of a compressor arrangement for implementing
the method according to the present invention
Detailed description of the drawings
[0033] In the following, the different embodiments according to the Figures are discussed
comprehensively, same reference signs indicating same or essentially same units. It
is appreciated that a person skilled in the art may combine certain components like
one or more compressor modules, a cooling unit, of an embodiment shown in a figure
with the features of the present invention as defined in the appended claims without
the need to include more than this certain component or even all other components
of this embodiment shown in said figure. In other words, the following figures show
different preferable aspects of the present invention, which can be combined to other
embodiments. The embodiments shown in the figures all relate to the application of
supplying fuel gas from an LNG source, but it is appreciated that a person skilled
in the art can easily transfer the embodiments to applications involving other cryogenic
gases or gas mixtures.
[0034] Figure 1 shows embodiment of a compressor arrangement 100, which receives gas from
a storage tank of liquefied gas 4 through a first line 15 fluidically connecting the
ullage space of the storage tank 4 and the screw compressor arrangement, and compress
the gas to the pressure required by the gas consumer 5
The compressor arrangement 100 comprise two parallel trains, each train comprising
one screw compressor module, i. e. the two screw compressor modules 1, 2 are arranged
in parallel.
The screw compressor module 2 is receiving from the storage tank 4 through a bypass-line
25, the bypass-line 25 branching off the first line 15 upstream of the second compressor
module 2, the bypass line 25 fluidically connecting the second compressor module 2
with the ullage space of the storage tank 4. A valve 26 is placed upstream of the
second compressor module 2 on the bypass line 25.
Each screw compressor module 1 and 2 comprises a screw compressor 13, 23, an electrical
motor 12, 22 to drive the screw compressor, and all other equipments like valves and
instruments of an independent screw compressor module. An independent screw compressor
module is meant to designate a screw compressor module that be operated independently
because the screw compressor of each screw compressor module is driven by its own
electrical motor, without sharing any common equipments with another screw compressor
module.
When the vaporized gas from the source is at cold temperature and rather high pressure,
the density of the gas to be compressed is high and the resulting actual inlet volume
flow at the suction of the compressors is too low for simultaneously operating the
two parallel screw compressor modules 1, 2 at their best efficiency point.
Thus, only the screw compressor module 1 of the two parallel screw compressor modules
1, 2 is in operation for compressing gas, the other screw compressor module 2 in dashed
lines being deactivated and not compressing gas. In addition, the valve 26 disposed
on the bypass line 25 is in closed position, thus isolating the second compressor
module 2 from the storage tank 4.
In some BOG conditions, however, one single compressor module may struggle to maintain
the required fuel gas pressure.
To maintain this required fuel gas pressure, a third screw compressor module 3 located
downstream of the first screw compressor module is operated to increase the number
of compression used for fuel gas compression, thus increasing the outlet pressure
of the compressor arrangement 100.
The third screw compressor module 3 also comprises a screw compressor 33, driven by
an electrical motor 32 and is located downstream the two parallel screw compressor
modules 1, 2.
As only the screw compressor module 1 is operated, the screw compressor module 3 is
only fed with gas compressed by the screw compressor module 1, the screw compressor
module 3 being in series with the screw compressor module 1.
To better adjust the speed of rotation of the screw compressor 33 within the screw
compressor module 3 to the variable suction conditions of the first screw compressor
module 1, the speed of the electrical motor 32 is changed by mean of a variable frequency
drive 31. When the speed of the electrical motor 32 is changed according to the suction
conditions by the variable frequency drive 31, the speed of rotation of the compressor
33 is also changed as the screw compressor is directly driven by the electrical motor.
[0035] The efficiency of the compressor arrangement 100 can be increased by also adjusting
the speed of rotation of the electrical motor 12 driving the first screw compressor
13 with a variable frequency drive 11.
[0036] This allows reaching the best efficiency point for each compressor stage with regards
to the variable suction conditions at the inlet of the compressor arrangement 100.
Thanks to VFD and the downstream screw compressor module, the compression system can
quickly and efficiently adapt to the new suction conditions equivalent to the first
compressor module discharge (typically medium pressure level, 40°C) to efficiently
provide fuel gas to the consumer 5 at the required pressure.
[0037] Optionally, a cooler 14, 24, 34 can be placed downstream each screw compressor module
to remove the heat of compression of the compression stage and thus further improving
the efficiency of the compression arrangement 100.
[0038] Figure 2 shows another embodiment, which is essentially based on the embodiment of
Figure 1.
In this embodiment, when higher mass flow of vaporized gas must be compressed, for
example when higher boil-off gas is generated inside the storage tank 4 during loading
or because of rough see conditions, two parallel screw compressor modules 1, 2 are
operated simultaneously, each being fed in vaporized gas from tank 1. In that case,
the valve 26 placed upstream the second compressor module 2 on the bypass line 25
is in an open position, and gas to be compressed is supplied to the second screw compressor
module 2 through the bypass line 25.
The use of two identical screw compressor modules instead of a single one as in the
first embodiment of figure 1 allows for the compression of the higher flow of gas
from the storage tank.
Similarly, to the first embodiment, a third screw compressor module 3 downstream the
two identical screw compressor modules 1 and 2 is operated to reach higher pressures.
Because the third screw compressor module 3 located downstream the two parallel screw
compressor modules 1, 2 is equipped with a variable frequency drive 31, the speed
of rotation of the screw compressor 33 located within the third screw compressor module
3 can be increased enough to cope with the additional flow of gas compressed by the
two compressors modules 1, 2 located upstream.
In that second embodiment, the second screw compressor module 2 can also be arranged
with its own variable frequency drive 31 to adjust the speed of rotation of the second
motor 22 to get the best efficiency of the second screw compressor 23.
List of reference signs
[0039]
- 1
- (first) compressor module
- 2
- (second) compressor module
- 3
- (third) compressor module
- 4
- Tank, source of liquefied gas
- 5
- Gas consumer
- 11, 21, 31
- Variable frequency drive
- 12, 22, 32
- Motor
- 13, 23, 33
- Screw compressor
- 14, 24, 34
- Cooler
- 15
- First Line
- 25
- Second line
- 26
- Valve
- 100
- Compressor arrangement
1. A method for providing pressurized gas from a source of liquefied gas (4) to a consumer
(5), wherein vaporized gas is supplied via a first line (15) from the source of liquefied
gas (4) to a compressor arrangement (100) for pressurizing the vaporized gas, the
compressor arrangement (100) comprising a first screw compressor module (1) and a
second screw compressor module (2) which are designed according to the redundancy
concept, each screw compressor module (1, 2) comprising an own screw compressor (13,
23) and an own motor (12, 22) for driving the screw compressor (13, 23), wherein the
first screw compressor module (1), being arranged at the first line (15) and being
fed with vaporized gas via the first line (15), is arranged in parallel to the second
screw compressor module (2), the second screw compressor module (2) being arranged
at a bypass-line (25), the bypass-line (25) branching off the first line (15) upstream
of the second screw compressor module (2), wherein the compressor arrangement (100)
is operated such that in a first mode of operation the vaporized gas is fed through
the first line (15) to the first screw compressor module (1) and through the bypass-line
(25) to the second screw compressor module (2) and the first screw compressor module
(1) and the second screw compressor module (2) are in operation, and in a second mode
of operation, the bypass-line (25) is closed with a valve (26) at a position upstream
of the second screw compressor module (2) and the second screw compressor module (2)
is not in operation.
2. The method of claim 1, wherein the speed of rotation of the electrical motor (12,
22) driving the screw compressor (13, 23) of at least one of the screw compressor
modules (1, 2) is adjusted with a variable frequency drive (11, 21) when the screw
compressor module (1, 2) is in operation, depending on at least one of pressure level,
temperature level, mass flow and composition of the gas to be provided to the consumer
(5).
3. The method of claim 1 or claim 2, wherein a third compressor module (3) is connected
in series downstream the first and/or the second screw compressor module (1, 2).
4. The method of claim 3, wherein the speed of rotation of an electrical motor (32) driving
a screw compressor (33) of the third screw compressor module (3) is adjusted with
a variable frequency drive (31), depending on at least one of pressure level, temperature
level, mass flow and composition of the gas to be provided to the consumer (5).
5. The method of any one of the preceding claims, wherein boil-off gas from the source
of liquefied gas (4) is used as the vaporized gas.
6. The method of any one of the preceding claims, wherein gas is cooled by conducting
the gas through a cooling unit (14, 24, 34) arranged downstream of at least one screw
compressor (13, 23, 33).
7. A compressor arrangement (100) for providing pressurized gas from a source of liquefied
gas (4) to a consumer (5), wherein vaporized gas is supplied via a first line (15)
from the source of liquefied gas (4) to the compressor arrangement (100) for pressurizing
the vaporized gas, the compressor arrangement (100) comprising a first screw compressor
module (1) and a second screw compressor module (2) which are designed according to
the redundancy concept, each screw compressor module (1, 2) comprising an own screw
compressor (13, 23) and an own motor (12, 22) for driving the screw compressor (13,
23), wherein the first screw compressor module (1), being arranged at the first line
(15) and being fed with vaporized gas via the first line (15), is arranged in parallel
to the second screw compressor module (2), the second screw compressor module (2)
being arranged at a bypass-line (25), the bypass-line (25) branching off the first
line (15) upstream of the second screw compressor module (2), wherein the compressor
arrangement (100) is operable such that in a first mode of operation the vaporized
gas is fed through the first line (15) to the first screw compressor module (1) and
through the bypass-line (25) to the second screw compressor module (2) and the first
screw compressor module (1) and the second screw compressor module (2) are in operation,
and in a second mode of operation, the bypass-line (25) is closed with a valve (26)
at a position upstream of the second screw compressor module (2) and the second screw
compressor module (2) is not in operation.
8. A compressor arrangement according to claim 7, wherein at least one of the screw compressor
modules (1, 2) comprises a variable frequency drive (11, 21) for adjusting the speed
of rotation of the electrical motor (12, 22) driving the screw compressor (13, 23)
when the screw compressor module (1, 2) is in operation, depending on at least one
of pressure level, temperature level, mass flow and composition of the gas to be provided
to the consumer (5).
9. The compressor arrangement according to claim 7 or 8, wherein the compressor arrangement
(100) comprises a third compressor module (3) connected in series downstream the first
and/or the second screw compressor module (1, 2).
10. The compressor arrangement of according to claim 9, further comprising a variable
frequency drive (31) for adjusting the speed of rotation of an electrical motor (32)
driving a screw compressor (33) of the third screw compressor module (3), depending
on at least one of pressure level, temperature level, mass flow and composition of
the gas to be provided to the consumer (5).
11. The compressor arrangement according to any of claims 7 to 10, wherein all the screw
compressors (13, 23, 33) of the screw compressor modules (1, 2, 3) have identical
actual inlet volume flows.
12. The compressor arrangement according to any of claims 7 to 11, wherein all the screw
compressor modules (1, 2, 3) have identical electrical motors (12, 22, 32) of identical
power rating.
13. The compressor arrangement according to any of claims 7 to 12, wherein at least one
of the screw compressor modules (1, 2, 3) comprises a cooling unit (14, 24, 34) downstream
the screw compressor (13, 23, 33) for cooling the compressed gas.
14. Ship for transporting liquefied comprising a compressor arrangement according to any
of claims 7 to 13.
15. Ship for transporting liquefied gas according to claim 14, wherein the liquefied gas
is transported at cryogenic temperatures.