[0001] This invention relates to a method and apparatus for the reliquefaction of a vapour,
particularly a method and apparatus which are operable on board ship to reliquefy
natural gas vapour.
[0002] Natural gas is conventionally transported over large distances in liquefied state.
For example, ocean going tankers are used to convey liquefied natural gas from a first
location in which the natural gas is liquefied to a second location in which it is
vaporised and sent to a gas distribution system. Since natural gas liquefies at cryogenic
temperatures, i.e. temperatures below - 100°C, there will be continuous boil-off of
the liquefied natural gas in any practical storage system. Accordingly, apparatus
needs to be provided in order to reliquefy the boiled-off vapour. In such an apparatus
a refrigeration cycle is performed comprising compressing a working fluid in a plurality
of compressors, cooling the compressed working fluid by indirect heat exchange, expanding
the working fluid, and warming the expanded working fluid in indirect heat exchange
with the compressed working fluid, and returning the warmed working fluid to one of
the compressors. The natural gas vapour, downstream of a compression stage, is at
least partially condensed by indirect heat exchange with the working fluid being warmed.
One example of an apparatus for performing such a refrigerant method is disclosed
in
US patent 3 857 245.
[0003] According to
US patent 3 857 245 the working fluid is derived from the natural gas itself and therefore an open refrigeration
cycle is operated. The expansion of the working fluid is performed by a valve. Partially
condensed natural gas is obtained. The partially condensed natural gas is separated
into a liquid phase which is returned to storage and a vapour phase which is mixed
with natural gas being sent to a burner for combustion. The working fluid is both
warmed and cooled in the same heat exchanger so that only one heat exchanger is required.
The heat exchanger is located on a first skid-mounted platform and the working fluid
compressors on a second skid-mounted platform.
[0004] Nowadays, it is preferred to employ a non-combustible gas as the working fluid. Further,
in order to reduce the work of compression that needs to be supplied externally, it
is preferred to employ an expansion turbine rather than a valve in order to expand
the working fluid.
[0005] An example of an apparatus which embodies both these improvements is given in
WO-A-98/43029. Now two heat exchangers are used, one to warm the working fluid in heat exchange
with the compressed natural gas vapour to be partially condensed, and the other to
cool the compressed working fluid.
[0006] WO-A-98/43029 points out that incomplete condensation of the natural gas vapour reduces the power
consumed in the refrigeration cycle (in comparison with complete condensation) and
suggests that the residual vapour - which is relatively rich in nitrogen - should
be vented to the atmosphere. Indeed, the partial condensation disclosed in
WO-A-98/43029 follows well known thermodynamic principles which dictate that the condensate yield
is purely a function of the pressure and temperature at which the condensation occurs.
[0007] Typically, the liquefied natural gas may be stored at a pressure a little above atmospheric
pressure and the boil-off vapour may be partially condensed at a pressure of 4 bar.
The resulting partially condensed mixture is typically flashed through an expansion
valve into a phase separator to enable the vapour to be vented at atmospheric pressure.
Even if the liquid phase entering the expansion valve contains as much as 10 mole
per cent of nitrogen at 4 bar, the resulting vapour phase at 1 bar still contains
in the order of 50% by volume of methane. In consequence, in a typical operation,
some 3000 to 5000 kg of methane may need to be vented daily from the phase separator.
Since methane is recognised as a greenhouse gas such a practice would be environmentally
unacceptable.
[0008] Another problem associated with the operation of the apparatus according to
WO-A-98/43029, is that there are considerable thermodynamic inefficiencies caused by a mismatch
between, on the one hand, the temperature and enthalpy of the compressed natural gas
and, on the other hand, the temperature and enthalpy of the working fluid.
[0009] EP-A-1 132 698 discloses a method that mitigates the problems that are caused when vapour is returned
with condensed natural gas to a liquefied natural gas (LNG) storage tank.
[0010] In the method according to
EP-A-1 132 698 the boiled off vapour and/or the natural gas condensate are mixed with liquefied
natural gas taken from storage.
[0011] Since the nitrogen mole fraction in the liquefied natural gas is less than the nitrogen
mole fraction in the boiled-off vapour and even less than that in flash gas formed
by the expansion through the valve of the condensed boil-off vapour, dilution of the
boiled-off vapour with the liquefied natural gas either upstream or downstream of
the condenser, or both, tends to dampen swings in the composition of the vapour phase
in the storage tank that would otherwise occur without the mixing of the boiled off
vapour or natural gas condensate with the liquefied natural gas from storage.
[0012] The method according to
EP-A-1 132 698 does not however greatly enhance the overall thermodynamic efficiency.
[0013] According to the present invention there is provided a method of reliquefying vapour
boiled off from at least one volume of liquefied natural gas held in at least one
storage tank, comprising compressing the vapour in first and second vapour compression
stages in series, condensing the compressed vapour in a condenser by heat exchange
with a working fluid flowing in a main endless working fluid cycle, and returning
at least some of the resulting condensate to the said storage tank, wherein in the
main working fluid cycle the working fluid is, in sequence, compressed in at least
one working fluid compressor, cooled in a first heat exchanger, expanded in an expansion
turbine, employed in the condenser to perform the condensation of the natural gas
vapour, warmed in the said first heat exchanger in heat exchange with the working
fluid being cooled and returned to the said working fluid compressor, characterised
in that in the main working fluid cycle intermediate the passage of the working fluid
through the condenser and its passage through the first heat exchanger, the working
fluid is employed to precool in a second heat exchanger the compressed natural gas
vapour downstream of the second vapour compression stage but upstream of the condenser,
and in that a flow of working fluid is diverted from a region of the main working
fluid cycle where the working fluid is flowing from the condenser to the second heat
exchanger and is passed through at least one third heat exchanger so as to cool the
natural gas vapour intermediate the first and second vapour compression stages, the
diverted working fluid being returned to the main working fluid cycle at a region
where the working fluid is flowing from the second heat exchanger to the first heat
exchanger.
[0014] The invention also provides apparatus for reliquefying natural gas vapour comprising
at least one storage tank for holding at least one volume of liquefied natural gas,
first and second vapour compression stages in series for compressing boiled-off natural
gas vapour communicating with at least one vapour space in the said storage tank,
a condenser for condensing the compressed vapour having a natural gas inlet communicating
with the second vapour compression stage and an outlet communicating with the said
storage tank, wherein the condenser is arranged so as to be cooled, in use, by a working
fluid, the condenser forming part of an endless main working fluid cycle comprising,
in sequence, (a) at least one working fluid compressor for compressing a flow of the
working fluid, (b) a cooling path through a first heat exchanger for cooling the working
fluid flow, (c) an expansion turbine for expanding the flow of working fluid, (d)
the condenser, (e) a warming path through the first heat exchanger for warming the
working fluid, and (f) an inlet to the said working fluid compressor, characterised
in that the main working fluid cycle comprises a second heat exchanger for cooling
the natural gas by heat exchange with the working fluid, the second heat exchanger
having a natural gas vapour path therethrough intermediate the second vapour compression
stage and the condenser and a working fluid path therethrough intermediate the working
fluid outlet from the condenser and the inlet to the warming path through the first
heat exchanger, and in that there is a third heat exchanger for cooling the natural
gas vapour intermediate the first and second natural gas vapour compression stages
by heat exchange with working fluid diverted from the main working fluid cycle, the
third heat exchanger having a working fluid path therethrough communicating at its
inlet with a region of the working fluid cycle intermediate the working fluid outlet
from the condenser and the working fluid inlet to the second heat exchanger and at
its outlet with a region of the working fluid cycle intermediate the working fluid
outlet from the second heat exchanger and the inlet to the warming path through the
first heat exchanger.
[0015] The method and apparatus according to the invention are able to achieve improved
thermodynamic efficiency of operation in comparison with the corresponding methods
and apparatuses disclosed in the prior documents mentioned above. We attribute the
improved thermodynamic efficiency to the integration of the working fluid cycle and
the natural gas condensation not only in the condenser but also in the second and
third heat exchangers. The improvement in thermodynamic efficiency can be exploited
by means of a reduced power consumption.
[0016] Preferably the proportion of the working fluid that is diverted from the main working
fluid cycle to the third heat exchanger is controlled in response to the temperature
at the inlet to the second vapour compression stage.
[0017] Preferably when the said storage tank is fully laden with liquefied natural gas,
the condenser is operated such that sub-cooled liquefied natural gas exits from it.
Sometimes, however, when the said storage tank contains only a relatively small amount
of liquefied natural gas return of the condensate to the tank has the effect of enriching
the boiled-off vapour in nitrogen. In consequence the vapour presented to the condenser
for condensation may contain an excess of nitrogen with the consequence that not only
is the condensate not sub-cooled but it is not even fully condensed. In such circumstances,
or if the storage tank contains a liquefied natural gas having a high nitrogen content,
for example, one that gives a boil-off gas containing 20 to 40% by volume of nitrogen,
the condensate, which contains uncondensed vapour, is flashed into a phase separator,
the resultant liquid phase being returned to the storage tank and the resultant vapour
phase being sent to the ship's engines (in the case of shipboard use if the engines
are powered by natural gas) or is burnt and vented to the atmosphere.
[0018] The first and second vapour compression stages are preferably driven by a single
plural speed motor.
[0019] Preferably the vapour upstream of the first vapour compression stage is precooled
by having mixed therewith a stream of condensed natural gas taken from the condenser.
Preferably the flow rate of the stream of condensed natural gas vapour is controlled
in response to the temperature at the inlet to the first compression stage.
[0020] The method and apparatus according to the invention will now be described by way
of example with reference to the accompanying drawing, in which:
Figure 1 is a schematic flow diagram of a shipboard installation for the storage of
liquefied natural gas (LNG).
[0021] The drawing is not to scale.
[0022] Referring to the drawing, the five thermally-insulated storage tanks 2, 4, 6, 8 and
10 are provided in the hull of a ship or other sea-going vessel (not shown). Two or
more of the storage tanks 2, 4, 6, 8 and 10 are provided with a submerged orifice
pipe 12 located in its bottom region through which LNG is introduced. For reasons
of ease of illustration, the orifice pipes in the tanks 2, 4 and 6 are not shown in
the drawing. If only some of the storage tanks are provided with submerged orifice
pipes, redistribution of returning LNG to tanks not so provided is by operation of
liquid pumps (not shown). The orifice pipe 12 is in normal operation submerged in
a volume 16 of LNG. In each of the tanks 2, 4, 6, 8 and 10 there is a vapour space
18 above the volume 16 of LNG therein.
[0023] Although the storage tanks 2, 4, 6, 8 and 10 are thermally insulated, because LNG
has a boiling point at normal pressures substantially below ambient temperature there
is a continuous evaporation of the LNG in each of the storage tanks 2, 4, 6, 8 and
10. Each of the tanks has a top outlet 22 for vapour which communicates with a boiled-off
gas header 24. Extending from the header 24 is a main pipeline 26 for the boiled-off
gas. Located in the pipeline 26 is a mixer 28, in which, in operation, the vapour
may be mixed with condensed LNG from a downstream part of the installation. In operation,
the condensed LNG evaporates in the boiled-off gas and thereby reduces the temperature
of this gas. A sensor 27 is provided downstream of the mixer and generates signals
representative of the temperature at the inlet to a first compression stage 40, which
signals are relayed to a valve controller 30, which in turn controls the setting of
the flow-control valve 32 in a LNG condensate pipeline 34 that terminates in a spray
nozzle 36 within the mixer 28. The mixer 28 may thus be operated so as to provide
natural gas at a chosen essentially constant cryogenic temperature below, say, minus
100°C to the first compression stage 40.
[0024] The boiled-off gas flows from the mixer 28 into the first compression stage. The
outlet of the first compression stage 40 indirectly communicates with the inlet of
a second compression stage 42. The compression stages 40 and 42 are typically driven
by a single electric motor 44 through, if desired, an integral gearbox 45.
[0025] The motor 44 is typically able to be operated at two different speeds.
[0026] Resulting compressed gas is supplied from the second compression stage 42 to a condenser
46, typically in the form of a plate fin or spirally wound heat exchanger, in which
it is condensed and once condensed subjected to subcooling. The resulting sub-cooled
condensate flows from the condenser 46 along a pipeline 48 to a condensate return
header 50 which feeds the orifice pipes 12 in the bottom regions of the tanks 8 and
10, or if each tank is equipped with the orifice pipe 12, to the tanks 2, 4, 6, 8
and 10.
[0027] Cooling for the condenser 46 is provided by a working or heat exchange fluid such
as nitrogen flowing at a first pressure in an essentially closed refrigeration cycle
60 such as a Brayton cycle.
[0028] In the Brayton cycle 60 nitrogen passing out of the condenser 46 is warmed in heat
exchange with returning compressed nitrogen at a second pressure higher than the first
in a gas-to-gas heat exchanger 62. The resulting warmed nitrogen flows to a compressor
64 which typically comprises three compression stages 66, 68 and 70 all having rotors
(not shown) mounted on an integral gearbox (not shown) or on the same shaft 72 able
to be driven by a motor 74 through a gearbox 75. A first intercooler 78 is located
downstream of the outlet from the first compression stage 66 and upstream of the inlet
to the second compression stage 68. A second intercooler 80 is located downstream
of the outlet from the second compression stage 68 and upstream of the inlet to the
third compression stage 70. An aftercooler 82 is located downstream of the outlet
from the third compression stage 70. The intercoolers 78 and 80 and the aftercooler
82 are typically all cooled by water and are operated so as to remove the heat of
compression from the circulating nitrogen in operation of the Brayton cycle. The resulting
aftercooled compressed nitrogen flow passes through the heat exchanger 63 as the previously
mentioned returning cold nitrogen stream. The compressed nitrogen stream is thus cooled
to a lower temperature in the heat exchanger 62. The compressed cooled nitrogen flow
passes to an expansion turbine 84 where it is expanded with the performance of extra
work. The expansion turbine 84 is typically mounted on the same integral gearbox (not
shown) or on the same shaft as the compression stages 66, 68 and 70. The expansion
turbine 84 thus helps to drive the compression stages 66, 68 and 70. The expansion
of the nitrogen in the turbine 84 generates the refrigeration necessary for the condensation
of the natural gas vapour in the condenser 46. The nitrogen thus continuously passes
through an endless circuit.
[0029] A particular feature of the Brayton cycle 60 illustrated in the drawing is that the
nitrogen does not pass directly from the condenser 46 to the heat exchanger 62. Instead
it passes through a second gas-to-gas countercurrent heat exchanger 86. The purpose
of this heat exchanger is to pre-cool the natural gas to a temperature close to its
condensation temperature upstream of entering the condenser 46. During typical operating
conditions when the tanks 2, 4, 6, 8 and 10 are fully laden with LNG the natural gas
is consequently not only liquefied but also sub-cooled in the condenser 46. The sub-cooling
of the liquefied natural gas keeps down the formation of flash gas when the LNG is
returned to the tanks.
[0030] A further feature of the particular form of Brayton cycle 6 shown in the drawings
is that a part of the nitrogen is withdrawn from a region of the Brayton cycle downstream
of the outlet from the condenser 46 but upstream of the inlet to the second heat exchanger
86 and flows through a third heat exchanger 88 which is located downstream of the
first natural gas compression stage 40 but upstream of the second natural gas compression
stage 42 and thus serves to remove the heat of compression generated in the natural
gas by operation of the first compression stage 40. As a result, the nitrogen passing
through the third heat exchanger 88 is warmed. The warmed nitrogen flow is returned
to the Brayton cycle 60 at a region downstream of the outlet from the second heat
exchanger 86 but upstream of the inlet to the warming passages through the first heat
exchanger 62. Typically, a control valve 90 controls the rate of flow of nitrogen
working fluid through the third heat exchanger in response to a temperature sensor
(not shown) at the inlet to the second natural gas compression stage 42. In a typical
arrangement, the control valve 90 operates to maintain a constant temperature at the
inlet to the second natural gas compression stage 42.
[0031] Not all the natural gas that is liquefied in the condenser 46 is typically returned
via the pipeline 50 to the tanks 2, 4, 6, 8 and 10. A portion of the condensate is
sent via the pipeline 34 to the mixer 28 so as to pre-cool the natural gas upstream
of the first compression stage 40.
[0032] In operation, there are various ways of operating the apparatus shown in the drawing
according to how laden with LNG the tanks 2, 4, 6, 8 and 10 are. When these tanks
are fully laden, the temperature at the inlet to the first natural gas compression
stage 40 is typically in the order of minus 100°C or even lower. The pressure at the
inlet is typically a little above 1 bar. The natural gas typically leaves the first
compression stage at a temperature of minus 65°C and a pressure in the order of 2
bar. The gas is typically cooled in the heat exchanger to a temperature in the order
of minus 130°C and enters the second natural gas compression stage at this temperature.
The natural gas typically leaves the second compression stage 42 at a pressure in
the order of 5 bar and a temperature of about minus 75°C. The natural gas is cooled
in the second heat exchanger to a temperature at which it will begin to condense.
The exact value of this temperature will depend on the composition of the natural
gas. The greater the mole fraction of nitrogen in the natural gas, the lower will
be the temperature at which it starts to condense. Because the condenser 46 is not
required to desuperheat the natural gas in normal operation, more efficient heat exchange
is made possible than in previously known cycles in which the corresponding condenser
has been required both to desuperheat and to condense the natural gas. As a result
of the intercooling, desuperheating and separate condensing with subcooling, the power
consumption of the refrigeration cycle is reduced.
[0033] As previously stated, the natural gas leaves the condenser 46 as a sub-cooled liquid.
Typically, its exit temperature is in the order of minus 165°C depending on the composition
of the natural gas. One of the advantages of such a low exit temperature is that relatively
little, if any, flash gas is formed on reintroduction of the LNG into the tanks 2,
4, 6, 8 and 10 through the orifice pipes 12. Moreover, when the tanks are fully laden,
any flash gas that is formed may be dissolved or condensed in the liquid before it
reaches the surface.
[0034] During normal operation when the tanks are fully laden the expansion turbine 84 typically
has an inlet temperature in the order of minus 104°C, an outlet temperature in the
order of minus 168°C, and an outlet pressure in the order of 10 bar. If the composition
of the natural gas is, say, 8.5% by volume of nitrogen and 91.5% by volume of methane,
this temperature is sufficiently low for the condensate produced in the condenser
46 to have a desired degree of sub-cooling. Sometimes, however, the ship in which
the tanks 2, 4, 6, 8 and 10 are located is required to transport sufficiently less
than the maximum amount of LNG for the liquid head in the tanks not to be sufficient
to prevent flashing of condensate returned through the orifice pipes 12 or to ensure
complete dissolution of fine bubbles of flash gas that are formed in the volumes 16
of LNG. As a result, the vapour that flows from the tanks 2, 4, 6, 8 and 10 to the
first compression stage 40 is enriched in nitrogen. As a consequence, its condensation
temperature at the outlet pressure of the second natural gas vapour compression stage
42 falls. Indeed, when the tanks are relatively lightly laden with LNG the degree
of enrichment may become so great that the condenser 46 no longer fully condenses
the vapour. In this case, instead of being passed to the conduit 50, the mixture of
condensate and uncondensed vapour may be selectively directed through a valve 100
into a phase separator 102. Liquid is withdrawn from the bottom of the phase separator
102 and sent to the conduit 50. Vapour passes from the phase separator 102 to a vent
line 104 which leads through a heater 106 to a gas combustion unit 108 so that the
natural gas content of the vapour may be burned and the resulting combustion gases
vented to the atmosphere.
[0035] The minimum and maximum flows of natural gas vapour in operation of the apparatus
shown in the drawing can vary widely. It is therefore typically preferred to employ
two sets of first and second natural gas compression stages 40 and 42, the two sets
being in parallel with one another. Thus, there are typically two third heat exchangers
88 in parallel with one another. Whether one or both sets are used depends on the
rate of vaporisation of the natural gas in the tanks 2, 4, 6, 8 and 10. Similarly,
they may be two or more sets of nitrogen compression stages 66, 68 and 70 in parallel,
and two or more expansion turbines 84 in parallel.
1. A method of reliquefying vapour boiled off from at least one volume of liquefied natural
gas held in at least one storage tank, comprising compressing the vapour in first
and second vapour compression stages in series, condensing the compressed vapour in
a condenser by heat exchange with a working fluid flowing in a main endless refrigeration
cycle, and returning at least some of the resulting condensate to the said storage
tank, wherein in the main working fluid cycle the working fluid is, in sequence, compressed
in at least one working fluid compressor, cooled in a first heat exchanger, expanded
in an expansion turbine, employed in the condenser to perform the condensation of
the natural gas vapour, warmed in the said first heat exchanger in heat exchange with
the working fluid being cooled and returned to the said working fluid compressor,
characterised in that in the main working fluid cycle intermediate the passage of the working fluid through
the condenser and its passage through the first heat exchanger, the working fluid
is employed to pre-cool in a second heat exchanger the compressed natural gas vapour
downstream of the second vapour compression stage but upstream of the condenser, and
in that a flow of working fluid is diverted from a region of the main working fluid cycle
where the working fluid is flowing from the condenser to the second heat exchanger
and is passed through at least one third heat exchanger so as to cool the natural
gas vapour intermediate the first and second vapour compression stages, the diverted
working fluid being returned to the main working fluid cycle at a region where the
working fluid is flowing from the second heat exchanger to the first heat exchanger.
2. A method according to claim 1, in which the proportion of the working fluid that is
diverted from the main working fluid cycle to the third heat exchanger is controlled
in response to the temperature at the inlet to the second vapour compression stage.
3. A method according to claim 1 or claim 2, wherein when the said storage tank is fully
laden with liquefied natural gas the condenser is operated such that sub-cooled liquefied
natural gas exits from it.
4. A method according to any one of the preceding claims, in which the vapour upstream
of the first vapour compression stage is pre-cooled by having mixed therewith a stream
of condensed natural gas taken from the condenser.
5. A method according to claim 4, in which the flow rate of the stream of condensed vapour
is controlled in response to the temperature at the inlet to the first compression
stage.
6. Apparatus for reliquefying natural gas vapour comprising at least one storage tank
for holding at least one volume of liquefied natural gas, first and second vapour
compression stages in series for compressing boiled-off natural gas vapour communicating
with at least one vapour space in the said storage tank, a condenser for condensing
the compressed vapour having a natural gas inlet communicating with a second vapour
compression stage and an outlet communicating with the said storage tank, wherein
the condenser is arranged so as to be cooled, in use, by a working fluid, the condenser
forming part of an endless main working fluid cycle comprising, in sequence, (a) at
least one working fluid compressor for compressing a flow of the working fluid, (b)
a cooling path through a first heat exchanger for cooling the working fluid flow,
(c) an expansion turbine for expanding the flow of working fluid, (d) the condenser,
(e) a warming path through the first heat exchanger for warming the working fluid,
and (f) an inlet to the said working fluid compressor, characterised in that the main working fluid cycle comprises the second heat exchanger for cooling the
natural gas by heat exchange with the working fluid, the second heat exchanger having
a natural gas vapour path therethrough intermediate the second vapour compression
stage and the condenser and a working fluid path therethrough intermediate the working
fluid outlet from the condenser and the inlet to the warming path through the first
heat exchanger, and in that there is a third heat exchanger for cooling the natural gas vapour intermediate the
first and second natural gas vapour compression stages by heat exchange with working
fluid diverted from the main working fluid cycle, the third heat exchanger having
a working fluid path therethrough communicating at its inlet with a region of the
working fluid cycle intermediate the working fluid outlet from the condenser and the
working fluid inlet to the second heat exchanger and at its outlet with a region of
the working fluid cycle intermediate the working fluid outlet from the second heat
exchanger and the inlet to the warming path through the first heat exchanger.
7. Apparatus according to claim 6, wherein there is a valve for controlling the proportion
of the working fluid that is diverted from the main working fluid cycle to the third
heat exchanger in response to the temperature at the inlet to the second vapour compression
stage.
8. Apparatus according to claim 6 or claim 7, in which the first and second vapour compression
stages are driven by a single plural speed motor.
9. Apparatus according to any one of claims 6 to 8, additionally including a mixer upstream
of the first vapour compression stage in which the natural gas vapour is able to be
cooled, the mixer having an inlet for condensed natural gas communicating with the
condenser.
10. Apparatus according to claim 9, including a valve for controlling the flow of condensate
to the mixer and operable to maintain constant the temperature at the inlet to the
first compression stage.
11. Apparatus according to any one of claims 6 to 10, wherein an outlet for condensate
from the condenser is able selectively to be placed through an expansion valve in
communication with a phase separator having an outlet for returning liquid to the
storage tank and an outlet for passing vapour to a combustion unit.