[0001] This invention relates to a process for recovering the cold deriving from liquid
methane gasification.
[0002] As methane has to be obtained from many regions of the world, it is not always possible
to use usual methane pipelines, and instead methane tankers specialized for this purpose
have to be used.
[0003] To be able to transport the maximum quantity of methane, these tankers are designed
to transport it in liquid form in order to reduce its volume. However to remain in
the liquid state, the methane has to be maintained at cryogenic temperature, the value
of which depends on the storage pressure (for example -154°C at 2 bar absolute).
[0004] In methane tankers the methane is contained in suitable tanks under high thermal
insulation (using the Dewar flask principle).
[0005] On reaching land, this methane has to be transported or used in gaseous form, and
must therefore be vaporized and heated. To express this concept in other words, it
could be said that in order to undergo vaporization and heating, it must transfer
its "cold" to another fluid, which hence itself becomes cold during said heat transfer.
[0006] In this respect, it is known that to cool a gas to a temperature less than the temperature
of the environment in which it is present requires considerable energy consumption
related to the application of usual thermodynamic refrigeration cycles.
[0007] Substantially, this energy consumption is imposed by the need to compress the gas
to be liquefied so that it becomes hot, and then to extract from it the heat associated
with the temperature increase deriving from this compression more efficiently as it
is effected at a higher temperature level. Subsequent expansion of the compressed
and cooled gas in a turbine further reduces its temperature to cryogenic values, with
resultant liquefaction of the gas.
[0008] Hence on this basis, liquid methane transported by methane tankers contains a "negative
energy" or cold, which it would be extremely advantageous to recover.
[0009] In this respect, one of the usual methods of heating liquid methane is to pass the
liquid methane through a heat exchanger through which water circulates in counter-current
to heat said methane from a temperature of -150°C to a temperature of +15°C.
[0010] Besides not providing any energy recovery, this gasification method alters the ecosystem
as it causes artificial intermittent cooling of the sea.
[0011] This is because the water used to heat the methane is withdrawn from the sea, cooled
and then returned to the sea at a temperature lower than that at which it was withdrawn.
[0012] Because of the progressive importance assumed by methane traffic, current research
is aimed at recovering the cold possessed by liquid methane in liquid air production
cycles (Linde machine, Claude machine).
[0013] These cycles consist of repeated compression, cooling and expansion until the air
becomes liquid at a temperature of -195°C.
[0014] More specifically, the known art uses the said cold mainly during cooling by suitable
heat exchangers.
[0015] However this known art does not provide a technical basis suitable for using the
said cold offered by liquid methane in a manner able to reduce the energy consumption
relating to the cooling and liquefaction of technical gases normally used in industry
(nitrogen, oxygen, argon).
[0016] To illustrate these concepts with numerical examples, expressive of current industrial
reality, 13,000 kWh are required to liquefy 25,000 Normal (atmospheric pressure, 0°C)
cubic metres of nitrogen.
[0017] If the cold yielded by liquid methane during its gasification or expansion to ambient
temperature is used with current techniques, this energy consumption is reduced to
only 8,400 kWh, hence saving 4,600 kWh.
[0018] This is evidently a considerable saving, but which could be better utilized if a
method could be found for using the said cold to liquefy industrial gases in a more
direct manner within the liquefaction process.
[0019] An object of the present invention is to define a process for using the cold deriving
from liquid methane gasification which is more advantageous than those currently used.
[0020] This and other objects which will be more apparent hereinafter will be seen to have
been attained on reading the ensuing description of a process for recovering the cold
deriving from liquid methane gasification characterised by cooling with the liquid
methane a cryogenic fluid, preferably nitrogen, then using said cryogenic fluid as
the cooling fluid in two nitrogen compressor units of a liquefier, both for the interstage
coolers and for the intake and final delivery coolers.
[0021] Nitrogen, assuming that to be the cryogenic fluid compressed by a first of said compressor
units, is liquefied in a heat exchanger by further nitrogen circulating in closed
cycle which is continuously compressed by a second compressor unit and then expanded
in a cryogenic turbine to achieve final cooling to a temperature of -190°C. The nitrogen
cooled by the turbine in this manner is used to cool all the nitrogen compressed by
the first compressor unit until a temperature of -180°C is attained, at which the
nitrogen liquefies. The liquid nitrogen produced in this manner is then used in the
air fractionation plant to produce liquid oxygen, nitrogen and argon, and for all
other possible uses of liquid nitrogen.
[0022] The invention is illustrated by way of non-limiting example in the accompanying drawing,
which shows a general scheme of a plant for implementing the process.
[0023] With reference to said drawing, a liquid methane inlet line 1 leads to a pump 2.
The pump 2 (indicatively of centrifugal type) feeds the liquid methane to a heat exchanger
4, which subtracts heat from a line 5 through which nitrogen passes in counter-current.
[0024] This nitrogen originates from another heat exchanger 6 in which a water line 7 had
previously raised its temperature from about -98°C to about -34°C.
[0025] Said nitrogen is maintained at a relatively high pressure to increase the temperature
difference between the methane and nitrogen in order, other conditions being equal,
to achieve greater absorption of the cold provided by the liquid methane.
[0026] The nitrogen cooled in this manner by heat transfer with liquid methane leaves the
heat exchanger 4 through a line 8, which branches into two lines 9 and 10 to enable
the cold of the nitrogen to be used to cool the nitrogen circulating within specific
circuits 16, 20 of the apparatus in which said nitrogen is liquefied.
[0027] More precisely, the line 9 conveys the cold withdrawn from the methane to the interstage
coolers (heat exchangers) 11, 12, 13 located respectively at the outlet of three stages
16, 15, 14 of a conventional compressor unit for the nitrogen in the circuit 18, which
is of closed type.
[0028] At the outlet of the interstage cooler 11 the nitrogen of the closed circuit 18,
cooled in this manner, has a pressure of about 10 bar and a temperature of about -141°C.
[0029] In this state it is expanded through a conventional cryogenic turbine 17 by which
its temperature falls to -190°C and its pressure to 1.4 bar.
[0030] The nitrogen, cooled in this manner in the closed circuit 18, passes through a heat
exchanger 16 to absorb heat from the nitrogen compressed in an open circuit 20.
[0031] This open circuit 20 comprises an inlet line 21, into which gaseous nitrogen is fed
at a pressure of 1.15 bar absolute and a temperature of +15°C. This nitrogen undergoes
successive compressions by a compressor unit composed of a first stage 22, a second
stage 23, a third stage 24, a fourth stage 25 and a fifth stage 26.
[0032] The nitrogen of the open circuit 20 undergoes the following cooling sequence: cooling
implemented by an intake heat exchanger 27, cooling implemented by a plurality of
interstage heat exchangers (28, 29, 30, 31) and further cooling implemented by a final
heat exchanger 32 upstream of said heat exchanger 19 located in the final part of
said open circuit 20.
[0033] Said heat exchangers 27, 28, 29, 30, 31 32, subtract heat from the nitrogen of the
open circuit 20 by transferring to it the cold present in the nitrogen passing through
the line 10, itself cooled by the cold subtracted from the liquid methane in the heat
exchanger 4.
[0034] After collecting heat through the respective heat exchangers 11, 12, 13, 27, 28,
29, 30, 31, 32, the nitrogen of the two lines 9 and 10 flows into a common line 33,
through which the nitrogen is fed to a compressor 34 which circulates it at a pressure
of about 70 bar along the paths already described and in the directions indicated
by the arrows.
[0035] As a result of this, the nitrogen enters the open circuit 20 in the gaseous state
through the line 21 and leaves in the liquid state through a line 3, by optimum use
of the cold deriving from the vaporization of the liquid methane.
[0036] The liquid nitrogen produced in this manner can itself be used in the usual air fractionation
plants to produce liquid oxygen, nitrogen and argon, and in addition for all the usual
possible uses of liquid nitrogen.
[0037] Advantageously, the process for recovering cold from liquid methane by liquid nitrogen
production cycles in the aforedescribed manner results in substantial energy savings.
[0038] With reference to the already stated real numerical values referring to a volume
of 25,000 Normal cubic metres of nitrogen, the energy consumption using this process
decreases to only 3,700 kWh, so drastically reducing the current energy requirement
using the common liquefaction methods (for nitrogen liquefaction).
1. A process for recovering the cold deriving from liquid methane gasification, characterised by cooling with the liquid methane (1) a cryogenic fluid (5), preferably nitrogen, and
then using said cryogenic fluid as coolant fluid in two compressor units (14-15-16,
22-23-24-25-26) for said nitrogen cryogenic fluid, both for the interstage coolers
(11, 12, 13, 27, 28, 29, 30, 31, 32) and for the intake and final delivery coolers
(27, 32), the cryogenic fluid (3) compressed by a first of said compressor units (22-23-24-25-26)
being liquefied in a heat exchanger (19) by the action of another cryogenic fluid
circulating in closed circuit, which is continuously compressed by a second of said
compressor units (14-15-16) and then expanded through a cryogenic turbine (17) to
achieve cooling to a temperature lower than the liquefaction temperature of the cryogenic
fluid.
2. A process as claimed in claim 1, wherein the cryogenic fluid is nitrogen which by
cooling through the cryogenic turbine (17) is brought to a temperature of -190°C so
as to obtain liquefaction of the nitrogen on reaching -180°C through said heat exchanger
(19), the liquid nitrogen leaving through a controlled line (3) of said open circuit.
3. A process as claimed in claim 2, wherein the nitrogen is used in an air fractionation
plant for the production of liquid oxygen, nitrogen and argon or for other possible
uses of liquid nitrogen.
4. An apparatus for implementing the process, characterised in that the cryogenic fluid (preferably nitrogen) circulating within a first closed circuit
(33) is cooled by liquid methane via heat exchanger means (4), said cooled cryogenic
fluid being used to cool within a second closed circuit (18) another separate cryogenic
fluid, said second closed circuit comprising compressor means (14, 15, 16), expander
means (17) and heat exchanger means (19), and to cool and liquefy in an open circuit
(20) a further separate cryogenic fluid, said open circuit comprising compressor means
(22-26) and heat exchanger means (32), said further cryogenic fluid circulating through
said heat exchanger means (19) of said second closed circuit (18) before leaving said
open circuit (20).