Method for leak testing a sealed and thermally insulating tank for storing a fluid
A method is described for checking the sealing of a sealed and thermally insulating tank for storing a liquefied gas at low temperature. The tank has a primary space and a secondary space where, in order to perform the check, a difference in pressure is created between the two spaces at least some of the inert gas injected into the primary space is recovered via at least one secondary outlet of the secondary space so as to be reinjected into the primary space.
1 . A method for checking the sealing of a sealed and thermally insulating tank ( 1 ) for storing a liquefied gas at low temperature ( 30 ), the tank ( 1 ) being at low temperature ( 30 ), the tank ( 1 ) comprising a carrier structure which has an inner hull ( 2 ) and an outer hull ( 3 ), a confined space ( 4 ) between the inner hull ( 2 ) and the outer hull ( 3 ), a primary sealing membrane ( 9 ) which is intended to be in contact with the liquefied gas at low temperature ( 30 ) contained in the tank ( 1 ), and a secondary sealing membrane ( 7 ) which is arranged between the primary sealing membrane ( 9 ) and the inner hull ( 2 ), a primary space ( 8 ) between the primary sealing membrane ( 9 ) and the secondary sealing membrane ( 7 ) and a secondary space ( 6 ) between the secondary sealing membrane ( 7 ) and the inner hull ( 2 ), the primary space ( 8 ) and the secondary space ( 6 ) comprising insulating materials, the primary space ( 8 ) comprising at least one primary gas inlet ( 18 ) and the secondary space ( 6 ) comprising at least one secondary gas outlet ( 19 ), said primary sealing membrane resting directly on the insulating materials contained in the primary space and said secondary sealing membrane resting directly on the insulating materials contained in the secondary space, the method comprising the following successive steps for detecting the location of a sealing defect of the secondary sealing membrane ( 7 ) in the form of a cold spot on the outer surface of the inner hull ( 2 ):
a step referred to as main step in which the secondary space ( 6 ) is brought to a pressure lower than the pressure of the primary space ( 8 ), with a pressure differential P 1 , by injecting an inert gas into the primary space via the primary gas inlet ( 18 ) and causing gas to be expelled or drawn from the secondary gas outlet ( 19 ) of the secondary space and then by measuring the temperature of an outer surface of the inner hull ( 2 ) from the confined space ( 4 ) situated around the inner hull ( 2 );
a step referred to as a subsequent step in which the temperature of the outer surface of the inner hull ( 2 ) is measured from the confined space ( 4 ) under the normal operating conditions of the tank ( 1 );
characterized in that, during the main step, at least some of the inert gas injected into the primary space ( 8 ) is recovered by at least one secondary outlet ( 19 , 20 or 23 ) of the secondary space ( 6 ) and is reinjected into the primary space ( 8 ).
2 . The method as claimed in claim 1 , wherein the entirety of the inert gas injected into the primary space ( 8 ) is reinjected into said space ( 8 ) after having been recovered by at least one suction means ( 80 ) connected to a secondary outlet ( 19 , 20 or 23 ) of the secondary space ( 6 ).
3 . The method as claimed in claim 1 , wherein just some of the inert gas injected into the primary space ( 8 ), advantageously representing between 20% and 80% of the inert gas injected into the primary space ( 80 ), is reinjected into said space ( 8 ) after having been recovered by at least one suction means ( 80 ) connected to a secondary outlet of the secondary space ( 6 ).
4 . The method as claimed in claim 1 , wherein said method comprises a step referred to as preliminary step in which the temperature of the outer surface of the inner hull ( 2 ) is measured from the confined space ( 4 ) under the normal operating conditions of the tank ( 1 ).
5 . The method as claimed in claim 1 , wherein the pressure differential P 1 is:
comprised between 500 Pa and 1500 Pa for a duration of at least 10 hours, or
comprised between 1800 Pa and 3200 Pa.
6 . The method as claimed in claim 1 , wherein the step referred to as the main step is preceded by a step referred to as an intermediate step in which the secondary space ( 6 ) is brought to a pressure lower than the pressure of the primary space ( 8 ), with a pressure differential of between 500 Pa and 1500 Pa by injecting an inert gas into the primary space via the primary gas inlet ( 18 ) and causing gas to be expelled or drawn from the secondary gas outlet ( 19 ) of the secondary space and then by measuring the temperature of an outer surface of the inner hull ( 2 ) from the confined space ( 4 ) situated around the inner hull ( 2 ).
7 . The method as claimed in claim 1 , wherein the inert gas consists of nitrous oxide.
8 . The method as claimed in claim 1 , wherein the duration of each temperature measurement is at the most five hours.
9 . The method as claimed in claim 1 , wherein P 1 , advantageously the pressure differential of the step referred to as the intermediate step, is kept stable while the temperature is being measured.
10 . A floating or onshore storage installation for a liquefied gas at low temperature ( 30 ), comprising:
a tank ( 1 ) at low temperature ( 30 ) comprising a carrier structure which has an inner hull ( 2 ) and an outer hull ( 3 ), the space between the inner hull ( 2 ) and the outer hull ( 3 ) being referred to as the confined space ( 4 ), a primary sealing membrane ( 9 ) which is intended to be in contact with the liquefied gas at low temperature ( 30 ) contained in the tank, and a secondary sealing membrane ( 7 ) which is arranged between the primary sealing membrane ( 9 ) and the inner hull ( 2 ), the space between the primary sealing membrane ( 9 ) and the secondary sealing membrane ( 7 ) is referred to as the primary space ( 8 ) and the space between the secondary sealing membrane ( 7 ) and the inner hull ( 2 ) is referred to as the secondary space ( 6 ), the primary space ( 8 ) and the secondary space ( 6 ) comprising insulating materials, the primary space ( 8 ) comprising at least one primary gas inlet ( 18 ), the secondary space ( 6 ) comprising at least one secondary gas outlet ( 19 ), said primary sealing membrane resting directly on the insulating materials contained in the primary space and said secondary sealing membrane resting directly on the insulating materials contained in the secondary space,
an inert gas reservoir ( 16 ) which is arranged in order to inject inert gas into the primary space ( 8 ) through the primary gas inlet,
an injection device ( 45 ) which is capable of injecting inert gas of the inert gas reservoir ( 16 ) via the primary gas inlet ( 18 ), and thus placing the primary space ( 8 ) under pressure relative to the secondary space ( 6 ),
a suction device ( 80 , 80 ′) which is connected to the secondary gas outlet ( 19 ) in order to generate a lower pressure in the secondary space ( 6 ) than the pressure in the primary space ( 8 ),
a device for measuring the temperature of the outer surface of the inner hull ( 2 ),
a system for displaying the temperature measurements in order to locate a sealing defect of the secondary sealing membrane ( 7 ) in the form of a cold spot on the outer surface of the inner hull ( 2 ),
characterized in that the suction device comprises at least one suction means ( 80 ) consisting of a pump that draws at least some of the inert gas out of the secondary space ( 6 ) and reinjects it into the primary space ( 8 ) via the aforesaid injection device ( 45 ).
11 . The installation as claimed in claim 10 , wherein the aforesaid suction means ( 80 ) forms the only suction means ( 80 ) of said device such that all of the inert gas recovered in the secondary space ( 6 ) is reinjected into the primary space ( 8 ).
12 . The installation as claimed in claim 10 , wherein the suction device also comprises at least one suction system ( 80 ′) recovering the inert gas and not reinjecting it into the primary space ( 8 ).
13 . The installation as claimed in claim 12 , wherein the suction system ( 80 ′) is a Venturi effect suction system ( 80 ′) which comprises a main pipe ( 83 ) which has an inlet which is capable of being connected to a pressurized gas source ( 71 ), and an outlet toward the outer side of the tank ( 1 ), a suction pipe ( 81 ) having an upstream side which is capable of being connected to the outlet port of the secondary space ( 6 ) and a downstream side which opens laterally in a convergent/divergent section of the main pipe ( 83 ) so that a gas flow in the main pipe ( 83 ) produces a reduced pressure in the suction pipe ( 81 ).
14 . The installation as claimed in claim 13 , wherein the pressurized gas source ( 71 ) is a compressed air circuit.
15 . The installation as claimed in claim 10 , wherein the injection device ( 45 ) comprises a compressor which is capable of injecting the inert gas from the inert gas reservoir ( 16 ) at a pressure between 3 and 8 bar.
16 . A vessel ( 100 ) for transporting a liquefied gas at low temperature ( 30 ), the vessel comprising an installation for storing a liquefied gas at low temperature ( 30 ) as claimed in claim 10 .