EP3881002A1 - Verfahren zur steuerung eines kryotanks, entsprechender kryotank und entsprechendes unterwasserbauwerk - Google Patents

Verfahren zur steuerung eines kryotanks, entsprechender kryotank und entsprechendes unterwasserbauwerk

Info

Publication number
EP3881002A1
EP3881002A1 EP19801564.6A EP19801564A EP3881002A1 EP 3881002 A1 EP3881002 A1 EP 3881002A1 EP 19801564 A EP19801564 A EP 19801564A EP 3881002 A1 EP3881002 A1 EP 3881002A1
Authority
EP
European Patent Office
Prior art keywords
liquid phase
temperature
parameter representative
pressure
cryogenic tank
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
EP19801564.6A
Other languages
English (en)
French (fr)
Inventor
Yannick RIO
Caroline SOLEILHAC
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Naval Group SA
Original Assignee
Naval Group SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Naval Group SA filed Critical Naval Group SA
Publication of EP3881002A1 publication Critical patent/EP3881002A1/de
Pending legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C13/00—Details of vessels or of the filling or discharging of vessels
    • F17C13/02—Special adaptations of indicating, measuring, or monitoring equipment
    • F17C13/026—Special adaptations of indicating, measuring, or monitoring equipment having the temperature as the parameter
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63G—OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
    • B63G8/00—Underwater vessels, e.g. submarines; Equipment specially adapted therefor
    • B63G8/08—Propulsion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C13/00—Details of vessels or of the filling or discharging of vessels
    • F17C13/02—Special adaptations of indicating, measuring, or monitoring equipment
    • F17C13/025—Special adaptations of indicating, measuring, or monitoring equipment having the pressure as the parameter
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00—Vessel construction, in particular walls or details thereof
    • F17C2203/03—Thermal insulations
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2221/00—Handled fluid, in particular type of fluid
    • F17C2221/01—Pure fluids
    • F17C2221/011—Oxygen
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
    • F17C2223/0146—Two-phase
    • F17C2223/0153—Liquefied gas, e.g. LPG, GPL
    • F17C2223/0161—Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/03—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
    • F17C2223/033—Small pressure, e.g. for liquefied gas
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2250/00—Accessories; Control means; Indicating, measuring or monitoring of parameters
    • F17C2250/03—Control means
    • F17C2250/032—Control means using computers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2250/00—Accessories; Control means; Indicating, measuring or monitoring of parameters
    • F17C2250/03—Control means
    • F17C2250/036—Control means using alarms
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2250/00—Accessories; Control means; Indicating, measuring or monitoring of parameters
    • F17C2250/04—Indicating or measuring of parameters as input values
    • F17C2250/0404—Parameters indicated or measured
    • F17C2250/0408—Level of content in the vessel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2250/00—Accessories; Control means; Indicating, measuring or monitoring of parameters
    • F17C2250/04—Indicating or measuring of parameters as input values
    • F17C2250/0404—Parameters indicated or measured
    • F17C2250/0421—Mass or weight of the content of the vessel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2250/00—Accessories; Control means; Indicating, measuring or monitoring of parameters
    • F17C2250/04—Indicating or measuring of parameters as input values
    • F17C2250/0404—Parameters indicated or measured
    • F17C2250/043—Pressure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2250/00—Accessories; Control means; Indicating, measuring or monitoring of parameters
    • F17C2250/04—Indicating or measuring of parameters as input values
    • F17C2250/0404—Parameters indicated or measured
    • F17C2250/043—Pressure
    • F17C2250/0434—Pressure difference
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2250/00—Accessories; Control means; Indicating, measuring or monitoring of parameters
    • F17C2250/04—Indicating or measuring of parameters as input values
    • F17C2250/0404—Parameters indicated or measured
    • F17C2250/0439—Temperature
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2250/00—Accessories; Control means; Indicating, measuring or monitoring of parameters
    • F17C2250/04—Indicating or measuring of parameters as input values
    • F17C2250/0486—Indicating or measuring characterised by the location
    • F17C2250/0491—Parameters measured at or inside the vessel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2250/00—Accessories; Control means; Indicating, measuring or monitoring of parameters
    • F17C2250/04—Indicating or measuring of parameters as input values
    • F17C2250/0486—Indicating or measuring characterised by the location
    • F17C2250/0495—Indicating or measuring characterised by the location the indicated parameter is a converted measured parameter
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2260/00—Purposes of gas storage and gas handling
    • F17C2260/01—Improving mechanical properties or manufacturing
    • F17C2260/015—Facilitating maintenance
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2260/00—Purposes of gas storage and gas handling
    • F17C2260/02—Improving properties related to fluid or fluid transfer
    • F17C2260/026—Improving properties related to fluid or fluid transfer by calculation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2270/00—Applications
    • F17C2270/01—Applications for fluid transport or storage
    • F17C2270/0102—Applications for fluid transport or storage on or in the water
    • F17C2270/0131—Submarines

Definitions

  • the present invention relates to a method for controlling a cryogenic tank comprising an enclosure containing a liquefied gas, the liquefied gas forming a liquid phase and a gaseous phase in the enclosure, the method comprising the following step: measurement of a parameter representative of a pressure in the gas phase and a parameter representative of a pressure in the liquid phase.
  • the invention also relates to a cryogenic tank and an underwater building comprising such a tank.
  • Anaerobic propulsion systems (or Al P, abbreviation for Air Independent Propulsion in English) are a relatively recent type of energy production system for submarines that can operate for a long time without using outside air. This prevents the anaerobic submarine from taking out its tube of fresh air (or snorkel), thus limiting the need for ascent close to the surface, and therefore its vulnerability.
  • the anaerobic propulsion system provides conventional submarines with a significant improvement in their diving autonomy (a few days, compared to a few dozen hours for a conventional propelled submarine) and therefore their discretion.
  • Anaerobic propulsion systems include in particular conventional combustion engines using standard fuel, such as diesel engines, and as an oxidizer of oxygen stored in liquid form on board the submarine, in a cryogenic tank. Liquid dioxygen can also be used to replenish part of the air breathed by the crew, which further increases autonomy.
  • a cryogenic tank may require purges to the outside of the building, which need to be anticipated as part of a mission requiring stealth.
  • cryogenic tank poses a certain number of difficulties, in particular in an underwater building constituting a confined environment and requiring to maintain a high discretion.
  • an object of the invention is to allow more precise and more reliable management of a liquefied gas tank, in particular within an underwater building.
  • the subject of the invention is a control method of the aforementioned type, in which the method also comprises the following steps:
  • the method according to the invention has one or more of the following characteristics, taken in isolation or in any technically feasible combination:
  • the parameter representative of the time course of the temperature of the liquid phase is a time derivative of the parameter representative of the temperature of the liquid phase
  • the first test being a comparison of the time derivative of the parameter representative of the temperature of the phase liquid with a predetermined threshold value, and the need for maintenance being signaled if the time derivative of the parameter representative of the temperature of the liquid phase is greater than the threshold value
  • the parameter representative of the time evolution of the temperature of the liquid phase is a time derivative of the temperature of the liquid phase
  • the second test comprises a calculation of a parameter representative of the continuity of the time derivative of the temperature of the liquid phase and the comparison of the parameter representative of the continuity with a predetermined threshold, the loss of thermal insulation being signaled if the parameter representative of the continuity is greater than the threshold;
  • the method further comprises the following steps:
  • cryogenic tank is located in an underwater building powered by a propulsion system including an energy production system.
  • the invention also relates to a cryogenic tank comprising:
  • a first pressure sensor arranged to measure a parameter representative of a pressure in the liquid phase
  • a second pressure sensor arranged to measure a parameter representative of a pressure of the gas phase
  • a temperature sensor arranged to measure a parameter representative of a temperature of the liquid phase
  • control module configured to control the first pressure sensor, the second pressure sensor and the temperature sensor, and to determine a total mass of the liquid phase from the temperature of the liquid phase, from the pressure in the liquid phase and gas phase pressure.
  • the invention further relates to an underwater anaerobic propulsion vessel, comprising a propulsion system comprising an energy production system and at least one cryogenic tank as defined above, the liquefied gas contained in the cryogenic tank being dioxygen and feeding the energy production system as oxidant.
  • FIG. 1 is a side view of an underwater building according to the invention.
  • FIG. 2 is a schematic sectional view of a cryogenic tank of the submarine of Figure 1;
  • Figures 3 and 4 are graphical representations of the time course of a temperature of the fluid contained in the reservoir of Figure 2.
  • FIG. 1 an underwater vessel 10 is shown plunged into a body of water 12, under a surface 14 of the body of water 12.
  • submarine is meant that the vessel is suitable and intended to make completely submerged journeys, in particular for a period greater than or equal to one day. Such a building is also able to return to the surface.
  • the underwater vessel 10 comprises a hull 16 delimiting an internal space which is sealed against the body of water 12, as well as a propulsion system 18 received in the internal space and at least one propeller driven 20 by the propulsion system 18, and suitable for setting in motion the underwater vessel.
  • the submarine building 10 is an anaerobic propelled submarine, that is to say that the propulsion system 18 does not require outside air for its operation.
  • the propulsion system 18 is a thermal-electric system, which comprises, in a known manner, an electric motor 22 driving the propeller 20, an alternator 24 and a turbine 26 supplying the electric motor 22.
  • the propulsion system 18 also comprises a steam generator 28, a condenser 30 and a heat exchanger 32 driving the turbine 26, as well as an energy production system 34, more particularly a combustion chamber, generating the heat supplying the heat exchanger 32.
  • the propulsion system 18 further comprises a fuel tank 36, for example containing ethanol, and a cryogenic tank 38, containing dioxygen.
  • the fuel tank 36 and the cryogenic tank 38 supply the energy production system 34, here the combustion chamber, with fuel and oxygen respectively, which plays the role of oxidizer therein, to participate in an exothermic combustion reaction.
  • the cryogenic tank 38 is shown in more detail in FIG. 2. It comprises a storage enclosure 40 comprising a thermally insulating wall 42, in particular a double wall, defining an internal space for storing liquid oxygen.
  • the oxygen contained in the cryogenic tank 38 forms a liquid phase 44 and a gas phase 46 in the enclosure 40, separated by an upper surface 47 from the liquid phase 44.
  • the cryogenic tank 38 is shown in FIG. 2 in relation to a direction of elevation Z-Z ′ oriented in the local direction of gravity.
  • the liquid phase 44 denser than the gas phase 46, occupies a lower part of the enclosure 40, and the gas phase 46 an upper part of the enclosure 40, relative to the direction of elevation Z-Z ’.
  • the cryogenic tank 38 also comprises a first conduit 50 opening into the lower part of the enclosure 40 and a second conduit 52 opening into the upper part of the enclosure 40.
  • the first conduit 50 is in particular an inlet conduit for liquid dioxygen in the enclosure 40
  • the second conduit 52 is in particular an outlet conduit from the enclosure 40.
  • the first conduit 50 and the second conduit 52 are respectively provided with a first valve 54 and with a second valve 56, suitable for controlling the entry and exit of fluid in the enclosure 40 through the first conduit 50 and the second conduit 52.
  • the first conduit 50 and the second conduit 52 advantageously comprise thermal insulation envelopes (not shown).
  • the first conduit 50 and the second conduit 52 comprise an internal portion extending between the enclosure 40 and the first valve 54 and the second valve 56 respectively, through the wall 42.
  • the internal portion of the first conduit 50 opens out through a lower face 58 of the enclosure 40, relative to the direction of elevation Z-Z ', in order to guarantee that the first conduit 50 opens out into the liquid phase 44 even for a low filling rate of the enclosure 40.
  • the cryogenic tank 38 further comprises a first pressure sensor 60, located in the lower part of the enclosure 40 and a second pressure sensor 62, located in the upper part of the enclosure 40.
  • the first and second pressure sensors 60, 62 are adapted to measure a hydrostatic pressure respectively in the liquid phase 44 and in the gas phase 46 of the oxygen contained in the enclosure 40.
  • the first and second pressure sensors 60, 62 are suitable for measuring a parameter representative of a hydrostatic pressure respectively at a point in the liquid phase 44 and at a point in the gas phase 46.
  • representative parameter it is meant that the sensor measures a physical quantity making it possible to obtain the pressure directly by a direct calculation.
  • the parameter representative of the pressure in the liquid phase 44 is the pressure in the liquid phase 44 itself and the parameter representative of the pressure of the gas phase 46 is the pressure of the gas phase 46 itself.
  • the cryogenic tank 40 also comprises a temperature sensor 64 located in the lower part of the enclosure 40, capable of measuring a temperature of the liquid phase 44.
  • the parameter representative of the temperature of the liquid phase 44 is the temperature of the liquid phase 44.
  • the temperature sensor 64 is able to measure a parameter representative of the temperature at a point in the liquid phase 44.
  • the parameter representative of the temperature is advantageously the temperature of the liquid phase 44 itself.
  • the temperature sensor 64 is for example a platinum resistance thermometer of the PT100 type.
  • the temperature sensor 64 is located in the internal portion of the first conduit 50, opposite the lower part of the enclosure 40, so that the temperature sensor 64 is able to measure the temperature of the liquid phase 44 itself for a low filling rate.
  • the first pressure sensor 60, the second pressure sensor 62, and the temperature sensor 64 are connected to a control module 66, configured to follow the respective temporal changes in the pressure of the liquid phase 44 at the level of the first sensor. pressure 60, the pressure of the gas phase 46 and the temperature of the liquid phase 44.
  • the control module 66 includes a processor suitable for executing computer programs and a memory suitable for storing data.
  • the control module 66 is also configured to implement a method for controlling the cryogenic tank 38 described below and to determine, as a function of the temperature and pressure measurements, a mass of the liquid phase 44 contained in the enclosure 40 , a possible need for maintenance of the cryogenic tank 38, a possible degradation of the thermal insulation of the enclosure 40 and a possible need to purge the cryogenic tank 38, as well as to predict a date for the need to purge the cryogenic tank 38.
  • the reservoir 38 also comprises a purge module 68 comprising a pump and fluidly connected to the first conduit 50 and to the second conduit 52 through purge valves 70.
  • the purge module 68 is capable of sucking up part of the gas phase 46, in particular through the second conduit 52, in order to reduce the pressure of the gas phase 46 in the enclosure 40, which causes a vaporization of part of the liquid phase 44.
  • the vaporization of part of the liquid phase 44 lowers the temperature in the enclosure 40, according to the enthalpy of vaporization of the oxygen.
  • the purging of the cryogenic tank 38 by the purging module 68 requires being able to evacuate the part of the aspirated gas phase 46, which can be a problem in a confined environment.
  • the cryogenic tank 38 comprises a differential pressure transmitter (not shown), in place of the first pressure sensor 60, located in the lower part of the enclosure 40 and the second pressure sensor 62 , located in the upper part of enclosure 40.
  • the differential pressure transmitter is for example arranged outside the cryogenic tank 38. This allows in particular that the differential pressure transmitter is not in contact with the liquid phase.
  • the cryogenic tank 38 contains liquid dioxygen forming a liquid phase 44 and a gas phase 46.
  • the method comprises a step of repeatedly measuring a pressure in the liquid phase 44 by the first pressure sensor 60, the pressure of the gas phase 46 by the second pressure sensor 62, and the temperature of the liquid phase 44 by the temperature sensor 64.
  • the pressure sensors 60, 62 and temperature 64 measure parameters representative respectively of the pressure in the liquid phase 44, of the pressure of the gas phase 46 and of the temperature of the liquid phase 44.
  • the parameters representative are respectively the pressure in the liquid phase 44, the pressure in the gas phase 46 and the temperature of the liquid phase 44 themselves.
  • the temperature and pressure measurements are controlled by the control module 66 and the results of the measurements recorded on the memory.
  • the method also includes a step of determining a mass m of the liquid phase 44, from temperature and pressure measurements.
  • a density p of the liquid dioxygen of the liquid phase 44 is evaluated from the temperature of the liquid phase 44, by the control module 66.
  • the filling height h corresponds to the height separating the first pressure sensor 60 and the upper surface 47 of the liquid phase 44.
  • the pressure in the gas phase 46 is considered to be substantially homogeneous, the gas phase 46 being much less dense than the liquid phase 44.
  • the mass m of the liquid phase 44 is then calculated as a function of the filling height h and the geometry of the enclosure 40.
  • the mass m the enclosure 40 is obtained by a direct calculation as a function of the geometry of the enclosure 40.
  • the mass m is obtained from a filling chart previously established and recorded in the memory.
  • the mass m of the liquid phase 44 is displayed, for example on a screen, in order to inform an operator.
  • the method further comprises a step of detecting a possible need for maintenance of the cryogenic tank 38.
  • a temporal change in the temperature of the liquid phase 44 is determined from the temperature measurements obtained through the temperature sensor 64, and a time derivative of the temperature is calculated repeatedly by the control module 66.
  • the time derivative of the temperature is compared with a predetermined threshold value, and the control module 66 determines that the reservoir 58 requires maintenance 66 if the time derivative of the temperature is greater than or equal to the threshold value.
  • the need for maintenance of the cryogenic tank 38 is then signaled to an operator, for example by displaying a message on a screen.
  • FIG. 3 is a graphic representation of the temperature T of the liquid phase as a function of time t.
  • the time derivative T of the temperature that is to say the local slope of the curve of the temperature T, increases over time t.
  • the time derivative T of the temperature T exceeds the threshold value T ' max, and the control module 66 signals a need for maintenance of the cryogenic tank 58.
  • the threshold value T'max of the time derivative of the temperature has an order of magnitude, for example, of 0.5 K / h, more particularly is equal to 0.5 K / h.
  • the increase in the time derivative T of the temperature T is observed on a time scale of the order of one or more years.
  • the detection of the need for maintenance by monitoring the temperature of the liquid phase 44 provides more precise information than the pre-existing methods, with which the maintenance was carried out at constant interval, without taking account of the specific aging of the cryogenic tank 38.
  • the method also includes a step of detecting any degradation of the thermal insulation of the enclosure 40.
  • the time derivative T of the temperature of the liquid phase 44 is calculated repeatedly as described above.
  • the loss of thermal insulation of the enclosure 40 is detected when the time derivative T of the temperature of the liquid phase 44 increases discontinuously.
  • the curve of the temperature T of the liquid phase 44 as a function of time t has a slope discontinuity, as represented in FIG. 4 at an instant t ⁇
  • the instant ⁇ corresponds to a detection by the module control 66 of the degradation of the insulation of the enclosure 40, which generally requires urgent intervention.
  • control module 66 calculates a parameter representative of the continuity of the time derivative of the temperature T of the liquid phase 44, and compares this parameter with a predetermined continuity threshold. The control module 66 detects the slope discontinuity when the parameter representative of the continuity is greater than the continuity threshold.
  • the parameter is for example a difference between two successive values of the time derivative of the temperature of the liquid phase 44.
  • the degradation of the insulation is then signaled to an operator, for example by displaying a message on a screen, and / or by means of an audible warning.
  • the detection of the loss of insulation from the temperature of the liquid phase 44 is faster than the detection from the monitoring of the pressure of the gas phase 46, according to the methods previously used. This makes it possible to react earlier to degradation of the insulation and reduces the risk of damage to the cryogenic tank 38.
  • the method further comprises a step of determining a need to purge the cryogenic tank 38, and predicting this need to purge.
  • the time course of the temperature of the liquid phase 44 as a function of time is determined as described above.
  • the need to purge the cryogenic tank is determined by the control module 66 when the temperature of the liquid phase 44 exceeds a predetermined purge threshold value.
  • the purge threshold value is for example equal to 1 10 K.
  • the need to purge the tank is signaled to an operator, for example by displaying a message on a screen.
  • control module 66 predicts a date on which the reservoir 38 must be purged, as a function of the temperature of the liquid phase 44, of the threshold value, and of the time derivative of the temperature of the liquid phase 44, calculated as above.
  • the next scheduled purge date is signaled to an operator, for example by displaying it on a screen.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
EP19801564.6A 2018-11-12 2019-11-12 Verfahren zur steuerung eines kryotanks, entsprechender kryotank und entsprechendes unterwasserbauwerk Pending EP3881002A1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1871500A FR3088406B1 (fr) 2018-11-12 2018-11-12 Procédé de contrôle d'un réservoir cryogénique, réservoir cryogénique et bâtiment sous-marin correspondants
PCT/EP2019/081034 WO2020099410A1 (fr) 2018-11-12 2019-11-12 Procédé de contrôle d'un réservoir cryogénique, réservoir cryogénique et bâtiment sous-marin correspondants

Publications (1)

Publication Number Publication Date
EP3881002A1 true EP3881002A1 (de) 2021-09-22

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EP19801564.6A Pending EP3881002A1 (de) 2018-11-12 2019-11-12 Verfahren zur steuerung eines kryotanks, entsprechender kryotank und entsprechendes unterwasserbauwerk

Country Status (5)

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EP (1) EP3881002A1 (de)
JP (1) JP7399961B2 (de)
KR (1) KR20210090246A (de)
FR (1) FR3088406B1 (de)
WO (1) WO2020099410A1 (de)

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JP2709676B2 (ja) * 1991-08-20 1998-02-04 大陽東洋酸素株式会社 低温液化ガスの水分低減方法
JP4574801B2 (ja) * 1999-08-27 2010-11-04 住友精化株式会社 液化ガスの混合装置
FR2811752B1 (fr) * 2000-07-13 2002-10-18 Profroid Procede et dispositif de mesure du volume d'un liquide
DE10305778A1 (de) * 2003-02-12 2004-08-26 Howaldtswerke-Deutsche Werft Ag Unterseeboot
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JP7399961B2 (ja) 2023-12-18
KR20210090246A (ko) 2021-07-19
WO2020099410A1 (fr) 2020-05-22
FR3088406B1 (fr) 2021-05-07
JP2022507067A (ja) 2022-01-18
FR3088406A1 (fr) 2020-05-15

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