Gas leak detection device and gas leak detection method

Abstract

To provide a gas leak detection device and a gas leak detection method that can easily detect a liquefied gas leak in a detection target space, identify the leak location, and are maintenance-free.SOLUTION: A gas leak detection device includes a plurality of thermal imaging cameras 1a, 1b arranged apart from each other and directed toward a detection target space in a ship in which detection targets 101, 102 storing liquefied gas are arranged, and a control device 2 that acquires images captured by the thermal imaging cameras 1a, 1b as thermal images. The control device 2 determines that liquefied gas is leaking when a ratio (α) of an area (At) of the area of the thermal image taken by at least one of the thermal imaging cameras 1a and 1b whose temperature is equal to or lower than the threshold temperature (Tr) to an area (A0) of the thermal image taken by the thermal imaging camera 1a or 1b is equal to or higher than a threshold ratio (αr), and the control device 2 records only the value of the ratio (α).SELECTED DRAWING: Figure 1

Description

Technical Field

[0001] The present invention relates to a gas leak detection device and a gas leak detection method, and more particularly, to a gas leak detection device and a gas leak detection method that can easily detect the leakage of liquefied gas in a detection target space, identify the leakage location, and are maintenance-free.

Background Art

[0002] Liquefied gases such as liquefied ammonia and LPG (liquefied petroleum gas) are used as fuels in addition to cargo on ships, and the demand is increasing.

[0003] When liquefied gas leaks due to damage or deterioration of tanks for storing liquefied gas, pipes for feeding liquefied gas, etc. inside a ship, it is necessary to detect the leakage in order to ensure the safety of crew members.

[0004] Conventionally, as methods for detecting the leakage of liquefied gas, there are a method using a semiconductor-type solid sensor and a method using a potentiostatic ionization-type electrochemical sensor.

[0005] Patent Document 1 describes a hydrogen leak detection device that detects the temperature rise of a hydrogen storage part made of a hydrogen storage alloy by a temperature sensor and determines the presence or absence of hydrogen leakage.

Prior Art Documents

Patent Documents

[0006]

Patent Document 1

Summary of the Invention

Problems to be Solved by the Invention

[0007] By the way, for the above-mentioned solid sensors and electrochemical sensors, it is necessary to select a sensor of a type suitable for the composition (type) of the liquefied gas for which leakage is to be detected. Therefore, in a ship that transports or uses liquefied gases of multiple compositions (types), sensors of multiple types must be used, and the number of sensors required increases.

[0008] In addition, these solid sensors and electrochemical sensors require a great deal of labor because they need to be periodically replaced and calibrated. Such labor-intensive maintenance can be promptly addressed on regular ships, but cannot be promptly addressed on tramp ships.

[0009] Also, since the leaked liquefied gas vaporizes and diffuses into the space, depending on the fixed gas detection sensor, if the leakage location is far from the sensor installation location, it takes a long time for the vaporized gas to reach the sensor before detection.

[0010] Furthermore, depending on fixed gas detection sensors or fixed temperature sensors such as those described in Patent Document 1, since the detectable area is limited, when the detection target space is large or there are many target devices, a large number of sensors must be installed, and the labor and cost of installation become extremely high. In this case, a method of intensifying and detecting the vaporized gas using a ventilation fan can be considered, but a large number of devices are required for the configuration, and the labor and cost of installation also become extremely high.

[0011] With fixed gas detection sensors or temperature sensors, it is complicated to identify the leakage location because an airtightness test or the like must be performed. Also, for the case of leakage from the liquid supply pipe, a method of installing a drip tray and a temperature sensor in this drip tray can be considered, but the temperature change cannot be grasped until the leaked material is concentrated in the drip tray, and if the leaked material is not concentrated, the leakage of the liquefied gas cannot be detected.

[0012] Incidentally, although it is conceivable to use a thermal imaging camera to detect a location that has been cooled due to a leakage of liquefied gas, the shapes of tanks, pipes, etc. on a ship are complex, and they may be installed not only in the ship's interior but also in open spaces such as on the deck. Therefore, it has been difficult to arrange the thermal imaging camera so that there are no blind spots, i.e., so that all surfaces of the tanks, pipes, etc. can be imaged.

[0013] Therefore, an object of the present invention is to provide a gas leak detection device and a gas leak detection method that can easily detect a leakage of liquefied gas in a detection target space without any undetected locations, can identify the leakage location, and are maintenance-free.

[0014] Furthermore, other objects of the present invention will become apparent from the following description.

Means for Solving the Problems

[0015] The above problems are solved by the following inventions. 1. In a ship, a plurality of thermal imaging cameras arranged apart from each other and directed toward a detection target space in which a detection target object storing liquefied gas is arranged, and a control device that acquires an image captured by the thermal imaging camera as a thermal image are provided. When, in a thermal image captured by at least one of the thermal imaging cameras, the ratio (α) of the area (At) of a region having a temperature equal to or lower than a threshold temperature (Tr) to the area (A0) of the thermal image captured by that one thermal imaging camera is equal to or higher than a threshold ratio (αr), the control device determines that the liquefied gas is leaking. The control device records only the numerical value of the ratio (α). A gas leak detection device characterized by the above. 2. The threshold temperature (Tr) is set to an arbitrary temperature between the saturation temperature of the liquefied gas under atmospheric pressure and the air temperature. The gas leak detection device according to the above 1, characterized by the above. 3. Each of the thermal imaging cameras is arranged in two lines, one on each of two straight lines where the central angle around the center of the circumscribed sphere of the object to be detected is 30° to 180°, for a total of two cameras. The gas leak detection device according to claim 1 or 2, characterized in that. 4. Each of the thermal imaging cameras is arranged in three lines, one on each of three straight lines where the central angle around the center of the circumscribed sphere of the object to be detected is 120°, for a total of three cameras. The gas leak detection device according to claim 1 or 2, characterized in that. 5. Each of the thermal imaging cameras is arranged in four lines, one on each of four straight lines where the central angle around the center of the circumscribed sphere of the object to be detected is 90° to 110°, for a total of four cameras. The gas leak detection device according to claim 1 or 2, characterized in that. 6. Each of the thermal imaging cameras is arranged in five positions, one on the front side, rear side, left side, right side, and upper side of the detection target space, for a total of five cameras. The gas leak detection device according to claim 1 or 2, characterized in that. 7. Each of the thermal imaging cameras is arranged in six positions, two facing each other on each axis of the xyz orthogonal coordinates with the center of the circumscribed sphere of the object to be detected as the origin, for a total of six cameras. The xyz orthogonal coordinates are rotated with respect to the detection target space, and the arrangement of the thermal imaging cameras on the floor surface of the detection target space is avoided. The gas leak detection device according to claim 1 or 2, characterized in that. 8. In a ship, a plurality of thermal imaging cameras directed at a detection target space in which an object to be detected for storing liquefied gas is arranged are arranged separately from each other. The detection target space is photographed by the thermal imaging cameras. An image photographed by the thermal imaging cameras is acquired as a thermal image. In the thermal image obtained by at least one of the thermal imaging cameras, when the ratio (α) of the area (At) of the region having a temperature equal to or lower than the threshold temperature (Tr) to the area (A0) of the thermal image obtained by the one thermal imaging camera is equal to or higher than the threshold ratio (αr), it is determined that the liquefied gas is leaking. Record only the numerical value of the ratio (α). A gas leak detection method characterized by this. 9. The threshold temperature (Tr) is set to any temperature between the saturation temperature of the liquefied gas under atmospheric pressure and the atmospheric temperature. The gas leak detection method according to item 8 above, characterized by this. 10. Two of the plurality of thermal imaging cameras are arranged one by one on two straight lines with a central angle around the center of the circumscribed sphere of the object to be detected being 30° to 180°. The gas leak detection method according to item 8 or 9 above, characterized by this. 11. Three of the plurality of thermal imaging cameras are arranged one by one on three straight lines with a central angle around the center of the circumscribed sphere of the object to be detected being 120°. The gas leak detection method according to item 8 or 9 above, characterized by this. 12. Four of the plurality of thermal imaging cameras are arranged one by one on four straight lines with a central angle around the center of the circumscribed sphere of the object to be detected being 90° to 110°. The gas leak detection method according to item 8 or 9 above, characterized by this. 13. Five of the plurality of thermal imaging cameras are arranged one by one on the front side, rear side, left side, right side, and upper side of the detection target space. The gas leak detection method according to item 8 or 9 above, characterized by this. 14. Six of the plurality of thermal imaging cameras are arranged in pairs facing each other on each axis of the xyz orthogonal coordinates with the center of the circumscribed sphere of the object to be detected as the origin. The gas leak detection method according to item 8 or 9 above, characterized by this.

Advantages of the Invention

[0016] According to the present invention, it is possible to provide a gas leak detection device and a gas leak detection method that can easily detect the leakage of liquefied gas in the detection target space without any undetected locations, can identify the leakage location, and are maintenance-free.

Brief Description of the Drawings

[0017]

Figure 1

Figure 2

Figure 3

Figure 4

Figure 5

Figure 6

Figure 7

Figure 8

Modes for Carrying Out the Invention

[0018] 〔First Embodiment〕 Hereinafter, preferred embodiments of the present invention will be described. FIG. 1 is a block diagram showing the configuration of the gas leak detection device according to the first embodiment.

[0019] As shown in FIG. 1, the gas leak detection device of the present embodiment is configured to include a plurality of thermal imaging cameras 1a and 1b. The plurality of thermal imaging cameras 1a and 1b are arranged in a ship toward a detection target space 103 where detection targets 101 and 102 for storing liquefied gas are arranged. Each of the thermal imaging cameras 1a and 1b is arranged separately from each other.

[0020] The objects to be detected 101 and 102 that store liquefied gas are, for example, a tank 101 that stores liquefied gas and / or a pipe 102 that delivers liquefied gas. However, it is not limited to only the tank 101 and the pipe 102, and various articles that store liquefied gas may be included in the objects to be detected. The "tank that stores liquefied gas" includes various tanks such as "fuel tank" and "buffer tank", and includes those that are not pressurized, those that are pressurized, those that are not cryogenic, and those that are cryogenic. The liquefied gas stored in the objects to be detected 101 and 102 is not particularly limited, and is, for example, liquefied ammonia, liquefied petroleum gas (LPG: Liquefied Petroleum Gas), or the like. Note that in the tank 101 and the pipe 102 that store liquefied gas, there may be a gas phase portion and a liquid phase portion. That is, the liquefied gas stored as a liquid is vaporized into a gas in the space above the liquid level in the tank 101 and the pipe 102. In addition, "gas leakage" includes any of the release of gaseous gas from the gas phase portion to the atmosphere, the release of liquefied gas from the liquid phase portion to the atmosphere, and the release of a gas-liquid mixed fluid in which a part is vaporized gas from the gas phase portion and the liquid phase portion to the atmosphere.

[0021] The detection target space 103 is, for example, a fuel adjustment room, but is not limited to this, and it does not matter whether it is in a ship's cabin or on deck. In addition, the detection target space 103 is not limited to a space closed by a ceiling, a wall surface, and a floor surface, and may be an open space conceptually regarded as a certain area.

[0022] The thermal imaging cameras 1a and 1b are, for example, infrared thermal imaging cameras, and for example, "Chino Thermal Imaging Camera" CPA-T1000 / CPA-T800 / CPA-T500 manufactured by Chino Corporation can be used. The infrared thermal imaging camera can capture a thermal image in which color separation is performed according to the surface temperature of an object to be detected (solid) such as the tank 101 and the pipe 102.

[0023] This gas leak detection device includes a control device 2. The control device 2 receives image signals captured by the thermal imaging cameras 1a and 1b and acquires the images captured by the thermal imaging cameras 1a and 1b as thermal images. The control device 2 displays the acquired thermal images on a display device (not shown).

[0024] When liquefied gas leaks into the atmosphere due to defects such as corrosion of the detection objects 101, 102 or loose joints, the surfaces of the detection objects 101, 102 that come into contact with the low-temperature leaked liquefied gas absorb heat and are cooled to below the air temperature, and when the leaked liquefied gas vaporizes, the surfaces of the detection objects 101, 102 absorb the heat of vaporization and are cooled to below the air temperature. The areas that have been cooled by the leakage of liquefied gas can be identified early and easily in the thermal images captured by the thermal imaging cameras 1a, 1b.

[0025] Figure 2 is a schematic diagram showing examples of thermal images captured by a thermal imaging camera. (a) is an image of a normal state with no leakage, (b) is an image of a state with leakage from a welded joint of the tank, and (c) is an image of a state with leakage from a flange surface.

[0026] The area cooled by the leakage of liquefied gas is detected by thermal imaging cameras 1a and 1b, as shown in Fig. 2. In Fig. 2, a tank 101 and a pipe 102 are shown as objects to be detected. Fig. 2(a) is an image of the tank 101 and the pipe 102 in a normal state without leakage. The tank 101 is placed on a drip tray 107, and the pipe 102 is connected at a welded portion 104. The pipe 102 is also connected to another pipe 102 by a flange 105. The periphery of the flange 105 is covered with a heat insulating material 106.

[0027] As shown in FIG. 2(b), if the liquefied gas in the tank 101 leaks from the welded portion 104, the leaked liquefied gas 108 will be exposed to atmospheric pressure and its temperature will drop, causing the surroundings of the leaked portion and the surroundings of the leaked liquefied gas 109 dripping onto the drip tray 107 to become colder, which will be detected in the thermal images captured by the thermal imaging cameras 1a and 1b.

[0028] Also, as shown in Fig. 2(c), when the liquefied gas in the tank 101 leaks from the mating surface of the flange 105, the leaked liquefied gas 109 drips onto the drip tray 107 from the gap of the heat insulating material 106, the surrounding area becomes low temperature, and it is detected in the thermal image captured by the thermal imaging cameras 1a and 1b.

[0029] In addition, in either case of Fig. 2(b) and (c), depending on the type of the liquefied gas in the tank 101, if a dedicated lens is used, the vaporized gas can also be detected, and it is also possible to widen the detection area.

[0030] Also, by providing a zoom function for enlarging the display of the leakage location, the accuracy of calculating the area of the leakage location can be improved. Further, by recording the thermal image together with the imaging time information, even at a time after the leakage time, the leakage location and the leakage time can be specified.

[0031] The thermal imaging cameras 1a and 1b do not need maintenance such as replacement or replenishment of sensors or chemicals as long as there are no malfunctions such as failures, and are so-called maintenance-free.

[0032] The detection of the leakage location (cooling location) of the liquefied gas by the thermal imaging cameras 1a and 1b is performed by setting an arbitrary temperature between the saturation temperature of the target liquefied gas under atmospheric pressure and the air temperature as the threshold temperature (leakage detection temperature) Tr, and specifying the location where the measured temperature Te is equal to or lower than the threshold temperature (leakage detection temperature) Tr as the cooling location. Note that the cooling of the surfaces of the detection objects 101 and 102 due to the leakage of the liquefied gas may be lower than the saturation temperature of the target liquefied gas under atmospheric pressure.

[0033] If the minimum temperature in winter is, for example, -20°C, and the target liquefied gas is liquefied ammonia, since the saturation temperature under atmospheric pressure is -33°C, the threshold temperature Tr can be set to -33°C to -21°C. If the target liquefied gas is liquefied petroleum gas, since the saturation temperature under atmospheric pressure is -42°C, the threshold temperature Tr can be set to -42°C to -21°C.

[0034] As in this embodiment, when there are two thermal imaging cameras 1a and 1b arranged separately from each other, these thermal imaging cameras 1a and 1b are arranged one by one on two straight lines where the central angle Ac around the center C of the circumscribed sphere S of the detection objects 101 and 102 is from approximately 30° to approximately 180°. If the central angle Ac is 30° or more, it can be said that the thermal imaging cameras 1a and 1b are separated from each other.

[0035] Regarding the positional relationship between the thermal imaging cameras, it is preferable to use the circumscribed sphere of the detection object as a reference. Since all detection objects are inside the circumscribed sphere and there are no detection objects outside the circumscribed sphere, it is necessary to photograph inside the circumscribed sphere and there is no need to photograph outside the circumscribed sphere.

[0036] By using the circumscribed sphere determined by the detection object as a reference, in a detection target space such as a fuel adjustment chamber, when detection objects such as tanks and pipes are unevenly installed, that is, when there are detection objects only in one corner of the fuel adjustment chamber, each thermal imaging camera can be arranged at an appropriate position according to the shape and position of the detection object to be photographed, regardless of the shape of the fuel adjustment chamber and the position of the wall surface. However, each thermal imaging camera does not necessarily have to be arranged outside the circumscribed sphere. As long as there are no blind spots, that is, no unimageable areas, on the surface of the detection object, it may be arranged on the spherical surface of the circumscribed sphere or inside the circumscribed sphere.

[0037] Also, when the detection target space where the detection object is installed is an open space such as on the deck rather than in a ship's cabin, by using the circumscribed sphere determined by the detection object as a reference, each thermal imaging camera can be arranged at an appropriate position according to the shape and position of the detection object to be photographed.

[0038] Note that the plane including the center C of the circumscribed sphere S and the two straight lines on which the thermal imaging cameras 1a and 1b are arranged is not limited to the horizontal plane, and may be an inclined plane or a vertical plane. Also, the distances between the center C of the circumscribed sphere S and the respective thermal imaging cameras do not have to be equal to each other, and may be different distances for each thermal imaging camera. These also apply to other embodiments described later in which three or more thermal imaging cameras are used.

[0039] The thermal imaging cameras 1a and 1b are arranged so that there are no imaging - impossible locations, i.e., no blind spots, on the surfaces of the detection objects 101 and 102. To ensure no blind spots, it is preferable to arrange one thermal imaging camera 1a and 1b on each of two straight lines with a central angle of approximately 180° around the center of the circumscribed sphere S of the detection object. Depending on the shape and arrangement of the detection objects 101 and 102, if blind spots occur with the two thermal imaging cameras 1a and 1b, it may be possible to arrange three or more thermal imaging cameras as in other embodiments described later.

[0040] FIG. 3 is a flowchart showing the procedure of the gas leak detection method according to the embodiment.

[0041] The control device 2 also has a function of analyzing the thermal images taken by the thermal imaging cameras 1a and 1b. That is, as shown in FIG. 3, the control device 2 executes the gas leak detection method of the embodiment. This gas leak detection method is also executed in the gas leak detection device of other embodiments described later.

[0042] The control device 2, which also functions as an image analysis device, sets the threshold temperature Tr (°C), the threshold ratio αr, and the detection interval t (sec) in step st1 and proceeds to step st2.

[0043] In step st2, the control device 2 measures the temperature Te (°C) in the thermal images (detection ranges) captured by the thermal imaging cameras 1a and 1b, calculates the area At of the region where the temperature Te (°C) is equal to or lower than the threshold temperature Tr (°C), and proceeds to step st3.

[0044] In step st3, the control device 2 determines whether the ratio α (= At / A0) of the area At to the area A0 of the thermal image is equal to or higher than the threshold ratio αr. If the ratio α is less than the threshold ratio αr, it proceeds to step st4. If the ratio α is equal to or higher than the threshold ratio αr, it proceeds to step st5. Note that the threshold ratio αr is preferably set as low as possible, for example, preferably about 1%.

[0045] Note that the area A0 of the thermal image may be the area of the thermal image by one thermal imaging camera, or may be the sum of the areas of a plurality of thermal images by a plurality of thermal imaging cameras. When the area A0 of the thermal image is the area of the thermal image by one thermal imaging camera, when the ratio α is equal to or higher than the threshold ratio αr in the thermal image by at least any one of the thermal imaging cameras, it proceeds to step st5.

[0046] When the area A0 of the thermal image is the whole of a plurality of thermal images by a plurality of thermal imaging cameras, when the ratio α is equal to or higher than the threshold ratio αr in the whole of the plurality of thermal images, it proceeds to step st5. In this case, the threshold ratio is determined as αr / n (∵n: the number of thermal imaging cameras). In this case, even if one region where the temperature is equal to or lower than the threshold temperature Tr (°C) is imaged in parts in a plurality of thermal images and the area of the part is small in one thermal image, the areas of these parts are totaled and correctly determined.

[0047] In step st4, the control device 2 determines that there is no leakage of liquefied gas and returns to step st2.

[0048] In step st5, the control device 2 determines that there is a leakage of liquefied gas, issues an alarm signal, records the thermal image, and proceeds to step st6.

[0049] In step st6, the control device 2 notifies the ship's interior that there is a leakage of liquefied gas based on the leakage signal. This notification is made by sounding a warning sound using a siren or the like, playing a pre-recorded warning message, emitting warning light using a red lamp or the like.

[0050] After measures are taken against the leakage of liquefied gas, the control device 2 starts again from step st1. Alternatively, when it is not necessary to reset the threshold temperature Tr (°C), the threshold ratio αr, and the detection interval t (sec), it may start from step st2.

[0051] In the gas leakage detection method of the present invention, by determining the presence or absence of gas leakage based on the ratio α (= At / A0) of the area At (the area of the region where the temperature Te (°C) is equal to or lower than the threshold temperature Tr (°C)) of the thermal image to the area A0 of the thermal image, the following effects are obtained. That is, instead of determining only based on the temperature of a fixed single point, stable determination can be performed by quantifying the region (area) where the temperature is equal to or lower than the threshold temperature Tr (°C). Also, if all the image data is recorded, the accumulated data volume will become extremely large. However, in the gas leakage detection device of the present invention, only the numerical value of the ratio α needs to be recorded, so the accumulated data volume can be reduced. Furthermore, if the threshold ratio αr is set, the determination can be fully automated.

[0052] As a method that does not use the ratio α, a method of comparing the pixels of a certain acquired image with the pixels of the next acquired image (after the detection interval t (sec)) can be considered. However, it is difficult to detect a temperature that changes continuously and gradually according to gas leakage. In the gas leakage detection method of the present invention, even when the temperature changes continuously and gradually, since the area ratio α changes, gas leakage can be surely detected. In addition, depending on the external environment, there may be an air current with a stronger wind force than the leakage gas. In this case, since the flow of the leakage gas changes, it is difficult to detect by comparing pixels. In the gas leakage detection method of the present invention, even when the flow of the leakage gas changes, the ratio α of the area changes, so that gas leakage can be surely detected.

[0053] 〔Second Embodiment〕 FIG. 4 is a block diagram showing the configuration of a gas leakage detection device according to the second embodiment.

[0054] In this embodiment, as shown in FIG. 4, a plurality of thermal imaging cameras 1a, 1b, 1c are arranged one by one on three straight lines with a central angle Ac of approximately 120° around the center C of the circumscribed sphere S of the detection objects 101, 102, for a total of three cameras.

[0055] By using three thermal imaging cameras 1a, 1b, 1c, it is possible to prevent dead angles from occurring on the surfaces of the detection objects 101, 102 compared to the case of using two cameras.

[0056] Note that the central angle Ac around the center C of the circumscribed sphere S can be appropriately set according to the shapes and arrangements of the detection objects 101, 102. Also, the heights of the arrangement positions of the thermal imaging cameras 1a, 1b, 1c can be appropriately set according to the shapes and arrangements of the detection objects 101, 102.

[0057] Also in this embodiment, the plane including the center C of the circumscribed sphere S and the two straight lines on which any two of the thermal imaging cameras 1a, 1b (1a, 1c) (1b, 1c) are arranged is not limited to the horizontal plane, and may be an inclined plane or a vertical plane. Further, the thermal imaging cameras 1a, 1b, 1c do not necessarily need to be arranged on one plane including the center C of the circumscribed sphere S, and two cameras may be arranged on three planes including the center C of the circumscribed sphere S.

[0058] Also in this embodiment, the gas leakage detection method described in the first embodiment is executed by the control device 2.

[0059] 〔Third Embodiment〕 FIG. 5 is a block diagram showing the configuration of a gas leak detection device according to the third embodiment.

[0060] In this embodiment, as shown in FIG. 5, a plurality of thermal imaging cameras 1a, 1b, 1c, 1d are arranged one by one on four straight lines where the central angle Ac around the center C of the circumscribed sphere S of the detection objects 101, 102 is approximately 90° to approximately 110°, for a total of four cameras.

[0061] By using four thermal imaging cameras 1a, 1b, 1c, 1d, it is possible to prevent dead angles from occurring on the surfaces of the detection objects 101, 102 compared to the case of using three cameras.

[0062] Note that the central angle Ac around the center C of the circumscribed sphere S can be appropriately set according to the shapes and arrangements of the detection objects 101, 102. Also, the heights of the arrangement positions of the thermal imaging cameras 1a, 1b, 1c, 1d can be appropriately set according to the shapes and arrangements of the detection objects 101, 102.

[0063] Also in this embodiment, the plane including the center C of the circumscribed sphere S and the two straight lines on which any two thermal imaging cameras are arranged is not limited to the horizontal plane, and may be an inclined plane or a vertical plane. Further, the thermal imaging cameras 1a, 1b, 1c, 1d do not necessarily need to be arranged on one plane including the center C of the circumscribed sphere S, and two cameras may be arranged on each of the four planes including the center C of the circumscribed sphere S.

[0064] FIG. 6 is a block diagram showing another example of the configuration of a gas leak detection device according to the third embodiment. When the central angle Ac between any two thermal imaging cameras is all set to approximately 110° and two cameras are arranged on each of the four planes including the center C of the circumscribed sphere S, as shown in FIG. 6, the four thermal imaging cameras 1a, 1b, 1c, 1d are arranged at the vertex positions of a regular tetrahedron centered on the center C of the circumscribed sphere S. In this case, the central angle Ac is 2tan -1 √2 ≈ 109.47°.

[0065] Also in this embodiment, the gas leak detection method described in the first embodiment is executed by the control device 2.

[0066] 〔Fourth Embodiment〕 FIG. 7 is a block diagram showing the configuration of the gas leak detection device according to the fourth embodiment.

[0067] In this embodiment, as shown in FIG. 7, a total of five thermal imaging cameras 1a, 1b, 1c, 1d, and 1e are arranged, one each on the front side, rear side, left side, right side, and upper side of the detection target space 103.

[0068] By using the five thermal imaging cameras 1a, 1b, 1c, 1d, and 1e, it is possible to prevent dead spots from occurring on the surfaces of the detection targets 101 and 102, compared to the case of using four cameras.

[0069] In this embodiment, the thermal imaging camera 1e arranged on the upper side (ceiling) can image the entire horizontal plane direction of the detection target space 103. Also, by not arranging a thermal imaging camera on the lower side (floor surface), it does not interfere with the arrangement of the detection targets 101 and 102 in the detection target space 103 and walking.

[0070] Note that the arrangement positions (directions and heights) of the thermal imaging cameras 1a, 1b, 1c, 1d, and 1e can be appropriately set individually for each of the thermal imaging cameras 1a, 1b, 1c, 1d, and 1e according to the shape and arrangement of the detection targets in the detection target space 103.

[0071] Also in this embodiment, the gas leak detection method described in the first embodiment is executed by the control device 2.

[0072] 〔Fifth Embodiment〕 FIG. 8 is a block diagram showing the configuration of the gas leak detection device according to the fifth embodiment.

[0073] In this embodiment, as shown in FIG. 8, two thermal imaging cameras 1a, 1b, 1c, 1d, 1e, and 1f are arranged in pairs facing each other on each axis of the xyz orthogonal coordinates with the center C of the object to be detected in the detection target space 103 as the origin, for a total of six cameras. The xyz orthogonal coordinates are rotated with respect to the detection target space 103, and the arrangement of the thermal imaging cameras on the floor surface of the detection target space 103 is avoided.

[0074] By using six thermal imaging cameras 1a, 1b, 1c, 1d, 1e, and 1f, it is possible to prevent dead angles from occurring on the surfaces of the objects to be detected 101 and 102, compared to the case of using five cameras.

[0075] In this embodiment, since the thermal imaging cameras 1a, 1b, 1c, 1d, 1e, and 1f can be arranged at point-symmetrical positions in all directions around the center C of the circumscribed sphere S of the object to be detected, it is possible to correspond to various shapes and various arrangements of the objects to be detected in the detection target space 103. Also, by not arranging the thermal imaging cameras on the lower side (floor surface), the arrangement of the objects to be detected 101 and 102 in the detection target space 103 and walking are not obstructed.

[0076] In this embodiment, the central angle Ac between any two thermal imaging cameras is all 90°, and the six thermal imaging cameras 1a, 1b, 1c, 1d, 1e, and 1f are arranged at the positions of the vertices of a regular octahedron centered on the center C of the circumscribed sphere S.

[0077] Note that the arrangement positions (directions and heights) of the thermal imaging cameras 1a, 1b, 1c, 1d, 1e, and 1f can be appropriately set individually for each of the thermal imaging cameras 1a, 1b, 1c, 1d, 1e, and 1f according to the shape and arrangement of the objects to be detected in the detection target space 103.

[0078] Also in this embodiment, the gas leak detection method described in the first embodiment is executed by the control device 2.

Description of Reference Numerals

[0079] 1a Thermal imaging camera 1b Thermal imaging camera 1c Thermal imaging camera 1d Thermal imaging camera 1e Thermal imaging camera 1f Thermal imaging camera 2 Control device 101 Tank (object to be detected) 102 Pipe (object to be detected) 103 Detection target space 104 Weld point 105 Flange 106 Heat insulation material 107 Drip tray 108 Leaked liquefied gas 109 Leaked liquefied gas S Circumscribed sphere of the object to be detected C Center of the circumscribed sphere Ac Central angle

Claims

1. In a ship, a plurality of thermal imaging cameras arranged apart from each other and directed toward a detection target space in which a detection target object for storing liquefied gas is arranged, and a control device that acquires an image captured by the thermal imaging camera as a thermal image are provided, and when, in a thermal image captured by at least one of the thermal imaging cameras, a ratio (α) of an area (At) of a region having a temperature equal to or lower than a threshold temperature (Tr) to an area (A0) of the thermal image captured by the one thermal imaging camera is equal to or higher than a threshold ratio (αr), the control device determines that the liquefied gas is leaking, and the control device records only a numerical value of the ratio (α) A gas leak detection device characterized by the above.

2. The threshold temperature (Tr) is set to an arbitrary temperature between the saturation temperature of the liquefied gas under atmospheric pressure and the air temperature. The gas leak detection device according to claim 1, characterized by the above.

3. Two of the thermal imaging cameras are arranged one by one on two straight lines around the center of the circumscribed sphere of the detection target object, with a central angle of 30° to 180°. The gas leak detection device according to claim 1 or 2, characterized by the above.

4. Three of the thermal imaging cameras are arranged one by one on three straight lines around the center of the circumscribed sphere of the detection target object, with a central angle of 120°. The gas leak detection device according to claim 1 or 2, characterized by the above.

5. Four of the thermal imaging cameras are arranged one by one on four straight lines around the center of the circumscribed sphere of the detection target object, with a central angle of 90° to 110°. The gas leak detection device according to claim 1 or 2, characterized by the above.

6. Five of the thermal imaging cameras are arranged one by one on the front side, rear side, left side, right side, and upper side of the detection target space. The gas leak detection device according to claim 1 or 2, characterized by the above.

7. Six of the thermal imaging cameras are arranged in pairs facing each other on each axis of an xyz orthogonal coordinate system having the center of the circumscribed sphere of the detection target object as the origin, the xyz orthogonal coordinate system is rotated with respect to the detection target space, and the arrangement of the thermal imaging cameras on the floor surface of the detection target space is avoided. The gas leak detection device according to claim 1 or 2, characterized by the above.

8. In a ship, a plurality of thermal imaging cameras directed toward a detection target space in which a detection target object for storing liquefied gas is arranged are arranged apart from each other, and the detection target space is photographed by the thermal imaging cameras. Obtain the image captured by the thermal imaging camera as a thermal image, In the thermal image obtained by at least one of the thermal imaging cameras, when the ratio (α) of the area (At) of the region with a temperature below the threshold temperature (Tr) to the area (A0) of the thermal image obtained by the one thermal imaging camera is equal to or greater than the threshold ratio (αr), it is determined that the liquefied gas is leaking, Record only the numerical value of the ratio (α) A gas leakage detection method characterized by the above.

9. The threshold temperature (Tr) is set to an arbitrary temperature between the saturation temperature of the liquefied gas under atmospheric pressure and the air temperature. The gas leakage detection method according to claim 8, characterized by the above.

10. The plurality of thermal imaging cameras are arranged one by one on two straight lines with a central angle around the center of the circumscribed sphere of the object to be detected being 30° to 180°, for a total of two cameras. The gas leakage detection method according to claim 8 or 9, characterized by the above.

11. The plurality of thermal imaging cameras are arranged one by one on three straight lines with a central angle around the center of the circumscribed sphere of the object to be detected being 120°, for a total of three cameras. The gas leakage detection method according to claim 8 or 9, characterized by the above.

12. The plurality of thermal imaging cameras are arranged one by one on four straight lines with a central angle around the center of the circumscribed sphere of the object to be detected being 90° to 110°, for a total of four cameras. The gas leakage detection method according to claim 8 or 9, characterized by the above.

13. The plurality of thermal imaging cameras are arranged one by one on the front side, rear side, left side, right side and upper side of the detection target space, for a total of five cameras. The gas leakage detection method according to claim 8 or 9, characterized by the above.

14. The plurality of thermal imaging cameras are arranged two by two facing each other on each axis of the xyz orthogonal coordinates with the center of the circumscribed sphere of the object to be detected as the origin, for a total of six cameras. The gas leakage detection method according to claim 8 or 9, characterized by the above.

Images