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|[ Original Paper ]|
|Journal of Advanced Marine Engineering and Technology - Vol. 46, No. 5, pp. 212-217|
|ISSN: 2234-7925 (Print) 2765-4796 (Online)|
|Print publication date 31 Oct 2022|
|Received 18 Oct 2022 Revised 24 Oct 2022 Accepted 24 Oct 2022|
|Technical guide for materials of containment system for hydrogen fuels for ships|
Kang Woo Chun†
|Correspondence to : †Principal Research Engineer, Korean Register of Shipping, 36, Myeongji ocean city 9-ro, Gangseo-gu, Busan, 46762 Korea, E-mail: firstname.lastname@example.org, Tel: +82-70-8799-8745|
Copyright ⓒ The Korean Society of Marine Engineering
This is an Open Access article distributed under the terms of the Creative Commons Attribution Non-Commercial License (http://creativecommons.org/licenses/by-nc/3.0), which permits unrestricted non-commercial use, distribution, and reproduction in any medium, provided the original work is properly cited.
The International Maritime Organization (IMO) is adopting various regulations, goals, and measures for decarbonizing ships within the present century. The most environmentally friendly fuels for replacing conventional fuels in ships are low-flashpoint fuels, which are corrosive or cause embrittlement. Therefore, it is necessary to identify the requirements for storing individual fuels and choose the most realistic and economically feasible methods. Among the many alternative fuels, sufficient information is available regarding materials applicable to methanol—liquefied petroleum gas (LPG) and liquefied natural gas (LNG). Considering these fuels have long been handled by ships as fuel or cargo, sufficient regulations exist regarding the materials applicable to them. In the absence of conditions that lower the mechanical performance of materials, such as a hydrogen exposure environment or corrosion, materials applicable to cryogenic environments are generally applicable to higher temperatures without a problem. Liquid hydrogen is the fuel that presents the most difficult technical challenge for large-scale storage in ships. Hydrogen should be liquefied and stored in a containment facility designed to maintain a temperature below 20 K. Empirical studies on liquid hydrogen storage and fuel propulsion ships conducted in advanced countries have focused on 316 L stainless steel.
|Keywords: Alternative Fuels, Hydrogen, Containment System, Safety, Technical guide
The International Maritime Organization (IMO) adopted the Initial IMO GHG Strategy for reducing greenhouse gas (GHG) emissions from ships at the 72nd Marine Environment Protection Committee (MEPC) held in April 2018. The initial strategy includes reduction goals and measures for decarbonizing ships in the present century and is aimed at reducing the carbon intensity of international shipping by 40% by 2030 and 70% by 2050 and reducing the total GHG emissions by 50% by 2050, compared with the levels in 2008.
In achieving the goals of reducing the total GHG emissions specified in the Initial IMO GHG Strategy, using liquefied natural gas (LNG) fuel has limitations because LNG can reduce GHG emissions by only about 20% compared with conventional fuels. Ultimately, it is necessary to use alternative fuels, such as low-carbon or carbon-free fuels, to drastically reduce GHG emissions. Currently, studies are being conducted to apply various alternative fuels, including ammonia, biogas, and hydrogen, to ships.
The commonality of environment-friendly alternative fuels is that they are low-flashpoint fuels. Their flashpoints are lower than those of fuel oils and they are stored in a liquid state under atmospheric pressure at a low temperature. LNG, one of the representative environment-friendly fuels, is stored in a cryogenic environment below −163 ℃ under atmospheric pressure. Therefore, strict standards were applied to select the materials applied to the fuel containment system and to design and evaluate the structure. Using hydrogen as a fuel for ships requires liquefaction and storage at a temperature below −253 ℃, close to absolute zero; thus, hydrogen is rarely used as a fuel for large transport vehicles such as ships or is rarely transported as cargo. Therefore, many technical obstacles exist to the use of hydrogen. In addition to the technical difficulties involved in cryogenic liquefaction and storage and hydrogen embrittlement, the infiltration of hydrogen into metallic materials to cause damage is another major obstacle.
This paper briefly introduces alternative fuels and their characteristics for ships currently being discussed in academic and industrial communities. Table 1 summarizes the physical properties and availability of alternative fuels.
|Storagecondition||– 163℃||– 42℃||Room Temp.||200 bar||– 253℃||– 34℃|
|Density(kg/m3)||430~470||503||786||17.5||71||603 (liquefied at 25℃)|
|Toxicity||Not Toxic||Not Toxic||Low acute toxicity||Not Toxic||Toxic|
|Gravimetricenergy density (MJ/kg)||50||46.3||19.9||120||120||18.6|
|Volumetricenergy density (GJ/m3)||23.4||24.7||15.8||4.5||8.5||12.7|
Hydrogen, the lightest element on Earth, does not emit any pollutants, except for a minimal amount of NOx generated by combustion. However, because the hydrogen on Earth is mostly included in water or organic compounds, hydrogen can be obtained through electrolysis of water, reforming of natural gas, or from a petroleum refining process.
Hydrogen is usually stored by compression at high pressure or by liquefaction. Liquefaction of hydrogen allows storing hydrogen in an amount approximately 800 times more than the hydrogen gas at room temperature under atmospheric pressure. Considering storage capacity, the storage density of liquid hydrogen is approximately four times higher than that of high-pressure hydrogen (200 bar), and the difference may be more than 10 times in terms of transport efficiency and installation site because manufacturing large high-pressure hydrogen vessels is difficult and requires numerous small-sized high-pressure hydrogen vessels. High-pressure hydrogen is normally stored at a pressure of 700 bar or lower; new technologies are now being developed in Korea to pressurize and store hydrogen at 900 bar.
Despite the disadvantages of hydrogen in terms of volume energy density, it is best in terms of mass-energy density . As mentioned above, storing the largest amount of hydrogen in a limited volume involves liquefying and storing it as liquid hydrogen. This method allows for storing the largest amount of energy per fuel mass.
Considering hydrogen molecules are extremely small, they can penetrate a storage vessel or permeate into a material to cause damage. Therefore, hydrogen storage requires an analysis of its resistance to hydrogen damage, hydrogen permeability, and leakage. Liquid hydrogen storage requires maintaining a temperature of −253 ℃ or lower, and a storage vessel with a dual vacuum structure is necessary to suppress or minimize the three modes of heat transfer.
Various factors affect the mechanical behavior of a material, ranging from the composition ratio to the manufacturing method of the material; however, temperature and strain rate are considered the major factors. Additional factors that affect the mechanical performance of a metal exposed to a hydrogen environment are described below.
Hydrogen atoms have an atomic radius of less than 1 Å, much smaller than that of other atoms; thus, they can easily penetrate the lattices of metals. Hydrogen embrittlement refers to the decrease in the mechanical properties of hydrogen-containing metals under an external force, including the yield strength, fracture strength, and elongation, caused by the internal pressure or dislocation slip due to the interactions between the grain boundary and hydrogen atoms. Generally, the average hydrogen concentration inside a material is not so high that embrittlement may occur, but the propagation of hydrogen atoms under the application of stress may result in the formation of hydrogen molecules in a local region of the material. When the threshold is reached, a sudden brittle fracture is likely to occur. The three major factors in hydrogen embrittlement fracture include the external environment to which the material is exposed, inherent properties of the material, and stress applied to the material.
Hydrogen embrittlement is viewed from different angles: 1) the process in which hydrogen permeates into a metallic material, and 2) the process in which the deterioration of the mechanical properties of a metallic material and fracture occurs due to hydrogen . When a metallic material is exposed to a high-temperature and high-pressure hydrogen atmosphere for a long time, hydrogen invades and diffuses into the material, reacts with the solid-soluble carbon or carbines in the metal, and eventually generates methane gas. The irreversible internal cracking or swelling caused by the accumulation of methane gas is explained by a hydrogen attack. In contrast, hydrogen embrittlement is known as the direct action of hydrogen that penetrates a metal as part of the deformation mechanism of the metal, resulting in a decrease in mechanical properties such as strength and ductility. While hydrogen attack is considered a direct cause of cracking, hydrogen embrittlement is related more to the enhancement of crack growth. Different theories exist regarding the mechanism of hydrogen embrittlement. Representative hydrogen embrittlement theories are listed below, with their details described in Appendix C.
In a hydrogen environment, metallic materials undergo a decrease in mechanical performance; for example, tensile strength and elongation. The effect is significantly different on the material characteristics, including the chemical composition, manufacturing process, and hydrogen atmosphere. A previous study showed that in 316 L stainless steel, despite having a high hydrogen concentration, the degree of hydrogen damage was almost constant at different hydrogen concentrations, similar to the conditions without hydrogen charging. In contrast, Inconel 625 showed a considerable decrease in elongation and tensile strength as hydrogen charging was increased . Figures 1 and 2 show the results of the tensile test with 316 L stainless steel and Inconel 625, depending on the hydrogen concentration.
Metallic materials for low-flashpoint fuel containment systems must satisfy the requirements of the IGC/IGF code and the Korean Register Rules for the classification of steel ships. Article 16 (Manufacturing and Testing) of the Low-Flashpoint Fuel Ship Rules, published by the Korean Register, stipulates that tensile tests, impact tests, flexural tests, and cross-sectional observations are necessary. In addition to the necessary testing methods and requirements, an evaluation of the thermal expansion coefficient and thermal conductivity (k) is required to determine the physical properties of the design.
The guidelines for ships carrying liquefied hydrogen in bulk published by the Korean Register require selecting appropriate materials to prevent damage caused by hydrogen embrittlement.
Hydrogen ions can easily diffuse into steel or other materials, caused by the exposure of the material to not only pure hydrogen gas but also the environment of other hydrogen-containing gases, including hydrogen sulfide, hydrogen chloride (HCl), and hydrogen bromide (HBr). Hydrogen ions that diffuse into the material affect its mechanical properties. In the case of steel, hydrogen ions decrease toughness and ductility, thereby embrittling the material. Considering embrittlement may cause a material to be quickly destroyed by a small impact load or deformation, a careful preliminary review of embrittlement is necessary considering its structural integrity.
Typical factors that cause embrittlement are the cryogenic and hydrogen environments. For cryogenic containment systems for low-flashpoint fuels in ships, embrittlement at a target temperature is the most important criterion in material selection. Therefore, to store and utilize liquid hydrogen as a fuel in a ship, it is necessary to determine the temperature and the embrittlement caused by hydrogen as one of the material selection criteria. ISO 16573 is a standard test method for evaluating the hydrogen embrittlement resistance of high-strength steels and presents electrochemical hydrogen charging . Compared with high-pressure hydrogen charging, this method is less expensive and safer. Considering that the amount of hydrogen charging is very small in a cryogenic environment, where the hydrogen mobility is low, electrochemical hydrogen charging is an appropriate testing method.
The international standard provides a method for evaluating hydrogen embrittlement resistance (hydrogen delayed fracture) through a constant load test using a hydrogen-charging specimen. In the case of continuous hydrogen absorption, such as hydrogen charging in an aqueous solution at corrosion potential, hydrogen charging in atmospheric corrosion environments, and hydrogen charging in high-pressure hydrogen gas, the evaluation method is briefly described.
There are four hydrogen charging methods: hydrogen absorption in an aqueous solution at free corrosion potential, cathodic charging, hydrogen absorption in atmospheric corrosion environments, and hydrogen absorption in high-pressure hydrogen gas. The amount of hydrogen absorbed in the specimens can be quantitatively analyzed by thermal desorption analysis, such as gas chromatography and mass spectrometry. The conditions for each method are as follows.
|Solution1||NaCl||30||Large amount of hydrogen|
|Solution 2||NaOH||4||Small amount ofhydrogen|
This study introduces materials suitable for low-flashpoint fuel-containment systems. The materials mentioned herein are based on the materials applicable to a design temperature of −165 ℃ according to Volume 2 (Materials and Welding) of the Korean Register Rules for the classification of steel ships. The rolled steel materials for the cryogenic environment include nickel alloys, rolled stainless steels, aluminum alloys, and highmanganese steels.
Guidelines from the world’s major research institutes and ISO standards provide the following considerations for selecting materials for liquid hydrogen storage: (1) Resistance to hydrogen embrittlement: materials insensitive to hydrogen; (2) Securing ductility at low temperatures: materials with a DBTT lower than the operational temperature; (3) Materials that simultaneously satisfy the two aforementioned conditions.
Performance tests in a high-pressure hydrogen environment have been suggested for evaluating the hydrogen embrittlement resistance of metallic materials. ANSI/CSA CHMC 1-2014(Test Methods for Evaluating Material Compatibility in Compressed Hydrogen Applications – Metals), which is the standard for evaluating compatibility with compressed hydrogen applications, recommends that the specimen should be exposed to a gaseous hydrogen environment at 300 ℃ and 100 bar for eight days to ensure that hydrogen can sufficiently reach the inside of the specimen. However, in liquid hydrogen environments below 20 K, hydrogen mobility is extremely low; thus, hydrogen penetration into the material is extremely limited. Therefore, high-temperature and high-pressure hydrogen environments may cause excessive hydrogen charging, in contrast to cryogenic environments. This study considers that electrochemical hydrogen charging, provided in ISO 16573, may be appropriate for evaluating compatibility with liquid-hydrogen environments.
Candidate materials for application to liquid hydrogen containment systems include a wider range of materials compared to materials applicable to LNG containment systems. Based on the evaluation results, candidates were classified into three groups.
Group A includes materials already extensively applied to liquid hydrogen vessels, with their performance and safety already validated. Group A included 316 L stainless steel and 6061-T6 aluminum alloys. Aluminum alloys have a considerably high resistance to hydrogen and are widely used in cryogenic environments; for instance, Al 6061-T6 is applied to Type 3 high-pressure hydrogen storage vessels.
Group B includes materials expected to be sufficiently applicable to liquid-hydrogen environments, but have not been used for liquid-hydrogen vessels. These are austenitic stainless steels and aluminum alloys that do not exhibit brittle behavior in cryogenic environments. Austenitic stainless steels may be inappropriate for high-pressure hydrogen environments but are highly appropriate for cryogenic environments where hydrogen mobility is decreased, and hydrogen permeation into the materials is low.
Group C includes materials not applicable to cryogenic environments below 20 K or hydrogen environments. Nickel steels with a low nickel content may not be used in cryogenic environments. Special alloy steels, which contain a large amount of nickel, can be used in cryogenic environments; however, they are highly vulnerable to hydrogen environments and are therefore, inapplicable. Nickel steel (9%) is not suitable for liquid hydrogen because it exhibits brittle behavior in cryogenic environments below the LNG storage temperature.
The most environmentally friendly fuels for replacing conventional fuels for ships are low-flashpoint fuels, which are corrosive or cause embrittlement. Therefore, it is necessary to identify the requirements for storing individual fuels and choose the most realistic and economically feasible methods.
Among the many alternative fuels, sufficient information is available regarding materials applicable to methanol, ethanol, ammonia, LPG, and LNG. As these fuels have long been handled by ships as fuel or cargo, sufficient regulations exist regarding the materials applicable to them. In the absence of conditions that lower the mechanical performance of materials, such as a hydrogen exposure environment or corrosion, materials applicable to cryogenic environments are generally applicable to higher temperatures without a problem.
Liquid hydrogen is the fuel that presents the most difficult technical challenge for large-scale storage in ships. Hydrogen should be liquefied and stored in a containment facility designed to maintain a temperature below 20 K. The IGC/IGF Code and the Korean Register Rules for the classification of steel ships require an impact test to be performed at temperatures lower than the operational temperature; however, realistically, it is difficult to carry out an impact test in a cryogenic environment below 20 K.
The design and manufacturing of low-flashpoint fuel containment systems should consider their effects on the base metal and welding. Hence, studies on applying liquid hydrogen to ships require the results of performance tests conducted under conditions equivalent to or harsher than the operational environments. Empirical studies on liquid hydrogen storage and fuel propulsion ships, carried out in advanced countries, have focused on 316 L stainless steel, which has traditionally been known to have excellent hydrogen resistance and applicability to cryogenic environments. However, using only one material is a substantial design constraint and may cause problems in terms of securing economic feasibility.
Therefore, we need to obtain mechanical performance data for tensile, fatigue, and fracture toughness at 20k through follow-up studies, which will provide the performance data of various materials, in addition to 316 L stainless steel, in liquid-hydrogen environments.
This paper is the result of “Development of the Safety standards for marine hydrogen storage vessels and fuel supply systems” research.
Investigation, K. W. Chun; Resources, K. W. Chun; Writing-Original Draft Preparation, K. W. Chun; Writing-Review & Editing, K. W. Chun.
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|2.||Ki-don K., Progress in Solution of Hydrogen Embrittlement of Steels, 2004 (in Korean).|
|3.||K. Murakami, N. Yabe, H. Suzuki, K. Takai, Y. Hagihara, Y. Wada, “Substitution of high-pressure charge by electrolysis charge and hydrogen environment embrittlement susceptibilities for inconel 625 and SUS 316L,” ASME Pressure Vessels and Piping/ICPVT-11 Conference, PVP2006-ICPVT-11-93397, pp. 563-570, 2008. https://doi.org/10.1115/PVP2006-ICPVT-11-93397.
|4.||International Organization for Standardization. ISO 16573 Steel - Measurement method for the evaluation of hydrogen embrittlement resistance of high strength steels, 2015.|
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|7.||NASA, Safety Standard for Hydrogen and Hydrogen Systems - Guidelines for Hydrogen System Design, Materials selection, Operations, Storage, and Transportation 2005.|
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