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The first chemical property of hydrogen discovered is that it forms water (H2O) by flammable reaction when combined with oxygen. Nearly all of the hydrogen on Earth exists in molecular form, such as water or organic compounds, as it forms covalent compounds with most nonmetallic elements. Its chemical formula is H2 and its CAS-Number is 1333-74-0[29].
Hydrogen is a highly flammable hazardous chemical showing flammability: 4 hazard classes (Fig. 1). Important physical and chemical properties of hydrogen are presented in Table 1.
Table 1. Physical and chemical properties of hydrogen[29].
Physical state Gas Form Compressed gas Color Colorless Smell Odorless Melting point −259.2 °C Boiling point −253 °C Critical temperature −240.0 °C Flammability Flammable gas Flammability upper value 74.2% (V) Flammability lower value 4% (V) Vapor pressure 165,316.8 kPa (25 °C) Humidity 0.069 Relative humidity 0.07 Solubility in water 1.62 mg/L Auto-ignition temperature 560 °C Hydrogen is dangerous due to its physical properties, such as high burning rate, low ignition temperature, and low flammability limit. The ignition temperature of hydrogen is lower than that of many other types of gases. Under normal atmospheric conditions, hydrogen concentrations between 4% and 74% with air can form an explosive mixture. Therefore, using or storing hydrogen in a confined space without ventilation is dangerous. The flammability of hydrogen is also a hazard. Once ignited, the flame can spread quickly and pose an explosion hazard. Additionally, when hydrogen burns, a blue flame emits high temperature and intense light. Therefore, it should be taken into account that if hydrogen burns, the flames can be so bright that they can temporarily blind the eyes.
Hydrogen storage tank characteristics
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The hydrogen storage tank specifications specified in the scenario could not be achieved for the hydrogen storage tank in the sample defense facility or another facility producing fuel cells throughout Türkiye. For this reason, locations where fuel cell production and hydrogen storage tanks are used have been researched worldwide. Analyses was carried out considering the hydrogen storage tank properties specified by Cui et al.[30] (Table 2).
Table 2. Hydrogen storage tank specifications[30]
Parameter Value Nominal volume (L) 140 Pressure (atm) 345 Temperature (°C) 24 Orientation Vertical Diameter (m) 4.03 Length (m) 10.98 Tank type Cylinder The high-pressure gaseous hydrogen storage tank included in the study has the most widespread use because it has a simple structure and fast charging and discharging characteristics, which is suitable for hydrogen use. Since the density of hydrogen is low, the design pressure of gas storage tanks generally reaches 35 MPa or even 70 MPa to improve the volumetric energy density of hydrogen tanks[7].
Analysis
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The B-S-T method and ALOHA software were used to determine the explosion effects caused by release in the hydrogen storage tank. Two scenarios were studied in the software, and possible physical impact areas were determined.
Analysis using the B-S-T method
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The B-S-T method was developed to estimate the overpressure (positive and negative pressure waves) and impulse coefficient resulting from VCE. The method assumes that only congested or partially confined parts of the flammable vapor cloud contribute to overpressure accumulation, and the explosion energy (E) is estimated. A curve determines Ps as the combustion energy scaled distance function in the B-S-T method. Numerically determined pressure and impulse coefficient curves taking the flame Mach number as parameters are also used[31].
The Baker-Strehlow-Tang method calculates the scaled distance (Eqn 1).
$ {\rm d}_{\rm n} = \dfrac{\mathit{d}}{{\mathit{M}}^{1/3}} $ (1) dn is the ratio of the distance from the explosion center to the point where the estimated overpressure should be calculated to the cube root of the charge masses (m kg−1/3). Here, d is the actual distance, and the mass value of the explosive is M (kg). The cube root of the charge masses at the explosion center is often used as a scaling parameter. When two explosives with similar geometry but different dimensions explode in the same atmosphere, similar peak overpressures are produced at the same scale distance. This is the simplest and most common form of explosion scaling. Another approach suggested by Sachs is the one that will be used below. The blast wave can be expressed as a scaled overpressure function and is calculated by Eq. (2)[31].
$ \Delta\rm{\mathit{P}}_{\rm{s}}=\dfrac{\mathit{P}\mathrm{\mathrm{_{\mathit{s}}}}}{\mathit{P}_0} $ (2) where, P0 is the atmospheric pressure (Pa), and ΔPs is the peak overpressure (Pa).
Combustion energy is calculated by scaled distance (or Sachs scaled distance) (Eqn 3).
$ \rm{R}=\dfrac{\mathit{d}}{(\mathit{E}/\mathit{P}_0)^{1/3}} $ (3) where, R is scaled distance (m), and E is explosion energy (J).
Analysis with ALOHA software
Location and chemical selection
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The analysis was performed at a defense industry company in Ankara (Türkiye), which houses a hydrogen storage tank for fuel cell production.
Atmospheric conditions
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Modeling studies were conducted in summer conditions to predict more considerable impact distances. Due to higher atmospheric mean temperature in warm seasons, ambient saturation concentration and vapor pressure are higher[26]. June was chosen to represent summer conditions. Summer conditions were chosen for the accident scenario because, in hot weather, hydrogen gas molecules in the air move more and disperse faster. This may cause hydrogen gas to mix with air quickly and react more easily with oxygen. The atmospheric conditions of Ankara province for June are given in Table 3.
Table 3. Atmospheric conditions of Ankara province in June[32].
Parameter Value Air temperature 24 °C Wind speed 3 m/s Wind direction Northwest Cloudiness Open Relative humidity 40% Surface roughness Low Atmospheric stability D Low wind speeds have been shown to account for over 70% of accidents involving VCEs. Low wind speeds cause fuel leakage due to gravity and are associated with massive clouds with a much higher ignition risk[9].
Scenario selection
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Based on past accident data, it was assumed that the release occurred due to the rupture of the 4.26 cm diameter pipe connected to the hydrogen storage tank. Analyses were performed using two different scenarios, which are listed below:
Scenario 1: No fire due to release;
Scenario 2: Jet fire due to release.
Because ALOHA is limited to chemicals that become airborne, it includes models to evaluate the rate at which a chemical will be released and volatilized from the congestion. These 'source strength' models can be critical components in assessing hazards. ALOHA couples source strength models to a dispersion model to estimate the spatial extent of toxic plumes, flammable vapors, and explosive vapor clouds. However, ALOHA does not model all combinations of source strength, scenario, and hazard category for combustion scenarios. The user must select a specific combination from a limited selection. ALOHA uses LOC (Levels of Concern) to address the impact of toxic air plumes, fires, and explosions on human populations. For inhalation hazards, ALOHA's LOCs are concentrations of airborne chemicals associated with adverse health effects. Because ALOHA is primarily used in situations where the goal is to assess the threat a chemical release poses to the general public, it includes LOCs specifically designed to predict how the general public will respond to a short-term release. In limited cases, exposure guidelines developed for worker safety are also compiled and provided to users as an option. The impact intensity of the ALOHA Software decreases in the red, orange, and yellow threat zone order. For toxic inhalation hazards, LOCs are chemical-specific. Thresholds for inhalation toxicity are derived from CAMEO Chemicals. AEGLs (Acute Exposure Guidelines), ERPGs (Emergency Response Planning Guidelines), PACs (Protective Action Criteria), and IDLH (Immediate Danger to Life and Health) limits are stored in data files integrated into ALOHA.
ALOHA models only combustion reactions. ALOHA predicts the blast wave from vapor cloud explosions that are not fully or partially confined by confining walls or ceilings (rapid deflagrations and detonations). Confined vapor cloud explosions produce more damaging blast waves than non-confining or partially confining explosions. The B-S-T model forms the basis of the ALOHA overpressure calculation[33]. The overpressure is estimated using dimensionless, experimentally derived detonation curves based on the flame front propagation velocity and the fuel mass involved in the reaction. The basic principle of this method is the existence of regions within the vapor cloud where physical structures can increase the flame front velocity. These regions are characterized by the structure intensity using a parameter called congestion. Flame velocity is related to the chemical properties of the fuel, the degree of congestion, and the nature of the ignition source. A reactivity term is used to characterize the chemical properties of the fuel. Reactivity ratings are classified according to the chemical laminar burning velocity in the B-S-T method. Low-reactivity chemicals have velocities of less than 45 cm s−1. High reactivity applies to chemicals with a burning rate greater than 75 cm s−1, and those in between are classified as having medium reactivity. Although some chemicals in the ALOHA database are classified according to these criteria, most flammable chemicals in ALOHA are not classified. ALOHA uses medium reactivity in this case because most chemicals do not exceed 75 cm s−1 in laminar burning. ALOHA's method for estimating normalized pressure as a function of distance from the center of the explosive cloud is built on a series of experimentally determined graphs. B-S-T reports pressure values as a function of normalized distance from the center of the congested region, along with different graphs for different flame speeds. For the application of these graphs in ALOHA, the graph data reported by B-S-T was fit to different functions[34].
$ \dfrac{\Delta P}{{P}_{atm}}=D\;\;if\;\;x \lt {x}_{0} $ (4) $ \rm{else}\dfrac{\Delta P}{P_{atm}}=A.B^{1/2}\cdot x^C $ (5) Here ∆P is the maximum overpressure, and A, B, C, D, and x0 are constants. The normalized distance, x, is defined as:
$ x=r{\left(\dfrac{{P}_{atm}}{E}\right)}^{1/3} $ (6) Patm is the atmospheric pressure, and r is the distance from the center of the exploding cloud. The energy contributed to the blast wave is:
$ E=ref.{H}_{c}Mass $ (7) Here, ref is a ground reflection factor, Hc is the fuel's combustion heat, and Mass is the mass of the fuel involved in the explosion. In ALOHA, the reflection factor is set to 2 by B-S-T. This takes into account the reflection of the blast wave from the ground. ALOHA's method is based on a simple conceptual model of the explosive cloud. The cloud is treated as a hemisphere with a uniform ground-level concentration. Higher clouds have a smaller reflection factor.
The most crucial difference between the B-S-T method and ALOHA is determining the mass of fuel contributing to the explosion. In the B-S-T method, the mass of fuel contributed to the explosion is determined by the mass of the compressed areas in a combustible cloud. From the ignition point, the flame travels to the compressed areas, accelerating and decelerating in the uncompressed areas. The mass of fuel contributing to the explosion is simply the mass of fuel in a compressed area. A combustible cloud from a single release can cause as many explosions as there are different compressed areas. Flame velocities are determined by the levels of compression in these areas. In uncompressed areas, the flame speed is assumed to be so slow that it does not produce a significant pressure increase. ALOHA uses a different approach to determine the mass of the fuel causing the explosion, based on recommendations from the American Institute of Chemical Engineers. AIChE recommends that B-S-T detonation curves be combined with an air distribution model to determine the mass of the explosive cloud and that all fuel within the explosive limit be multiplied by an efficiency factor. An efficiency factor of 5% to 20% is recommended, with ALOHA using 20%. ALOHA deviates slightly from AIChE recommendations by using fuel in the concentration range between the upper explosive limit and 90% of the lower explosive limit. This minor change is included in ALOHA to create another protective line in the hazard zone calculation. In ALOHA, referred to as 'hard ignition', or if the average intensity level shows a transition to detonation, 100% of the explosive cloud is used, and Mach 5.2 is used for the flame speed[34].
ALOHA uses a solid flame model to calculate jet-fire thermal radiation hazards. The thermal radiation impinging on a distant target is calculated from the product of the thermal radiation flux at the fire surface, the geometric viewing factor, and the thermal radiative transmittance factor of the atmosphere.
$ q=E.F.\daleth $ (8) where q is the thermal radiation flux incident on a vertical surface (W m−2), E is the thermal radiation energy flux at the surface of the fireball (W m−2), F is the geometric view factor, and
is the transmissivity of the atmosphere to thermal radiation.$\daleth $ Chamberlain's formula is used in ALOHA to determine the flame height of a gas released from a tank. The effect of wind is integrated into the thermal radiation component, the geometric view factor, by correlations. The effects of thermal radiation are a function of the energy flow and the exposure time. For fires exceeding 30 s, the LOC is based on the thermal radiation produced by the flame[34].
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Empirical formulas derived from the best experimental data have been applied to predict hydrogen explosion overpressures, and theoretical derivation and design guidelines for flammable gases and explosives have also been transferred and used for hydrogen explosion overpressure predictions. In engineering applications, there are three traditional approaches widely used to estimate the blast load of VCE: the TNT equivalent method (TNT-EM), the TNO multiple energy method (TNO-MEM), and the Baker-Strehlow-Tang method (B-S-T). TNT-EM converts the released energy of the explosive into the charge energy of TNT in an explosion. TNO-MEM considers the strength of the vapor cloud explosion depending on the boundary conditions, which assumes that the unconstrained part of the vapor cloud contributes little to the blast intensity. The BST method considers different flame speeds of different explosives or VCEs, but is generally similar to TNO-MEM[35,36]. In the B-S-T method, the curve is used to determine the peak pressure (Fig. 2).
Figure 2.
Variation of peak pressure with combustion energy scale distance for different Mach numbers[31].
The strength of the blast wave is proportional to the maximum flame speed in the cloud. The flame Mach number is the apparent flame speed divided by the ambient speed divided by the speed of sound. The appropriate Mf (Mach number) for each modeled case can be selected from Table 4.
Table 4. Mach numbers used in the B-S-T method[31].
Flame expansion Reactivity Congestion Low Medium High 2D High 0.599 DDT DDT Medium 0.47 0.66 1.6 Low 0.079 0.47 0.66 2.5D High 0.47 DDT DDT Medium 0.29 0.55 1.0 Low 0.053 0.35 0.50 3D High 0.36 DDT DDT Medium 0.11 0.44 0.50 Low 0.026 0.23 0.34 In Table 4, no plane limiting flame expansion is considered 3D. The presence of a single limiting plane means 2D flame expansion. Congestion category 2.5D corresponds to situations where the confinement is made either of a frangible panel (which can be expected to fail rapidly and provide ventilation) or a nearly solid confinement plane. Congestion is considered low if the area occupancy rate is below 10%, medium if between 10% and 40%, and high if above 40%. Hydrogen is a highly reactive, highly dispersive gas. Considering the sample plant layout, congestion is selected as low. Considering the low congestion, high reactivity, and 3D propagation, the Mf was determined as 0.36 from Table 4. Calculations were made using the specified correlations and values (Eqns 1−3). The explosion energy E = 154,308 × 106 J was calculated by multiplying the 44,088 m3 (3,968 kg) release gas volume by 5 × 106 J m−3. The scaled distance (R) was obtained as 1.8 at the target distance of 207 m. The dimensionless peak pressure (∆Ps) was determined as 0.06 from the curve in Fig. 2. The peak pressure (Ps) was calculated as 6,079.5 Pa by multiplying this value by the atmospheric pressure (P0). When the vulnerability that the peak pressure would create was interpreted, it was revealed that this pressure would shatter windows and glass[13].
As an active, flammable chemical, hydrogen has a high risk of deflagration and explosion. Post-incident investigations have shown that 20% of the losses in hydrogen accidents are due to fire, while more than 75% are due to explosion. The overpressure in explosions can vary from close to zero to several bars. The threshold value for a safety distance is 2.07 kPa, below which the probability of no severe damage to property is stated to be 0.95%[7].
Traditional methods are designed for a symmetric barrier-free environment, which differs from the specific scenario of hydrogen explosions in confined space. Moreover, hydrogen is more active than traditional flammable gas, which releases more energy and thus produces higher explosion pressure. The existing TNO MEM and BST model parameters for hydrocarbon fuels may not be suitable for hydrogen[7]. The approach, which combines empirical and CFD methods in a balanced way, can provide a tool for more accurate and practical risk assessment related to hydrogen release[1].
Analysis with ALOHA software
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Damage in VCE is related to the shape and size of the blast wave. Peak overpressure and impulse are often used to characterize the blast wave. ALOHA uses only peak pressure to characterize detrimental effects due to the blast wave. The explosion threat zone of the vapor cloud obtained with Scenario-1 is given in Fig. 3.
The chemical mass in the tank is 3,995 kg. The release time is 23 min. The maximum release rate is 971 kg min−1, and the total amount released is 3,968 kg. Red and orange threat zones could not be determined because the exposure limit value was not exceeded in the ALOHA Software. An impact distance of 207 m from the source was determined for the yellow threat zone (> 1.0 psi). In a possible accident scenario, a pressure greater than 1.0 psi will be felt due to the explosion, and the windows of buildings within 207 m will be broken. A Google Earth image of the explosion effect is given in Fig. 4.
Figure 4.
Google Earth image of the explosion threat zone of the vapor cloud for hydrogen storage tanks (Scenario -1).
The hydrogen tank is stored in a closed environment inside the building. For this reason, threat zones are shown in the building where the tank is located. Since the sample facility is located in an industrial area, many facilities are around it. Since the facilities are very close, domino effects can be seen inside and outside the facility. As a result of a possible explosion, the battery factory near the facility may also be affected. Batteries or other flammable materials inside the facility may catch fire, and the fire may spread rapidly. There are also residential areas near the facility. People around may be harmed. Chemicals released due to the explosion can cause water pollution and damage the ecosystem. It is essential to eliminate or minimize this impact in emergency plans. It is challenging to mitigate the hydrogen explosion in the event of a leak by eliminating ignition sources. In addition, due to the minimal ignition energy, when hydrogen is released at high pressure, the strong shock wave generated by the high-pressure hydrogen jet can cause hydrogen to ignite spontaneously. The minimum ignition energy required by the hydrogen-air cloud is affected by the ambient temperature, which decreases as the temperature increases[7]. Other threat zones identified within the scope of Scenario-1 are given in Fig. 5.
Figure 5.
(a) Flammable threat zone of vapor clouds. (b) Toxic threat zone of the vapor cloud for hydrogen storage tanks (Scenario-1).
The toxic threat zone represents the region where the vapor cloud contains chemicals that have toxic effects. AEGLs, ERPGs, and PACs are level public exposure guidelines developed for accidental chemical release events. Although developed by different organizations, all three exposure guidelines share the approach of assessing the effects of chemical exposure by using levels to define increasing severity associated with increasing concentration. Toxic effects that may harm human health may occur in this zone due to inhalation or contact with vapor. Two factors affect the consequences of inhaling toxic substances. The first is the concentration of the inhaled substance, and the second is the duration of inhalation[28]. The largest impact distance in the toxic threat zone was seen in the yellow region, 130 m (> 65,000 ppm, PAC-1) away from the source. Lethal effects were observed at a distance of 52 m (> 400,000 ppm, PAC-3) from the source. Atmospheric conditions and emission height in accident scenarios are important variables that determine the size of the toxic vapor cloud[4]. Atmospheric stability refers to the stability of the vertical movement of air masses. In simpler terms, it indicates how strong or weak the tendency of an air mass in the atmosphere to rise or fall is. The D-class stability selected in the study generally refers to a stable air mass in the atmosphere. The flammable threat zone of the vapor cloud refers to the zone where the vapor cloud has flammable properties. In this zone, there may be a risk of burns and explosions if the steam comes into contact with an ignition source. In the flammable zone analysis, 60% of the lower flammability limit is used as the level of concern. It was observed that lethal effects may occur 301 m (> 24,000 ppm, 60% LEL: Flame Pockets) away from the source. Wind direction confidence lines around the threat zone, and approximately 95% of the chemical plume is expected to remain contained[25]. The Google Earth image of the flammable area of the vapor cloud where the largest effects were observed is given in Fig. 6.
Figure 6.
Google Earth Image of the flammable threat zone of vapor clouds for hydrogen storage tanks (Scenario-1).
From Fig. 6, it can be seen that thermal radiation may affect the facilities and settlements. Hydrogen has a wider flammable concentration range than most hydrocarbons. The flammability limit range is greater when a hydrogen flame propagates upward than when it propagates downward. Factors such as temperature, pressure, the presence or absence of diluent, and the structure's shape can all affect hydrogen's flammability limits. Hydrogen can only ignite when the ignition energy is greater than the minimum ignition energy. The minimum ignition energy of hydrogen in air is 101.3 kPa and less than 0.02 MJ at ambient temperature. Therefore, hydrogen can ignite in the presence of any weak ignition source (electric spark, hot surface, open flame, etc.) or even static electricity from the human body (up to 8.33 MJ)[7].
The thermal radiation threat zone determined according to Scenario-2 is given in Fig. 7.
The maximum flame length is 9 m, and the burn lasts 23 min. The effects of thermal radiation are a function of energy flow and exposure time. The effect of thermal radiation on humans depends on the exposure time and radiation intensity. ALOHA calculates the energy flux associated with radiation as a function of distance and fire duration. The impact distance to the red threat zone is 40 m (> 10 kW m−2), and the effect of thermal radiation is considered lethal. The impact distance for the orange threat zone is 56 m (> 5 kW m−2), and second-degree burns may occur as a consequence; the impact distance for the yellow threat zone is 87 m and may cause pain (> 2 kW m−2).
All impact distances determined for the scenarios are given briefly in Table 5.
Table 5. All impact distances for scenarios used in the present study.
Scenario Zone Red threat zone (m) Orange threat zone (m) Yellow threat zone (m) Scenario-1: No fire due to release Toxic threat zone 52 69 130 Flammable threat zone 301 − 711 Explosion threat zone − − 207 Scenario-2: Jet fire due to release Thermal radiation threat zone 40 56 87 As a result of the release of the chemical without burning (Scenario-1), a toxic zone, a vapor cloud flammable zone, and a vapor cloud explosion zone were detected. With Scenario-2, the thermal radiation threat zone was obtained due to a jet fire. The largest impact distance for the hydrogen storage tank was determined for the flammable threat zone of the vapor cloud where there was no fire due to release. It has been seen that it is necessary to create a protective zone around the hydrogen tank to reduce the hazards. It is known that the protective zone distances are different for each chemical. These distances vary depending on the degree of danger of the chemical, its physical and chemical properties, vapor movement, or momentum speed[37,38]. In terms of the affected population, factors such as the number of people, distance from the tank, shelter, operator intervention, etc., gain importance[39,40]. The use of personal protective equipment, training, etc., and strategies for employees within the threat zones estimated by ALOHA, can be applied to reduce the loss of life[27].
The vapor cloud explosion threat zone refers to the potentially explosive region of the vapor cloud. An explosion may occur in this region when explosion pressure and ignition conditions are met. ALOHA includes three LOCs that quantify indirect and direct effects. Glass windows can break above 1 psi, and at 3.5 psi, severe injuries from eardrum rupture and flying debris can occur. At 8 psi, the risk of ear and lung damage and indirect effects due to the collapse of unreinforced buildings becomes significant. For the yellow threat zone, it has been determined that the windows of buildings can be broken by the explosion effect (1 psi) in the impact distance 207 m away from the source. At the same distance, the peak pressure was calculated as 6.1 kPa (~1 psi) using the B-S-T method, and it was concluded that the windows could break. Although there are no direct effects on human health, it can be said that injuries due to glass breakage may occur. Software and correlation results were found to be compatible. This is an inherent consequence of the software based on the B-S-T explosion model. In Scenario-2, the largest impact distance of thermal radiation was in the yellow threat zone. The yellow threat zone is less harmful than the orange and red threat zone. The results obtained with the hazardous properties of hydrogen were parallel.
Assessing the role and effectiveness of barriers against hydrogen leaks with QRA (Quantitative Risk Assessment) and calculating the probability of barrier failure for the final consequences can help to reach more realistic conclusions. Combining the results of the researchers' work with the results of this study can provide a more accurate decision-making ability to manage safety risks[26].
Ventilation is one of the simplest and most effective ways to reduce and mitigate gas explosions. Ventilation can help reduce the concentration of flammable gas and relieve explosion overpressure[41]. Explosion suppression materials/structures are of interest to mitigate hydrogen-air cloud explosions in confined spaces. Explosion suppression materials are mesh or porous structures filled into confined containers or channels. With specially designed shapes and dimensions, these structures will reduce flame speed and hydrogen concentration, thus mitigating the explosion effect[42]. Drainage systems should be equipped with water traps to prevent flammable vapors from penetrating the drainage system. Control rooms should be designed to prevent the entry of flammable vapors when there is a risk of exposure to flammable gas. For example, a vapor-tight building with positive internal pressure may be designed to prevent the penetration of a flammable cloud into the building. Maintenance procedures should provide increased oversight of those parts of the plant that contain more reactive flammable liquids and vapors. Operators and maintenance engineers should be briefed on the hazards of explosions as part of process safety training courses[12]. One way to limit the extent of a flammable cloud is to use a vapor fence to contain the cloud. This may have the advantage of limiting the spread of heavier-than-air pancake-shaped clouds. In dense areas, fuel gas sensors can be installed to give dangerous flammable clouds the needed size. Careful consideration should also be given to the exact use of trees and vegetation around the site, limiting their width to less than 2 m. When designing new facilities, attention should be paid to separating congested areas to limit flame acceleration. Empty buildings located near or within process units may have a collapsible wall to prevent high overpressures from building up inside the building. This can prevent the transition of an external flammable cloud to a high-velocity jet of ignition and possible explosion[15].
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I want to thank Beyza Akbas for her contribution to the study.
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About this article
Cite this article
Cetinyokus S. 2024. Determination of possible industrial accident effects on a hydrogen storage tank in a fuel cell production facility. Emergency Management Science and Technology 4: e020 doi: 10.48130/emst-0024-0020
Determination of possible industrial accident effects on a hydrogen storage tank in a fuel cell production facility
- Received: 22 July 2024
- Revised: 31 August 2024
- Accepted: 14 September 2024
- Published online: 10 October 2024
Abstract: Hydrogen fuel cells are an essential energy alternative in reducing emissions that cause climate change. However, hydrogen is not an innocent chemical, and it is crucial to ensure safety measures. The aim of the current study was to contribute to the relevant safety research by determining the possible accident effects of hydrogen storage tanks in a fuel cell production facility. ALOHA (Areal Locations of Hazardous Atmospheres) Software and the B-S-T (Baker-Strehlow-Tang) method were used to model the accident effects. The first case study for Türkiye was performed by taking a fuel cell production facility in Ankara. Considering past accident data, it was assumed that there was a leak of 4.26 cm in diameter in the hydrogen storage tank (D = 4.03 m, L = 10.58 m, V = 140 L) operated at 345 atm in the example facility. Meteorological data for June for the province represented the conditions where hydrogen would show a more significant dispersion. Two different scenarios, no fire and jet fire due to release, were modeled with ALOHA Software. For the release of hydrogen with no fire, the toxic threat zone of the vapor cloud, the flammable threat zone of the vapor cloud, and the explosion threat zone of the vapor cloud were determined. Thermal radiation threat zones were determined in case of a jet fire. The largest impact distances were obtained for the flammable threat zone of the vapor cloud (red threat zone = 301 m, > 24,000 ppm, 60% LEL: Lower Explosive Limit). This was followed by the explosion threat zone of the vapor cloud with an impact distance of 207 m (> 1 psi). It was determined that the windows of buildings can be broken by the explosion effect (1 psi) at a distance of approximately 200 m using the B-S-T method. Software and correlation results were found to be compatible with each other. Although there were no direct effects on human health, it was shown that injuries due to glass breakage may occur.