Strength Analysis of Ductile Iron Gearbox Housing for AC Locomotives

In the present study, I conducted a comprehensive strength assessment of a ductile iron gearbox housing used in AC electric locomotives. As a key structural component in the locomotive traction system, the gearbox housing must withstand complex alternating loads including impact loads, vibration loads, and periodically varying torques under harsh operating conditions. The material of the housing is ductile iron, specifically EN-GJS-400-18-LT, which exhibits excellent mechanical properties and fatigue resistance. My investigation covers both normal working conditions and abnormal conditions, with detailed finite element simulation carried out under multiple load combinations.

The analysis demonstrates that ductile iron castings are increasingly important in modern railway applications. The inherent strength, damping capacity, and casting flexibility of ductile iron castings make them an ideal choice for complex transmission housings. Through finite element analysis, I computed the stress distribution under various loading states defined according to the IEC 61373–2010 standard. For normal working conditions, I adopted the maximum starting torque of 310 N·m together with direction-dependent inertial impact accelerations. For abnormal working conditions, I applied the motor short-circuit torque of 740 N·m. The fatigue strength was evaluated using the Goodman criterion under normal working conditions, while yield strength and ultimate tensile strength were applied as evaluation benchmarks for the abnormal conditions.

My results confirm that all node stress states under normal working conditions fall within the safe region bounded by the Goodman curve, thus satisfying the fatigue requirements of the relevant technical specification TJ/JW 064–2015. Under abnormal working conditions, the maximum Von Mises stress and maximum principal tensile stress remain well below the yield limit and the ultimate tensile strength of ductile iron castings respectively. Several stress concentration zones were identified, particularly around the suspension rod seats and bearing mounting positions, which provide valuable insight for future structural optimization. The detailed methodology, simulation parameters, and quantitative results are presented in the following sections.

1. Gearbox Configuration and Design Parameters

The gearbox under study plays a vital role in the overall traction system of the AC locomotive. It is responsible for transmitting power from the traction motor to the wheelset, reducing the rotational speed, and bearing the complex dynamic loads generated during gear meshing. The gearbox adopts a two-stage helical gear transmission architecture, which enables a compact structural envelop while providing a high reduction ratio. The housing is manufactured as an integral casting using ductile iron, which is known for its superior combination of strength, ductility, and impact resistance. These attributes of ductile iron castings render them particularly suitable for railway gearbox housings where integrity under cyclic loads is critical.

The gearbox structure includes several functional features integrated into the housing: bearing seats, lubrication oil passages, mounting brackets, and suspension lugs. The main components comprising the gearbox assembly include the housing, gear pump, bearings, seals, and suspension rods. The input shaft is connected to the traction motor and carries high rotational speeds, whereas the output shaft is coupled to the wheelset and transmits high torque. The housing supports all static and dynamic loads and must possess sufficient stiffness to maintain gear alignment and mesh quality. A forced lubrication system is adopted to ensure reliable operation of gears and bearings under high-speed running conditions.

Table 1 summarizes the fundamental calculation parameters of the gearbox considered in my analysis.

Parameter Value
Transmission type Two-stage helical gear
Gear ratio 13.647
Motor rated power / kW 31
Motor starting torque / (N·m) 310
Motor rated speed / (r/min) 1150
Motor rated torque / (N·m) 257

Table 1. Gearbox fundamental calculation parameters

The housing material employed in my simulation is ductile iron specified as EN-GJS-400-18-LT. This grade of ductile iron castings provides a guaranteed minimum yield strength of 240 MPa and ultimate tensile strength of 400 MPa, along with an elongation of 18% at break. The mechanical properties of the material used in the finite element model are listed in Table 2.

Property Value
Tensile strength Rm / MPa ≥ 400
Yield strength Rp0.2 / MPa ≥ 240
Elongation A / % ≥ 18

Table 2. Mechanical properties of ductile iron EN-GJS-400-18-LT

Ductile iron castings exhibit a characteristic stress-strain response that differs from that of steel in certain aspects. For the purpose of the strength analysis, I treated the material as elastoplastic with linear hardening in the plastic regime. The constitutive model may be expressed in simplified form as:

$$ \sigma = \begin{cases} E\,\varepsilon & \text{for } \sigma \leq R_{p0.2} \\[4pt] R_{p0.2} + E_{t}\left(\varepsilon – \varepsilon_{y}\right) & \text{for } \sigma > R_{p0.2} \end{cases} $$

where $E$ is the elastic modulus, $E_{t}$ is the tangent modulus in the plastic region, and $\varepsilon_{y}$ denotes the strain at the yield point. The yield strength of ductile iron castings is a major consideration when evaluating the structural performance under overload conditions. By using the well-documented properties of EN-GJS-400-18-LT, I ensured that the simulation accurately reflects the realistic behavior of the housing under the applied loading profiles.

2. Finite Element Modelling of the Gearbox Housing

I developed a detailed three-dimensional finite element model of the gearbox housing to evaluate its structural integrity. Because the housing geometry is complex with curved surfaces, bolt holes, bosses, and reinforcement ribs, special attention is required in mesh generation and boundary condition definition to achieve accurate results without excessive computational cost. The complete model includes the upper casing, lower casing, gear shafts, bearings, and various accessory components that collectively represent the load transmission path.

2.1 Geometric Model Simplification

Before constructing the finite element mesh, I performed a geometric cleanup process on the CAD model. Small features that do not affect the global stress distribution, such as small chamfers, threaded holes, nameplate recesses, and minor fillets, were either removed or suppressed. This simplification is necessary to mitigate unwanted local stress singularities and to reduce the total number of elements. However, all geometrically significant details that could influence load transfer, such as bearing housings, bolted joint regions, and suspension attachments, were retained with their original dimensions.

2.2 Meshing Strategy

The mesh was generated using a combination of tetrahedral and hexahedral elements. The gear teeth and bearing areas, which require higher fidelity, were meshed with refined hexahedral elements. The remaining portions of the housing were predominantly meshed with tetrahedral elements. The total number of nodes exceeded one million, which is sufficient to capture the stress gradients in the loaded regions. Figure 1 illustrates the overall mesh of the gearbox housing, while Figure 2 presents the detailed mesh at the gear contact region.




The mesh quality was verified by examining aspect ratios and Jacobian values of the elements in critical zones. The minimum element size near the fillets and around bearing seats was kept below 1.5 mm to resolve the local stress concentration. The element quality metrics satisfied the acceptance criteria recommended by the solver documentation, ensuring that the computed stress values are reliable. A convergence study was also carried out by comparing stress results with successively refined mesh densities. The difference in maximum Von Mises stress between the intermediate and fine mesh configurations was less than 3%, indicating that the mesh density used is adequate for the strength evaluation.

2.3 Contact Interface Definitions

The interaction between different components of the gearbox assembly influences the load distribution in the housing. I defined appropriate contact pairs at all critical interfaces, as listed in Table 3. The bearing-to-housing contacts are represented using revolute joint elements, which permit rotational degrees of freedom while constraining translational motion. This approach correctly simulates the load transfer through rolling element bearings into the housing structure.

Contact Pair Components Interface Type
Bearing-housing contacts Housing and input bearing Joint-Revolute
Bearing-housing contacts Input sleeve and input bearing Joint-Revolute
Bearing-housing contacts Upper housing and intermediate shaft bearing Joint-Revolute
Bearing-housing contacts Output sleeve and output bearing Joint-Revolute
Bearing-housing contacts Lower housing and intermediate shaft bearing Joint-Revolute
Gear-to-gear contact Input gear and output gear No Separation
Other connections Various Bonded

Table 3. Contact interface types in the finite element model

2.4 Boundary Conditions and Load Application

To accurately replicate the actual operating environment of the gearbox housing, I applied three types of boundary conditions: inertial acceleration, gravitational acceleration, and torque loading. In the finite element model, the acceleration values were assigned at the center of mass reference point using the coordinate system convention specified in the standard. The applied loads are depicted in Figure 3. The point labeled A in the figure represents the location where inertial impact accelerations are applied. The magnitude and direction of these accelerations are listed in Tables 4 and 5 for normal and abnormal conditions, respectively. Point B indicates the gravity acceleration acting in the vertical direction with a value of $g = 9.8\,\text{m/s}^2$.

Torque is applied at point C according to the values presented in the corresponding tables. Fixed constraints are imposed at the suspension rod seats (point D), at the bearing locations (point F), and at the secondary driven gear (point E). These constraints replicate the actual mounting configuration of the gearbox to the locomotive bogie frame. The load cases are defined to cover all combinations of positive and negative directions of the inertial accelerations, thereby maximizing the coverage of possible loading scenarios.

3. Loading Conditions

3.1 Normal Working Conditions

Normal working conditions correspond to the regular operation of the locomotive. Among these conditions, the starting condition generates the highest motor torque (310 N·m), while other running states produce lower torque values. According to the provisions of IEC 61373–2010, inertial impact accelerations must be applied in different directions simultaneously. In my evaluation, I selected the starting condition as the representative normal working condition because it produces the highest boundary stresses. If the fatigue strength at this extreme state satisfies the Goodman criterion, all other normal operating states will automatically meet the requirement.

A total of sixteen load combinations were constructed for the normal working condition by combining the torque direction and eight acceleration direction combinations. The load cases are identified as ZZ1 through ZZ8 as well as ZF1 through ZF8, where the letter Z denotes the normal case; the second letter Z or F indicates positive or negative torque direction respectively. The detailed values are provided in Table 4.

Case Ax (running direction) / (m/s²) Ay (axle direction) / (m/s²) Az (vertical) / (m/s²) Torque / (N·m)
ZZ1 64.3 129 144 310
ZZ2 64.3 129 -144 310
ZZ3 -64.3 129 144 310
ZZ4 -64.3 129 -144 310
ZZ5 64.3 -129 144 310
ZZ6 64.3 -129 -144 310
ZZ7 -64.3 -129 144 310
ZZ8 -64.3 -129 -144 310
ZF1 64.3 129 144 -310
ZF2 64.3 129 -144 -310
ZF3 -64.3 129 144 -310
ZF4 -64.3 129 -144 -310
ZF5 64.3 -129 144 -310
ZF6 64.3 -129 -144 -310
ZF7 -64.3 -129 144 -310
ZF8 -64.3 -129 -144 -310

Table 4. Normal working condition load cases with acceleration and torque values

3.2 Abnormal Working Conditions

Abnormal working conditions represent extreme states that may occur rarely but must be considered in structural design. The motor short-circuit condition produces the highest possible torque on the gearbox, making it the most severe abnormal case. I selected this condition with an input torque of 740 N·m. Similar to the normal working conditions, inertial impact accelerations were applied according to IEC 61373–2010 requirements. A total of sixteen load combinations (CZ1–CZ8 and CF1–CF8) were defined for this scenario, as listed in Table 5. The evaluation result of these abnormal cases was compared against the yield strength and the ultimate tensile strength of the ductile iron castings.

Case Ax (running direction) / (m/s²) Ay (axle direction) / (m/s²) Az (vertical) / (m/s²) Torque / (N·m)
CZ1 1000 1000 1000 740
CZ2 1000 1000 -1000 740
CZ3 -1000 1000 1000 740
CZ4 -1000 1000 -1000 740
CZ5 1000 -1000 1000 740
CZ6 1000 -1000 -1000 740
CZ7 -1000 -1000 1000 740
CZ8 -1000 -1000 -1000 740
CF1 1000 1000 1000 -740
CF2 1000 1000 -1000 -740
CF3 -1000 1000 1000 -740
CF4 -1000 1000 -1000 -740
CF5 1000 -1000 1000 -740
CF6 1000 -1000 -1000 -740
CF7 -1000 -1000 1000 -740
CF8 -1000 -1000 -1000 -740

Table 5. Abnormal working condition load cases with acceleration and torque values

4. Fatigue Strength Evaluation under Normal Working Conditions

4.1 Goodman Fatigue Criterion for Ductile Iron Castings

Fatigue failure is a primary concern for the gearbox housing of AC locomotives due to the highly cyclic nature of the applied loading. The alternating load originates from gear meshing forces, inertial forces during vehicle motion, and torque fluctuations from the traction motor. To evaluate the fatigue performance of the housing, I employed the Goodman fatigue criterion, which is widely used for assessing the combined effects of mean stress and alternating stress. The Goodman relationship is defined as:

$$ \frac{\sigma_a}{\sigma_{e}} + \frac{\sigma_m}{R_m} = 1 $$

where $\sigma_a$ represents the alternating stress amplitude, $\sigma_m$ is the mean stress, $\sigma_{e}$ is the fatigue limit of the material under fully reversed loading, and $R_m$ is the ultimate tensile strength. For each node in the finite element model, I extracted the maximum and minimum principal stresses from the load combinations in Table 4. The alternating stress and mean stress are then calculated as:

$$ \sigma_a = \frac{\sigma_{\max} – \sigma_{\min}}{2} $$

$$ \sigma_m = \frac{\sigma_{\max} + \sigma_{\min}}{2} $$

The fatigue safety factor $n_f$ at each node is subsequently determined from:

$$ n_f = \frac{1}{\dfrac{\sigma_a}{\sigma_e} + \dfrac{\sigma_m}{R_m}} $$

where $R_m = 400$ MPa is the tensile strength of ductile iron castings EN-GJS-400-18-LT, and the fatigue limit $\sigma_e$ is taken as 183 MPa for the considered material and surface condition. This fatigue limit value corresponds to the endurance limit for high-cycle fatigue of smooth specimens under rotating bending loading.

4.2 Construction of the Goodman Diagram

I constructed the Goodman diagram based on the allowable stress region specified by the relevant technical standard TJ/JW 064–2015. The allowable region in the mean stress – alternating stress coordinate system is defined by a polygon with vertices having the following coordinates:

Point Mean stress $\sigma_m$ / MPa Alternating stress $\sigma_a$ / MPa
A 0 183
B 105 240
C 240 240
D 105 -30
E 0 -183
F -57 -240
G -240 -240
H -57 126

Table 6. Coordinates of the vertices defining the Goodman fatigue safety region

For each node in the housing finite element model and for each pair of load cases with the same acceleration direction but opposite torque direction, I computed the maximum principal stress $\sigma_{\max}$ and minimum principal stress $\sigma_{\min}$. The mean stress and alternating stress were then determined from the expressions above. These points were plotted on the Goodman diagram to verify whether all of them lie within the allowable region.

4.3 Fatigue Analysis Results

After conducting the finite element analysis for the sixteen normal working condition load cases, I extracted the principal stress values at every node of the housing model. The resulting scattered points were plotted on the Goodman diagram as shown in my analysis. All points corresponding to the entire set of housing nodes were found to be contained within the boundaries of the Goodman region. This indicates that the ductile iron gearbox housing possesses adequate fatigue strength to withstand the alternating loads associated with the starting condition, which is the most severe normal operating condition.

From the fatigue analysis, the minimum fatigue safety factor obtained among all nodes was approximately 1.25, which occurs at the suspension rod seat region. This value exceeds the allowable minimum of 1.0, and thus confirms the fatigue safety of the design. The margin of 25% provides additional robustness against uncertainties in loading estimation, material property variation, and manufacturing imperfections. Since ductile iron castings are known to exhibit variability in their mechanical properties depending on casting quality and section thickness, this safety margin is particularly meaningful for ensuring long-term reliability.

It is important to highlight that the fatigue verification considered all nodes simultaneously, rather than only the maximum principal stress locations. This conservative approach ensures that even the most critical point in the housing satisfies the fatigue requirement. The comprehensive node-based evaluation also accounts for multiaxial stress states and local geometric effects, which are essential for a robust fatigue assessment of complex component geometries.

5. Strength Evaluation under Abnormal Working Conditions

5.1 Evaluation Criteria

For the abnormal working conditions, I used a static strength criterion because these conditions occur only once or a few times during the lifetime of the gearbox. The maximum torque of 740 N·m generated during motor short-circuit conditions creates severe stresses that shall not cause permanent deformation or fracture of the housing. Two strength limits are considered for the ductile iron material:

$$ \sigma_{e,\max} < R_{p0.2} = 240\,\text{MPa} $$

$$ \sigma_{t,\max} < R_m = 400\,\text{MPa} $$

where $\sigma_{e,\max}$ is the maximum Von Mises equivalent stress and $\sigma_{t,\max}$ is the maximum principal tensile stress. The first criterion ensures that the material remains in the elastic range, preventing permanent plastic deformation of the gearbox housing. The second criterion guarantees that no fracture will occur even if local yielding takes place at high-stress regions. Since the material of the housing, ductile iron EN-GJS-400-18-LT, has a ratio of tensile strength to yield strength equal to 1.67, satisfying the yield criterion automatically ensures a substantial margin against rupture.

5.2 Von Mises Equivalent Stress Calculation

The Von Mises equivalent stress at each node was computed using the standard formulation based on the three principal stresses, denoted by $\sigma_1$, $\sigma_2$, and $\sigma_3$:

$$ \sigma_{e} = \sqrt{\frac{1}{2}\left[(\sigma_1 – \sigma_2)^2 + (\sigma_2 – \sigma_3)^2 + (\sigma_3 – \sigma_1)^2\right]} $$

This equivalent stress is compared directly with the yield strength of the material for the static strength verification. The maximum principal tensile stress $\sigma_1$ was likewise extracted for each load case to assess the risk of brittle fracture, which is advisable for ductile iron castings containing graphite nodules that might act as crack initiation sites under sufficient tensile loading.

5.3 Simulation Results for Abnormal Conditions

The finite element analysis for the sixteen abnormal load cases produced consistent results in terms of stress magnitudes and locations. Table 7 summarizes the maximum Von Mises stress and the maximum principal tensile stress computed for each load case. As can be observed from the table, all values are significantly below the yield strength of 240 MPa. The largest Von Mises equivalent stress among all abnormal cases is 110.8 MPa, obtained for load case CZ5, while the largest principal tensile stress is 141 MPa, which belongs to load cases CZ2 and CF2.

Load Case Maximum Von Mises Stress / MPa Maximum Principal Tensile Stress / MPa
CZ1 101.8 94.1
CZ2 105.0 141.0
CZ3 91.9 101.4
CZ4 106.7 127.5
CZ5 110.8 77.5
CZ6 92.3 106.1
CZ7 107.5 113.2
CZ8 98.7 111.4
CF1 101.8 94.1
CF2 105.0 141.0
CF3 91.9 101.4
CF4 106.7 127.5
CF5 110.8 77.5
CF6 92.3 106.1
CF7 107.5 113.2
CF8 98.7 111.4

Table 7. Maximum equivalent and principal tensile stresses under abnormal working conditions

The stress analysis shows a clear anisotropy in the structural response: certain load cases produce higher tensile stresses while others produce higher Von Mises stresses. For instance, load case CZ2 is characterized by the highest tensile stress while CZ5 produces the highest Von Mises stress. This demonstrates that evaluating only one stress measure may not be sufficient to fully assess structural integrity. Hence, my dual criterion approach provides a more comprehensive safety evaluation.

5.4 Stress Distribution in Critical Regions

For load case CZ2, the maximum principal tensile stress occurs at the suspension rod lug connection region, with a magnitude of 141 MPa. The Von Mises stress under this same load case reaches a value of 105 MPa and is located at the lower left zone of the input shaft bearing housing. For load case CZ5, on the other hand, the maximum Von Mises stress is located at the intermediate shaft bearing position with a magnitude of 111 MPa, while the maximum principal tensile stress of 77.6 MPa appears at the lower position of the input gear shaft axis.

The difference in the positions of the maximum stresses between these two load cases indicates that the stress distribution is highly sensitive to the direction of the inertial accelerations. This is an important observation for the design of ductile iron castings for railway applications. The stress concentrations observed in the simulation are associated with geometric discontinuities such as sudden changes in cross-section, reduction of wall thickness, and bearing seating areas. These regions should be carefully considered during the structural optimization phase to further enhance the fatigue resistance of the housing.

5.5 Strength Margins

To quantify the safety margin under abnormal conditions, I calculated the utilization factor defined as the ratio of the computed stress to the allowable strength. For the maximum Von Mises stress of 110.8 MPa, the utilization with respect to the yield strength is:

$$ \eta_{y} = \frac{110.8}{240} = 0.462 = 46.2\% $$

For the maximum principal tensile stress of 141 MPa, the utilization with respect to the ultimate tensile strength is:

$$ \eta_{u} = \frac{141}{400} = 0.353 = 35.3\% $$

These utilization factors indicate that the gearbox housing retains sufficiently large strength reserves even under the most severe abnormal conditions examined in my study. The safety factors corresponding to these utilization rates are 2.17 and 2.84 respectively, which are well above the minimum recommended values for such critical components.

6. Discussion

6.1 Interpretation of Stress Concentration Zones

My simulation identified regions of elevated stress at the suspension rod seats, at the lower side of the input bearing, and at the intermediate bearing bore. These locations represent inherent geometric discontinuities where load paths change direction abruptly, and hence create localized stress intensification. In ductile iron castings, such stress concentrations are particularly relevant because graphite nodules can act as internal stress raisers under cyclic loading. However, since the maximum stresses observed are well below the fatigue and static strength limits, the component is considered safe for the intended application.

6.2 Effect of Material Variability in Ductile Iron Castings

The mechanical properties of ductile iron castings can vary depending on the solidification cooling rate, section thickness, heat treatment condition, and quality of the casting process. To account for this variability, design specifications commonly assume minimum guaranteed values, which I used in my evaluation. The analysis results confirm that even with the minimum property values, the gearbox housing exhibits sufficient safety margins. This provides confidence in the reliability of ductile iron castings for this type of structural application.

6.3 Recommendations for Design Optimization

Although the current design satisfies all strength requirements, I observed that certain regions exhibit higher stresses than the surrounding areas. To enhance the fatigue life and ensure robustness at the stress concentration locations, the following structural optimization measures could be implemented:

  1. Increase the fillet radius at the junction between the suspension rod seats and the housing main body.
  2. Add reinforcement ribs around the input bearing housing to distribute loads more broadly over the casing.
  3. Optimize the wall thickness distribution to achieve a more uniform stress state throughout the housing.
  4. Improve the local surface quality by grinding or shot peening in the high-stress zones to increase the fatigue strength of the ductile iron castings.

These measures would further reduce the risk of fatigue crack initiation in the long-term service life of the gearbox. Since ductile iron castings offer excellent machinability and casting flexibility, implementing such geometric changes typically requires only minimal modifications to the casting patterns, thereby limiting the incremental manufacturing cost.

6.4 Validation of the Finite Element Methodology

The finite element approach used in my work is based on well-established principles of structural mechanics and has been validated through extensive engineering practice in the railway industry. The loads and boundary conditions are defined in accordance with international standards, and the material properties correspond to the certified characteristics of EN-GJS-400-18-LT ductile iron. The integration of the Goodman fatigue criterion with node-based evaluation provides a rigorous and conservative assessment of fatigue safety. The same methodology may be directly applied to evaluate other gearbox housings manufactured from ductile iron castings with similar geometry and loading conditions.

7. Conclusion

In this work, I performed a comprehensive structural strength analysis of the ductile iron gearbox housing used in AC electric locomotives. The evaluation covered both normal working conditions and abnormal working conditions with all relevant load combinations specified by the applicable standards. The following conclusions can be drawn from my study.

(1) Under normal working conditions, the starting state with the maximum motor torque of 310 N·m is the governing load case. The Goodman fatigue criterion applied to all housing nodes demonstrates that the minimum and maximum principal stresses for all nodes lie within the allowed fatigue safety region. This confirms that the gearbox housing has sufficient fatigue strength for long-term reliable operation.

(2) Under abnormal working conditions characterized by the motor short-circuit torque of 740 N·m, the maximum Von Mises equivalent stress is 110.8 MPa and the maximum principal tensile stress is 141 MPa. Both values are significantly lower than the yield strength (240 MPa) and the ultimate tensile strength (400 MPa) of the ductile iron material, respectively. The corresponding safety factors are 2.17 for yielding and 2.84 for fracture, confirming the robustness of the structural design.

(3) Stress concentrations are present at the suspension rod attachments, the lower input shaft bearing area, and the intermediate bearing seating region. These locations exhibit higher stresses but still remain within acceptable limits. Future design iterations should focus on enlarging fillet radii and adding local reinforcing ribs at these critical positions to further improve the fatigue performance of the ductile iron castings.

(4) The finite element analysis methodology established in my study, including load case construction, boundary condition definition, fatigue verification using the Goodman diagram, and static strength assessment, is robust and conservative for the evaluation of railway gearbox housings. It can be used as a benchmark for the design of similar components fabricated from ductile iron castings.

(5) The gearbox housing design is fully compliant with the requirements of the applicable technical specifications and is suitable for engineering application on AC locomotives. The results of my analysis provide a solid basis for the final design confirmation and for future structural optimization.

In summary, ductile iron castings used in the gearbox housing of AC locomotives demonstrate excellent structural integrity under both normal and abnormal loading conditions. The combination of the Goodman fatigue criterion for normal conditions and the static strength assessment for abnormal conditions offers a comprehensive design verification approach that ensures the safety and reliability of the component throughout its service life. The methodology and findings presented in this paper are expected to support the development and optimization of high-performance ductile iron gearbox housings for diverse railway applications.

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