Simulation Study on Methods for Reducing Dynamic Cable Curvature in Floating Wind Power Platforms
Abstract
:1. Introduction
2. Fatigue Analysis Method for Dynamic Cables
- (1)
- Firstly, it is necessary to clarify the load history experienced by dynamic cables, including external environmental factors (such as wind, waves, and currents) and the loads generated by the cable’s vibration. Since dynamic cables are flexible cables with high damping characteristics and are less prone to vortex-induced vibrations, the impact of vortex-induced vibration on the fatigue damage of dynamic cables can be neglected in the line design [22]. When dealing with sea conditions, relevant standards such as IEC 61400-3 [23] and DNV-OS-F201 [24] should be referenced. By referring to measured data, determine the operating conditions the wind turbine undergoes during its service life. Based on the joint probability distribution table of measured data, a fatigue operating conditions table can be established for different characteristic wave heights, spectral peak periods, directions, and other factors.
- (2)
- Establish a numerical model for the dynamic cable system based on the parameters of the dynamic cable. The model includes the float to which the dynamic cable is connected, the dynamic cable itself, and the necessary accessories for the dynamic cable. The time domain analysis of the dynamic cable is carried out to obtain the stress time history of the dynamic cable at different time points.
- (3)
- Fatigue life prediction for dynamic cables can utilize the stress coefficient method. The dynamic cable is a multi-layer wound structure, and each layer has different material mechanical properties, leading to varying stress coefficients. The main structures include the conductor, insulation, filling, armor wires, and sheath. Among them, the insulation, filling, and sheath are made of polyethylene polymer materials, which generally have a low elastic modulus and high Poisson’s ratio, making them less prone to fatigue failure. The focus is primarily on the fatigue damage of the metallic materials in the dynamic cable, such as the conductor and armor wires. Therefore, the stress distribution calculation for the main force-bearing structures, the conductor, and the armor wires in the dynamic cable is carried out through Formula (1) [25].
- (4)
- The stress time history response obtained above is irregular, and this irregular response can be considered to be composed of a large number of full cycles and half cycles. To further conduct a fatigue life analysis and fatigue load spectrum analysis, the widely used Rain flow counting method in the engineering field is applied to convert the load time response into several load cycles [26]. Through the statistical analysis of the Rain flow counting method, a series of data for full cycles and half cycles are obtained, preparing for the subsequent fatigue analysis.
- (5)
- The several cyclic loads obtained from the Rain flow counting method cannot be directly used for fatigue calculation. During the operation of the dynamic cable, due to the self-weight and motion of the upper floating body, the cable will experience significant tensile loads, resulting in a nonzero average stress. However, the commonly used S-N curve is obtained under conditions of zero-symmetric cyclic loads. Therefore, before using the S-N curve, it is necessary to correct the average stress. Various scholars have proposed different correction methods, such as Goodman, Gerber, Smith–Watson–Topper, etc. Among them, the Goodman correction method [12] is widely applied in engineering practice due to its simplicity. The expression for the corrected stress amplitude is as follows:
- (6)
- To calculate the fatigue damage value, it is necessary to reference the corresponding material S-N curve. The S-N curve is plotted by subjecting standard material specimens to cyclic loading at different stress amplitudes until failure under a given mean stress condition. The logarithmic form of the S-N curve formula is shown in Equation (3) [25].
- (7)
- Due to the randomness of the loads, the structure will endure a significant number of corrected stress amplitudes and corresponding stress cycle counts. To obtain the overall fatigue damage of the structure, it is necessary to accumulate damage for each stress state. Currently, the most widely used fatigue accumulation theory in the field of marine engineering is the linear fatigue accumulation method based on the Miner criterion [12]. This method neglects the influence of unordered loading caused by the randomness of the load. Specifically, by comparing the cycle count for each stress state obtained by the Rain flow counting method with the material failure cycle count determined by the S-N curve for that stress amplitude state, the fatigue damage for that stress amplitude can be obtained. The total fatigue damage is then given by :
3. Conditions and Characteristics of the Dynamic Cable
3.1. Hydrological Conditions
3.2. Cable Cross-Sectional Structure
3.3. Selection of S-N Curves
4. Results and Discussion
4.1. Calculation of Local Stress Coefficients
4.2. Results
4.3. Discussion
- (1)
- Method I: Drawing inspiration from similar measures used in flexible cables [21], add weight blocks to the section of the dynamic cable exiting the bend stiffener (as shown in Figure 14). The parameters of the weight block are listed in Table 9. The results, depicted in Figure 15, reveal a significant reduction in the curvature of the submarine cable at the exit of the bend stiffener compared to Figure 11. However, under Condition 6, the curvature at the root of the bend stiffener exceeds the allowable limit. The literature [21] suggests that this occurrence may be due to insufficient strength of the bend stiffener. It can be inferred that the addition of the weight block increases the load on the dynamic cable, causing the bend stiffener to lack the necessary strength. To ensure that the curvature of the entire cable is within the allowable range under this condition, further adjustments to the parameters of the weight block are required. Under Condition 5, the curvature in the arched area behind the dynamic cable’s float block exceeds the allowable limit. When no weight block is added, the curvature in this area is close to the allowable limit. This indicates that adding the weight block has some influence on the curvature in this area. However, the main factor causing excessive curvature in this area is the float block.
- (2)
- Method II: Changing the hanging angle of the dynamic cable’s bend stiffener (as shown in Figure 16), studying the influence of the bend stiffener hanging angle on the maximum curvature, effective tension, and von Mises stress of the dynamic cable under different conditions. Figure 17 shows the distribution of the maximum curvature along the length of the dynamic cable with a hanging angle of 45°. Compared with Figure 11, the curvature of the cable at the bend stiffener outlet is significantly reduced. Therefore, adjusting the hanging angle can effectively reduce the cable curvature. By varying the hanging angle, further research on its impact on the dynamic cable’s maximum curvature, effective tension, and von Mises stress is conducted, and the results are shown in Figure 18, Figure 19 and Figure 20. As the hanging angle of the dynamic cable’s bend stiffener increases, the curvature at the bend stiffener outlet gradually decreases under Condition 6, and at 40°, it is lower than the allowable curvature, and in this condition, the dynamic cable’s maximum curvature always occurs at the bend stiffener outlet. For Conditions 1 to 5, the curvature at the bend stiffener outlet decreases with the increase in the hanging angle. In working Conditions 1 to 5, when the hanging angle is adjusted to 15°, 20°, 30°, 30°, and 30°, the curvature of the dynamic cable bending preventer is reduced to lower than the curvature of the rest of the dynamic cable, respectively; the maximum curvature of the dynamic cable shifts from the exit of the bend stiffener to the midpoint of the arch behind the buoyancy block. Therefore, there is a maximum value for adjusting the overall maximum curvature of the cable with the hanging angle. Beyond this value, the dynamic cable’s maximum curvature shifts from the bend stiffener outlet to the midpoint of the arch after the floating block area, and the effect of adjusting the hanging angle disappears. With the increase in the hanging angle, the maximum effective tension and maximum von Mises stress for each condition gradually increase, but the increase is relatively slow. As indicated in Figure 19 and Figure 20, with the increase in the hanging angle, the maximum effective tension (i.e., the maximum pulling force experienced by the cable during operation) and the maximum von Mises stress of the dynamic cable gradually increase for each working condition, but the magnitude of the increase is relatively moderate. Therefore, applying a certain hanging angle to the dynamic cable can ensure that the cable curvature at the bend stiffener outlet meets the allowable requirements. However, the hanging angle of the bend stiffener should not be too large to avoid ineffective adjustment and unnecessary increases in cable tension and stress.
5. Conclusions
- (1)
- The fatigue analysis of the cable indicates that, with a safety factor of 10, the dynamic cable meets the design requirement of a 30-year service life in the studied marine area. The fatigue analysis was conducted under six typical operating conditions corresponding to different wave heights. It was observed that the dynamic cable experiences maximum curvature at the bend stiffener exit. To reduce this curvature, two methods were employed in this study: Method I, involving the addition of a weight block, and Method II, adjusting the hanging angle of the bend stiffener. Both methods effectively reduced the curvature at the bend stiffener exit, leading to increased effective tension and von Mises stress from the bend stiffener to the floating block section. However, the maximum effective tension and von Mises stress generated by Method II were 45.87% and 45.86% lower than those produced by Method I, respectively.
- (2)
- Given the challenges associated with changing the weight block parameters of the dynamic cable in response to different operating conditions, the method proposed in this paper involves adjusting the bend stiffener’s hanging angle to reduce the curvature of the dynamic cable. To address varying operating conditions, an automated bend stiffener capable of adjusting its hanging angle according to different scenarios can be designed based on the method proposed in this study. This bend stiffener can be an extension of the existing structure, incorporating a hanging angle adjustment mechanism and an intelligent control system. When facing different operating conditions, especially unexpected extreme conditions, the control system can regulate the hanging angle adjustment mechanism to ensure that the bend stiffener adapts its angle. This ensures that the curvature of the dynamic cable remains within the allowable range, preventing failure due to curvature exceeding permissible limits. Designing such a bend stiffener with automatic hanging angle adjustment presents several challenges. Firstly, current bend stiffener designs are still limited to traditional fixed types, lacking designs for hanging angle adjustment mechanisms and control systems. Secondly, addressing the energy supply for this bend stiffener is crucial. It can be powered by the floating wind turbine’s self-generation capabilities, or an integrated wave energy harvesting device can provide the necessary power. Finally, the response speed of the bend stiffener in adjusting the hanging angle needs to be considered when facing different operating conditions.
Author Contributions
Funding
Institutional Review Board Statement
Informed Consent Statement
Data Availability Statement
Conflicts of Interest
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Hs(m)\ Direction | N | NE | E | SE | S | SW | W | NW | Subtotal |
---|---|---|---|---|---|---|---|---|---|
0.0–0.5 | 2.49 | 6.10 | 13.60 | 4.84 | 4.04 | 6.78 | 1.78 | 1.20 | 40.83 |
0.5–1.0 | 4.28 | 8.98 | 10.33 | 0.83 | 1.13 | 11.32 | 0.80 | 0.10 | 37.79 |
1.0–1.5 | 5.05 | 2.31 | 1.07 | 0.14 | 0.08 | 5.06 | 0.37 | 0.05 | 14.14 |
1.5–2.0 | 3.46 | 0.42 | 0.07 | 0 | 0 | 0.49 | 0.06 | 0 | 4.50 |
2.0–2.5 | 1.23 | 0.10 | 0.03 | 0 | 0 | 0 | 0.01 | 0.046 | 1.43 |
2.5–3.0 | 0.51 | 0.01 | 0.02 | 0 | 0 | 0 | 0 | 0.046 | 0.59 |
3.0–3.5 | 0.29 | 0.03 | 0 | 0 | 0 | 0 | 0 | 0.023 | 0.34 |
3.5–4.0 | 0.18 | 0.01 | 0 | 0 | 0 | 0 | 0 | 0 | 0.19 |
4.0–4.5 | 0.07 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0.07 |
4.5–5.0 | 0.02 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0.02 |
5.0–5.5 | 0.05 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0.05 |
5.5–6.0 | 0.03 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0.03 |
>6.0 | 0.02 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0.02 |
Subtotal | 17.72 | 17.97 | 25.13 | 5.81 | 5.25 | 23.65 | 3.01 | 1.46 | 100 |
Maximum Value | 6.15 | 3.59 | 2.71 | 1.46 | 1.18 | 1.82 | 2.12 | 3.16 |
Operating Condition | Wave Height (m) | Wave Period (s) | Wave Direction | Wind Speed (m/s) | Wind Direction |
---|---|---|---|---|---|
100-Year Return Period Wave under 100-Year Return Period High Tide Level | 11.8 | 9.4 | NW | 40 | NW |
100-Year Return Period Wave under 100-Year Return Period Low Tide Level | 10.62 | 9.1 | NW | 40 | NW |
Multi-Year Average Wave | 1.0 | 3 | NE | 6 | NE |
Type | One-Year Return Period Current Velocity (m/s) | Ten-Year Return Period Current Velocity (m/s) | Fifty-Year Return Period Current Velocity (m/s) |
---|---|---|---|
Surface Current | 1.0 | 2.0 | 2.5 |
Midlayer Current | 0.8 | 1.6 | 2.0 |
Near-Bottom Current | 0.4 | 0.7 | 1.0 |
Parameters | Values | Parameters | Values | ||
---|---|---|---|---|---|
X | Y | Z | |||
Length (m) | 103 | Centre of gravity (m) | 2.53 | 0 | −1.97 |
Width (m) | 15.95 | ||||
Molded depth (m) | 13.32 | Moment of inertia tensor (t·m2) | 254.9 × 103 | 5.980 × 106 | 5.980 × 106 |
Platform draft (m) | 6.66 | ||||
Mass (t) | 9017.95 |
Vertices | X (m) | Y (m) | Z (m) |
---|---|---|---|
1 | 53 | 0 | 6.66 |
2 | 35 | 8 | 6.66 |
3 | −50 | 8 | 6.66 |
4 | −50 | −8 | 6.66 |
5 | 35 | −8 | 6.66 |
6 | 40 | 0 | −6.66 |
7 | 35 | 8 | −6.66 |
8 | −50 | 8 | −6.66 |
9 | −50 | −8 | −6.66 |
10 | 35 | −8 | −6.66 |
Parameters | Values | Parameters | Values |
---|---|---|---|
Outer Diameter (mm) | 147.3 | Torsional Stiffness (kN·m2) | 209.8 |
Dry Weight (kg/m) | 45.90 (in air) | Minimum Bending Radius (m) | 1.80 |
Wet Weight (kg/m) | 28.43 (underwater) | Minimum Breaking Force (kN) | 1351.5 |
Axial Stiffness (MN) | 631.7 | Maximum Operating Force (kN) | 330.5 |
Bending Stiffness (kN·m2) | 10.3 | Design Lifetime (years) | 30 |
Structure | log(a) | m |
---|---|---|
Armoring Steel Wires | 14.917 | 4 |
Copper Conductors | 12.75 | 3.75 |
Working Conditions | Wave Height (m) | Wave Direction |
---|---|---|
Condition 1 | 2 | N |
Condition 2 | 3 | N |
Condition 3 | 4 | N |
Condition 4 | 5 | N |
Condition 5 | 6 | N |
Condition 6 | 11.8 | NW |
Weight Block | Weight/t | Position/m |
---|---|---|
Weight Block 1 | 0.3 | 6 |
Weight Block 2 | 0.3 | 8 |
Weight Block 3 | 0.3 | 10 |
Weight Block 4 | 0.3 | 12 |
Weight Block 5 | 0.3 | 14 |
Weight Block 6 | 0.3 | 16 |
Weight Block 7 | 0.3 | 18 |
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Guo, Z.; Zhao, X.; Ma, Q.; Li, J.; Wu, Z. Simulation Study on Methods for Reducing Dynamic Cable Curvature in Floating Wind Power Platforms. J. Mar. Sci. Eng. 2024, 12, 334. https://doi.org/10.3390/jmse12020334
Guo Z, Zhao X, Ma Q, Li J, Wu Z. Simulation Study on Methods for Reducing Dynamic Cable Curvature in Floating Wind Power Platforms. Journal of Marine Science and Engineering. 2024; 12(2):334. https://doi.org/10.3390/jmse12020334
Chicago/Turabian StyleGuo, Zhitao, Xudong Zhao, Qingfen Ma, Jingru Li, and Zhongye Wu. 2024. "Simulation Study on Methods for Reducing Dynamic Cable Curvature in Floating Wind Power Platforms" Journal of Marine Science and Engineering 12, no. 2: 334. https://doi.org/10.3390/jmse12020334
APA StyleGuo, Z., Zhao, X., Ma, Q., Li, J., & Wu, Z. (2024). Simulation Study on Methods for Reducing Dynamic Cable Curvature in Floating Wind Power Platforms. Journal of Marine Science and Engineering, 12(2), 334. https://doi.org/10.3390/jmse12020334