Optimization Design of Dynamic Cable Configuration Considering Thermo-Mechanical Coupling Effects
Abstract
1. Introduction
2. Coupling Analysis Model of Floating Wind Turbine
2.1. OC3-Hywind Floating Wind Turbine
2.2. Marine Environmental Loading
2.3. Dynamic Cable
2.3.1. Global Configuration Design
2.3.2. Equivalent Stiffness Calculation
3. Dynamic Cable Configuration Optimization Model
3.1. Optimization Parameters and Objectives
3.2. Optimal Latin Hypercube Sampling (OLHS)
3.3. RBF Surrogate Model
3.4. NSGA-II Optimization Algorithm
- (1)
- The Optimal Latin Hypercube Sampling (OLHS) method is used to generate a sufficient number of sample points that are uniformly distributed in the design space, ensuring comprehensive coverage of the key design variable ranges. To avoid issues such as touchdown of the hanging segment or excessive arching of the buoyant segment in the static configuration of the dynamic cable, initial screening is conducted to filter out inappropriate configurations, thereby improving computational efficiency. Based on the filtered samples, extreme responses under two working conditions—maximum effective tension and maximum bending curvature—are calculated using time-domain models of the dynamic cable under different stiffness conditions.
- (2)
- Based on the sampled data, a Radial Basis Function (RBF) neural network is used to construct a surrogate model that captures the nonlinear relationships between key design variables and response indicators. The prediction accuracy of the surrogate model is evaluated through error analysis, ensuring that the error between the model predictions and validation samples is minimized, thereby enhancing the model’s accuracy and reliability.
- (3)
- Using the nonlinear relationships established by the RBF surrogate model, the NSGA-II algorithm is applied to search for the Pareto-optimal front within the design variable space, achieving multi-objective optimization of cable tension and curvature. This ensures that multiple objectives are optimized simultaneously under different design variable combinations, providing a scientific basis for evaluating and selecting design solutions. The specific steps of the optimization process are illustrated in Figure 9.
4. Discussion of Optimization Results
4.1. Effective Tension
4.2. Bending Curvature
4.3. Fatigue Life
5. Conclusions
- (1)
- The maximum deviation between the single-objective optimization results and numerical simulations is 6.15%, verifying the feasibility and accuracy of the proposed optimization model.
- (2)
- Compared to the initial design, the optimized configurations based on mechanical and thermo-mechanical coupling analyses achieved reductions in effective tension by 4.93% and 2.59%, respectively, and reductions in curvature by 7.39% and 9.42%, respectively.
- (3)
- While the total length of the dynamic cable was slightly reduced, its global dynamic response was significantly improved, and its fatigue life was markedly enhanced, with improvements of 13.04% and 20.24%, respectively, relative to the initial design. Notably, the optimization based on thermo-mechanical coupling demonstrated superior performance, offering a new perspective for dynamic cable configuration optimization.
Author Contributions
Funding
Data Availability Statement
Conflicts of Interest
References
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Name | Parameters |
---|---|
Rated power | 5 MW |
Rotor orientation, configuration | Upwind, 3 blades |
Rotor, hub diameter | 126, 3 m |
Hub height | 90 m |
Cut-in, rated, cut-out speed | 3, 11.4, 25 m/s |
Cut-in, rated rotor speed | 6.9 rpm, 12.1 rpm |
Rotor mass | 110,000 kg |
Nacelle mass | 240,000 kg |
Tower mass | 347,460 kg |
Name | Wind Speed [m/s] | Wave Height [m] | Period [s] | Current at Surface [m/s] | Turbine Status |
---|---|---|---|---|---|
Rated loads | 11.4 | 6.0 | 10.0 | 0.486 | Operating |
Extreme loads | 29.0 | 13.2 | 15.1 | 1.070 | Shutdown |
Name | Parameter | |
---|---|---|
Mechanical Analysis | Thermo-Mechanical Coupling Analysis | |
Outer diameter | 0.116 m | |
Weight in air | 25.0 kg/m | |
Axial stiffness | 345.0 MN | 233.0 MN |
Nonlinear bending stiffness | ||
Tension at conductor yield | 885 kN | |
Maximum bending curvature | 0.555 m−1 | |
Drag coefficient (normal, axial) | 1.2, 0.008 | |
Added mass coefficient (normal, axial) | 1.0, 0.0 |
Name | Parameter | |
---|---|---|
Mechanical Analysis | Thermo-Mechanical Coupling Analysis | |
Outer diameter | 0.361 m | |
Weight in air | 59.0 kg/m | |
Axial stiffness | 345.0 MN | Axial stiffness |
Nonlinear bending stiffness | Nonlinear bending stiffness | |
Drag coefficient (normal, axial) | 2.617, 0.345 | |
Added mass coefficient (normal, axial) | 1.0, 0.469 |
Analysis Methods | Maximum Effective Tension | Maximum Bending Curvature | > 0.95 |
---|---|---|---|
Error () | Error () | ||
Mechanical Analysis | 0.969 | 0.994 | Yes |
Thermo-Mechanical Coupling Analysis | 0.968 | 0.995 | Yes |
Parameter | Population Size | Number of Generations | Crossover Probability | Mutation Probability |
---|---|---|---|---|
Value | 50 | 100 | 0.9 | 0.1 |
Calculation Method | Tension Optimal Design | Curvature Optimal Design | ||
---|---|---|---|---|
Maximum Effective Tension/[kN] | Maximum Bending Curvature/[m−1] | Maximum Effective Tension/[kN] | Maximum Bending Curvature/[m−1] | |
Surrogate model | 35.68 | 0.05049 | 80.73 | 0.02596 |
Numerical simulation | 38.02 | 0.05124 | 82.24 | 0.02729 |
Error/% | 6.15% | 0.29% | 1.84% | 4.87% |
Calculation Method | Tension Optimal Design | Curvature Optimal Design | ||
---|---|---|---|---|
Maximum Effective Tension/[kN] | Maximum Bending Curvature/[m−1] | Maximum Effective Tension/[kN] | Maximum Bending Curvature/[m−1] | |
Surrogate model | 37.85 | 0.04939 | 80.98 | 0.02756 |
Numerical simulation | 40.27 | 0.04976 | 82.71 | 0.02833 |
Error/% | 6.01% | 0.07% | 2.09% | 2.72% |
Comparison of Design Schemes | Optimization Objective | Global Configuration Parameters | |||
---|---|---|---|---|---|
Maximum Effective Tension/[kN] | Hanging Segment/[m] | Buoyant Segment/[m] | Descending Segment/[m] | Total Length/[m] | |
Initial design | 54.44 | 400.0 | 80.0 | 270.0 | 750.0 |
Mechanical analysis | 51.88 | 365.5 | 100.4 | 279.8 | 745.7 |
Change rate | −4.93% | - | - | - | −0.57% |
Thermo-mechanical coupling analysis | 53.03 | 369.4 | 99.8 | 273.5 | 742.7 |
Change rate | −2.59% | - | - | - | −0.97% |
Comparison of Design Schemes | Optimization Objective | Global Configuration Parameters | |||
---|---|---|---|---|---|
Maximum Bending Curvature/[m−1] | Hanging Segment/[m] | Buoyant Segment/[m] | Descending Segment/[m] | Total Length/[m] | |
Initial design | 0.03747 | 400.0 | 80.0 | 270.0 | 750.0 |
Mechanical analysis | 0.03470 | 365.5 | 100.4 | 279.8 | 745.7 |
Change rate | −7.39% | - | - | - | −0.57% |
Thermo-mechanical coupling analysis | 0.03394 | 369.4 | 99.8 | 273.5 | 742.7 |
Change rate | −9.42% | - | - | - | −0.97% |
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Li, Y.; Zou, G.; Yang, S.; Qiao, D.; Wang, B. Optimization Design of Dynamic Cable Configuration Considering Thermo-Mechanical Coupling Effects. J. Mar. Sci. Eng. 2025, 13, 1336. https://doi.org/10.3390/jmse13071336
Li Y, Zou G, Yang S, Qiao D, Wang B. Optimization Design of Dynamic Cable Configuration Considering Thermo-Mechanical Coupling Effects. Journal of Marine Science and Engineering. 2025; 13(7):1336. https://doi.org/10.3390/jmse13071336
Chicago/Turabian StyleLi, Ying, Guanggen Zou, Suchun Yang, Dongsheng Qiao, and Bin Wang. 2025. "Optimization Design of Dynamic Cable Configuration Considering Thermo-Mechanical Coupling Effects" Journal of Marine Science and Engineering 13, no. 7: 1336. https://doi.org/10.3390/jmse13071336
APA StyleLi, Y., Zou, G., Yang, S., Qiao, D., & Wang, B. (2025). Optimization Design of Dynamic Cable Configuration Considering Thermo-Mechanical Coupling Effects. Journal of Marine Science and Engineering, 13(7), 1336. https://doi.org/10.3390/jmse13071336