This chapter presents the design of a monopile OWSS. It is choses to design for a water depth of 28 m since this is the average water depth at the site.

## 4.1. Initial dimensioning

### 4.1.1. Dimensions of Monopile

The design starts with an initial estimate of the geometry. The monopile diameter is chosen such that the first natural frequency of the structure is within the allowable soft –stiff range. As presented in Section 3, this range is between 0,22 to 0,31 Hz so is aimed for a first natural period near 0,26 Hz. Using a stick model and formulas (1) and (2), a first estimate of the diameter is obtained. That was 6.5 m with the wall thickness set to 80 mm (D/t ≈ 80-90) and f=0.258.

The next step to improve the design is to use readily available calculations tools available (spreadsheets, ANSYS etc). Using those tools it is possible to take into account the change in diameter and thickness along the structure, the concentrated weights, the RNA, the soil properties etc. The results of such analysis show that we can use a monopile with D=6.2, and TP and tower as described in following pages. Then, the natural frequencies of the structure are within the limits set. The first natural period is 0.266 Hz (soft-stiff range) and the second natural period is 1.062 Hz (stiff-stiff range).

** Table 18: Modal frequencies of monopile support structure**

f1 | 0.266 Hz | f6 | 6.348 Hz | |

f2 | 1.062 Hz | f7 | 9.680 Hz | |

f3 | 3.198 Hz | f8 | 11.287 Hz | |

f4 | 5.916 Hz | f9 | 11.368 Hz | |

f5 | 6.008 Hz | f10 | 13.349 Hz |

Since the currently available hammers for driving piles are limited to diameters up to 5.5 m, a conical part is used to decrease the top diameter of the monopile to 5.5 m. The conical part extents from el. – 5 m to el. -7 m. For more dimensions, please refer to Drawing 1, Appendix 2.

The top of the monopile is at el. +4.75 m for easy installation of the transition piece. The initial thickness of the monopile is set at t = 80 mm (D/t = 80). The required thickness is determined later when performing the necessary ULS checks.

### 4.1.2. Dimensions of Transition Piece (TP)

The transition piece (TP) extents from just below the LSWL to the interface level. A grout connection connects the TP to the monopile. The characteristics of the connection influence our decision for the initial dimensions of the TP. The following are considered:

- Grout length = 1,5· Dpile + grout skirt at bottom of TP = 1,5 · 5,5 + 0.5 = 8,75 m
- Grout thickness = Min thickness + allowance for alignment (0.5°) + allowance for wall thickness variation of TP = 150 mm +230 mm + 10 mm = 390 mm
- Transition piece diameter = Dpile + grout thickness + 2 * TP wall thickness = 5,5 + 0,39 + 0,14 ≈
**6 m**

Given the above considerations, the TP diameter at the location of the connection should be 6 m. Since the bottom diameter of the tower is also 6 m we chose to keep the same diameter for the full height of the TP.

**4.1.3. Dimensions of Tower**

For the initial geometry for the tower information is used from other wind farms (Lars Bulow, 2008).

- @ Tower BASE: D=6 m, t=35 mm
- @ Tower TOP: D=4,5 m, t=20 mm
- Tower Mass =π*5.25*0.026*70*7,850 = 235 tonnes

## 4.2. Loads

The loads calculated in Section 2 are summarized below

**Aerodynamic**

Thrust Force

D_{ax}= 780 kN at +85 (from MSL)

Drag force on Tower

50-year wind @+45m – 28.8 m/s —> Force 183 kN acting at 45 m above MSL.

5-year wind @+45m – 26.5 m/s —> Force 155 kN acting at 45 m above MSL.

**Hydrodynamic**

Description | Hydrodynamic Force at seabed level [kN] | Hydrodynamic Moment at seabed level [MNm] |

50-year water level, 5-year wave, 5-year current | 4650 | 103 |

50-year water level, 50-year wave, 5-year current | 5450 | 122 |

50-year water level, 5-year wave, 50-year current | 4800 | 106 |

**Weight**

Below is a breakdown of the weight of monopile

Mass (t) | Weight (kN) | |

Nacelle | 290 | 2900 |

Rotor | 120 | 1200 |

Tower (π*5.25*0,0275*7,850 = 3.56 t/m ) | 250 | 2500 |

Total at interface level | 6600 kN | |

Transition piece (π∙6,0∙0,08∙19∙7,850) | 200 | 2000 |

Pile above seabed (π∙6,3∙0,08∙32∙7,850) | 397 | 3970 |

Buoyancy (π∙6,0∙0,08∙19∙7,850) | -50 | -500 |

Total Vertical action at seabed level | 12070 kN≈12.07 MN |

**Table 20:**Weight breakdown for monopile OWSS

Notes:

The weight of all other parts of a wind turbine is neglected (secondary steel, platform, fittings, etc.)

The variable weight load from people, equipment, boats etc. is also neglected.

## 4.3. Load Combinations

### 4.3.1. **Combining the environmental loads**

We prepared load combinations 1,2 and 3 as descript in section 4.1. We choose not to calculate the combination 4 and 5 and instead add the weight of the 50-year ice on the weight of the structure. This results in an increase of vertical load (at foundation level) of less than 5% and since we already have omitted the weight on secondary steel etc, we do not expect that this addition will lead to an overdesign that will influence the overall design of the structure.

**Combining loads for the ULS**

Next, we calculate the design load effects for selected sections of the structure. We choose to do this for section A, B, C, D as descript below and shown in (Figure 8):

- Top of the tower (+ 83 m)
- Bottom of the tower (+ 15 m)
- Transition piece at elevation +5 m (just above the end of the monopile)
- Pile at seabed level (- 28 m)

To find the design load effect we combine the load effects from environment load, from permanent load and from variable loads. These is done using two load factor sets (set A and set B) as descript in section 4.1. When forming those sets, for the environmental load effects we use the values that come from the most sever environmental load combination (i.e. 1, 2, 3)

## 4.4. Strength checks

The structure is checked to ensure that the yield stress is not exceeded and that no global buckling occurs. The equations and criteria of the check are presented in section 4.3. The results are shown in Tables 21 and 22

The applied material factors are:

– γm = 1.1 ULS stress checks (as given in C103, Sec.7, DNV for tabular members)

– γm = 1.2 ULS global buckling check (as given in C104, Sec.7, DNV for tabular members)

Tables 21 and 22 present the main loads and strength checks at sections A,B,C and D. More specifically:

- The load effects (M, V, N) for each load category
- The total load effects using load factor set (a)
- The total load effects using load factor set (b)
- The yield stress check
- The buckling check

Combined design load effect at the ULS due to loading from various types of loads

Load type | Load factor Set (a) | Load factor Set (b) | Section A | el: + 83 | Section B | el: + 15 | ||

M [MNm] | N [MN] | M [MNm] | V [MN] | N [MN] | ||||

Environmental (highest load effect from the 3 combinations) | 1.00 | 1.35 | 3.120 | 0.78 | 0.550 | 60.090 | 0.963 | 0.550 |

Permanent | 1.25 | 1.00 | 0.000 | 0.00 | 4.100 | 0.000 | 0.000 | 6.592 |

Variable | 1.25 | 1.00 | 0.000 | 0.00 | 0.000 | 0.000 | 0.000 | 0.000 |

Total load using load factor set a | 3.120 | 0.78 | 5.675 | 60.09 | 0.963 | 8.790 | ||

Total load using load factor set b | 4.212 | 1.05 | 4.843 | 81.12 | 1.300 | 7.335 | ||

Wall thickness of section | [m] | 0.020 | 0.035 | |||||

Section diameter | [m] | 4.50 | 6.00 | |||||

Section Area | [m²] | 15.90 | 28.27 | |||||

Moment of Inertia | [m4] | 0.72 | 2.97 | |||||

Design stress (set a) | [MPa] | 10.17 | 61.03 | |||||

Design stress (set b) | [MPa] | 13.55 | 82.23 | |||||

σ yield, d (factored) | 304.5 | 304.55 | ||||||

Nkt,d | 23.41 | 97.11 | ||||||

Np | 4843 | 8610 | ||||||

Mp | 96.87 | 301.37 | ||||||

λ | 15.08 | 9.87 | ||||||

Φ | 115.8 | 50.28 | ||||||

Κ | 0.004 | 0.0100 | ||||||

Buckling check | 0.402 | 0.4010 |

Table 22: Load effects and strength checks for selected sections (con’t)

Combined design load effect at the ULS due to loading from various types of loads | ||||||||

Load type | Load factor Set (a) | Load factor Set (b) | Section C | el.: + 5 | Section D | el.: -28 | ||

M [MNm] | V [MN] | N [MN] | M [MNm] | V [MN] | N [MN] | |||

Environmental (highest load effect from the 3 combinations) | 1.00 | 1.35 | 69.720 | 0.963 | 0.550 | 221.455 | 6.385 | 0.550 |

Permanent | 1.25 | 1.00 | 0.000 | 0.000 | 7.622 | 0.000 | 0.000 | 12.08 |

Variable | 1.25 | 1.00 | 0.000 | 0.000 | 0.000 | 0.000 | 0.000 | 0.000 |

Total load using load factor set a | 69.720 | 0.963 | 10.078 | 221.455 | 6.385 | 15.658 | ||

Total load using load factor set b | 94.122 | 1.300 | 8.365 | 298.964 | 8.620 | 12.829 | ||

Wall thickness of section | [m] | 0.070 | 0.080 | |||||

Section diameter | [m] | 6.00 | 6.20 | |||||

Section Area | [m²] | 28.27 | 30.19 | |||||

Moment of Inertia | [m4] | 5.94 | 7.49 | |||||

Design stress (set a) | [MPa] | 35.58 | 92.21 | |||||

Design stress (set b) | [MPa] | 47.85 | 124.21 | |||||

σ yield, d (factored) | 295.45 | 286.36 | ||||||

Nkt,d | 194.22 | 244.92 | ||||||

Np | 8353.78 | 8645 | ||||||

Mp | 584.76 | 691.6 | ||||||

Λ | 6.87 | 6.2 | ||||||

Φ | 24.85 | 20.5 | ||||||

Κ | 0.0205 | 0.024 | ||||||

Buckling check | 0.2780 | 0.492 |