Rotor
1 Parameters
Blades and actuators
Blade type
Click to open the blade database window, where you can select and customize the blade of the rotor.
The default blade is the NREL 5 MW blade
- Default value: NREL 5MW
- Unit: —
Number of blades
The number of blades of the rotor (typically 2 or 3 - max value is 30)
- Default value: 3
- Unit: —
- Range: 0 — 30
Cone angle
The angle between the rotor's plane of rotation and the direction of the blades. A positive angle cones the blades "forward", towards the wind direction.- Default value: 2.5
- Unit: $°$
- Range: -80 — 80
Pitch actuator mode
The requested pitch angles determined by the pitch controller can be applied to the blade structure in several ways.
Options:
PID controller:
Will apply a torque at the root of the blades about the pitch axis. The magnitude of this torque is determined by the pitch actuator gains.
Python script:
Use a Python script, see Python script controller
No structural pitch (default):
Causes the blade structure to remain in its initial pitch orientation. However, the aerodynamic loads on the blades are affected by the pitch angle.
This option does not have an effect if stiff blades are used.
Pitch rotational inertia
The rotational inertia (i.e angular mass) of the blade about the pitch axis. This value is relevant when tuning the pitch actuator gains.
- Default value: 28600
- Unit: $\text{kg}\cdot\text{m}^2$
- Range: 0 — 1e+08
Reference actuator torque
The reference torque that the actuator will apply at the root of the blade when pitching. This value is multiplied by the output of the PID.
- Default value: 5e+06
- Unit: $\text{N}\cdot\text{m}$
- Range: 0 — 1e+08
Proportional gain
The factor that the pitch error will be multiplied by when computing the pitch actuator torque.
- Default value: 1
- Unit: ${1} \over {\text{rad}}$
- Range: -1e+07 — 1e+08
Integral gain
The factor that the integral of the pitch error will be multiplied by when computing the pitch actuator torque.
- Default value: 2
- Unit: ${1} \over {\text{rad}\cdot\text{s}}$
- Range: -1e+07 — 1e+08
Derivative gain
The factor that the time derivative of the pitch error will be multiplied by when computing the pitch actuator torque.
- Default value: 0.25
- Unit: ${\text{s}} \over {\text{rad}}$
- Range: -1e+07 — 1e+08
Advanced
Reduction factor for structural data
This number of structural stations (location along the blade with given structural properties) are averaged into one station (i.e. a value of 2 will half the number of structural stations ).
- Default value: 1
- Unit: —
- Range: 1 — 200
Structural scale factor
This factor scales the blade stiffness up or down.
Note that if the Rotor model is set to Stiff in the Analysis parameters dialog, the structural scale factor has no influence.
- Default value: 1
- Unit: —
- Range: 0.001 — 10000
Torsional inertia factor
The torsional inertia of each finite element of the blade will be multiplied by this value.- Default value: 1
- Unit: —
- Range: 1e-99 — 1e+99
Target Cp
The target efficiency (Cp) of the rotor as a percentage of the incoming power. The maximum calue is Betz' limit: 16/27 = 59.3% Typically in the area 40-55% for a well designed blade. This value is only used for calculating rotor info, and not used in any simulation.- Default value: 49
- Unit: $\text{%}$
- Range: 1 — 59.3
Target rated rpm
The target rated rpm of the rotor. Typically in the area 10 - 14 rpm for a utility scale wind turbine (2-10 MW). This value is used for calculating rotor info, and not used in any simulation. It is also used to calculate gear box ratio if the 'Ratio scheme' is 'From generator'. It is useful when using Ashes to make a new WT design or change an existing one. Thus, a typical use case is the initial stage of a project when there are several alternatives to use for WT rating. A representative WT can then quickly be designed to be used in preliminary design of sub structr
- Default value: 12
- Unit: $\text{rpm}$
- Range: 1 — 10000
Target cut-in rpm
The target cut-in rpm is the minimum operational rpm. Cut-in rpm is where the the WT starts producing power and corresponds to the cut-in wind speed. This parameter is called 'target' as it is only used to calculate rotor info about the corresponding intervals for 1P and nP frequencies (and periods) and is not used for any simulation.
If it is set greater than the Target rated rpm parameter, then it autimatically is reduced to be equal.
This parameter is not shown if the number of blades is zero.
This parameter does not necessarily correspond to the actual generator cut-in rpm. However, the user can (and it is generally recommended to) manually set this parameter to the actual cut-in rpm of the generator.
The default value is the cut-in rpm of the NREL 5MW ref. WT.
- Default value: 6.9
- Unit: $\text{rpm}$
- Range: 0 — 10000
2 Information Pane
2.1 Required/ rated characteristics
2.1.1 Example 1
2.1.2 Example 2
- Add the new 8 MW blades to the rotor
- Go to the Generator part and modify the rated power to 8 MW
- Check the Rotor characteristics and establish the optimal TSR (in this case 8) and optimal Cp (in this case 49%)
- Insert the optimal Cp in the Target Cp parameter
- Based on the Cp, the rated power and the swept area of the rotor, Ashes will establish the required rated wind speed (for example 11.08 m.s-1)
- Based on this wind speed, the optimal TSR and the rotor radius (in this case, accounting for the hub radius and the cone and tilt angle, Ashes gives a radius of 81.26 m), establish the rated RPM (in this case 10.41)
- Enter the rated RPM in the Target rated RPM parameter
- The information pane will tell you which values can be input to the Generator rated RPM (in this case 1010) or to the Gearbox ratio (in this case 112.7) so that their characteristics match those of the rotor
- Modify the characteristics of the Generator or the Gearbox
2.1.3 Suggested time step
where
- $$\omega_R$$is the rated speed in degrees per second
- $$RPM_g$$is the rated generator speed, in rotations per minute
- $$G$$is the gearbox ratio
2.2 Wind speed table
Wind | Wind speed for which the characteristics are given |
TSR | Tip speed ratio corresponding to the rated RPM and the given wind speed |
Betz | Maximum power extractable from the wind according to Betz law (i.e. assuming that the Cp of the rotor is equal to Bezt limit, 16/27) |
Req. eff | Gives the efficiency required to produce the rated power and what percentage of the Bezt limit that corresponds to. Note that no value is given if an efficiency higher than the Betz limit is required. |
X% | Gives the power produced at that wind speed assuming the target Cp (without pitching the blades) |