Structural loads at pitch and yaw actuator
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 Joined: Tue Apr 20, 2010 1:34 am
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Structural loads at pitch and yaw actuator
Hello everyone,
to validate the mass parameters and the response of the structural model of my wind turbine I do run tests without aerodynamic forces.
There are two test cases where I got some problems to get the expected results. In the first test all DOF’s are switched off.
I do control the pitch angle using a BLADEDDLL. The output of the blade 1 pitch angle (PtchPMzc1) is exactly like the demanded angle of the controller.
What I do wonder is that the blade 1 pitching moment at the blade root (RootMzb1) remains zero.
Here I would have expected to measure a drive torque in response to the moment of inertia about the pitch axis.
The demanded pitch angle changes quadratically in respect to the simulation time. The acceleration in the pitch joint should stay constant.
Does the FASTModel consider the internal loads if the turbine blade will be accelerate about the pitch axis?
In the second test I want to get the response of the yaw actuator (YawMom) if the demanded yaw rate and the correlated yaw angle are controlled.
In the FAST user guide I found that it is possible to get the response due the moment of inertia of the nacelle and rotor about the yaw axis by setting YawDOF to True.
I now got the problem if the YawDOF has been set to False I will get the demanded yaw angle but got a zero YawMom. If I set the YawDOF to True the yaw angle and YawMom remains zero.
I found in the source file BladedDLLInterface.f90 that in the UserYawCont() routine a valid YawPosCom will be generated from the provided YawRate.
Any help is much appreciated!
Best regards,
Matthias
to validate the mass parameters and the response of the structural model of my wind turbine I do run tests without aerodynamic forces.
There are two test cases where I got some problems to get the expected results. In the first test all DOF’s are switched off.
I do control the pitch angle using a BLADEDDLL. The output of the blade 1 pitch angle (PtchPMzc1) is exactly like the demanded angle of the controller.
What I do wonder is that the blade 1 pitching moment at the blade root (RootMzb1) remains zero.
Here I would have expected to measure a drive torque in response to the moment of inertia about the pitch axis.
The demanded pitch angle changes quadratically in respect to the simulation time. The acceleration in the pitch joint should stay constant.
Does the FASTModel consider the internal loads if the turbine blade will be accelerate about the pitch axis?
In the second test I want to get the response of the yaw actuator (YawMom) if the demanded yaw rate and the correlated yaw angle are controlled.
In the FAST user guide I found that it is possible to get the response due the moment of inertia of the nacelle and rotor about the yaw axis by setting YawDOF to True.
I now got the problem if the YawDOF has been set to False I will get the demanded yaw angle but got a zero YawMom. If I set the YawDOF to True the yaw angle and YawMom remains zero.
I found in the source file BladedDLLInterface.f90 that in the UserYawCont() routine a valid YawPosCom will be generated from the provided YawRate.
Any help is much appreciated!
Best regards,
Matthias

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Re: Structural loads at pitch and yaw actuator
Dear Matthias,
The current version of FAST has no pitch dynamics. That is, the pitchangle command from the controller is simply used in FAST to orient the blade (instantaneously) with no dynamics. Certainly this misses some physics by decoupling the pitch motions from the rest of the system equations of motion. For example, when the bladepitch angles change because of commands from the pitch controller, because there is no bladepitch DOF, there are no associated pitch rates or accelerations computed by FAST and the inertia, Coriolis, and other potential loads from the pitch motion will not be included in the output loads at the blade root. The magnitude of these ignored terms will depend on how fast the blades pitch and on the degree to which the blades deflect. With no pitch dynamics, no aerodynamics, and no blade deflection (because you've disabled these features), the pitching moment will be zero.
With regards to the nacelle yaw control in FAST, if the yaw DOF is disabled, then the commanded yaw angle and rate will be the actual yaw angle and yaw rate used internally by FAST. In this case, FAST will not compute the correlated yaw acceleration, but assume that it is zero. With a zerovalued yaw acceleration and a perfectly balanced rotor with no aerodynamic loads, the yaw moment would be zero. If the yaw DOF is enabled in FAST, then the commanded yaw angle and rate, YawPosCom and YawRateCom, become the neutral yaw angle, YawNeut, and neutral yaw rate, YawRateNeut, in FAST's builtin secondorder actuator model defined by inputs YawSpr and YawDamp. If YawSpr and YawDamp are specified as zero in FAST's primary input file, then the yaw inertia loads would balance with the yaw excitation loads, such that the yaw moment would also be zero (and if the yaw excitation loads are zero, the yaw angle would also be zero). Are YawSpr and YawDamp zerovalued in your model?
Best regards,
The current version of FAST has no pitch dynamics. That is, the pitchangle command from the controller is simply used in FAST to orient the blade (instantaneously) with no dynamics. Certainly this misses some physics by decoupling the pitch motions from the rest of the system equations of motion. For example, when the bladepitch angles change because of commands from the pitch controller, because there is no bladepitch DOF, there are no associated pitch rates or accelerations computed by FAST and the inertia, Coriolis, and other potential loads from the pitch motion will not be included in the output loads at the blade root. The magnitude of these ignored terms will depend on how fast the blades pitch and on the degree to which the blades deflect. With no pitch dynamics, no aerodynamics, and no blade deflection (because you've disabled these features), the pitching moment will be zero.
With regards to the nacelle yaw control in FAST, if the yaw DOF is disabled, then the commanded yaw angle and rate will be the actual yaw angle and yaw rate used internally by FAST. In this case, FAST will not compute the correlated yaw acceleration, but assume that it is zero. With a zerovalued yaw acceleration and a perfectly balanced rotor with no aerodynamic loads, the yaw moment would be zero. If the yaw DOF is enabled in FAST, then the commanded yaw angle and rate, YawPosCom and YawRateCom, become the neutral yaw angle, YawNeut, and neutral yaw rate, YawRateNeut, in FAST's builtin secondorder actuator model defined by inputs YawSpr and YawDamp. If YawSpr and YawDamp are specified as zero in FAST's primary input file, then the yaw inertia loads would balance with the yaw excitation loads, such that the yaw moment would also be zero (and if the yaw excitation loads are zero, the yaw angle would also be zero). Are YawSpr and YawDamp zerovalued in your model?
Best regards,
Jason Jonkman, Ph.D.
Senior Engineer  National Wind Technology Center (NWTC)
National Renewable Energy Laboratory (NREL)
15013 Denver West Parkway  Golden, CO 80401
+1 (303) 384 – 7026  Fax: +1 (303) 384 – 6901
nwtc.nrel.gov
Senior Engineer  National Wind Technology Center (NWTC)
National Renewable Energy Laboratory (NREL)
15013 Denver West Parkway  Golden, CO 80401
+1 (303) 384 – 7026  Fax: +1 (303) 384 – 6901
nwtc.nrel.gov

 Posts: 14
 Joined: Tue Apr 20, 2010 1:34 am
 Organization: Institut für Mechatronik Chemnitz
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Re: Structural loads at pitch and yaw actuator
Dear Jason,
indeed YawSpr and YawDamp had been zerovalued in my model. I didn’t notice that the yaw angle and yaw rate
constraints are controlled through a torque which will supplied by your actuator model.
Now I chosen for YawSpr = 1e9 and for YawDamp = 1e5. The demanded yaw angle is
PI/7200*TIME^2 and the correlated yaw rate is PI/3600*TIME. The figure 1 shows the response for the yaw angle (YawPzn).
Unfortunately the YawMom doesn’t came out as expected.
Because the yaw acceleration has been constant the YawMom should be constant as well.
I tried all ready different values for the YawDamp value but without any success.
It still seems to be a free vibration of the actuator model.
Any help is much appreciated!
Best regards,
Matthias
indeed YawSpr and YawDamp had been zerovalued in my model. I didn’t notice that the yaw angle and yaw rate
constraints are controlled through a torque which will supplied by your actuator model.
Now I chosen for YawSpr = 1e9 and for YawDamp = 1e5. The demanded yaw angle is
PI/7200*TIME^2 and the correlated yaw rate is PI/3600*TIME. The figure 1 shows the response for the yaw angle (YawPzn).
Unfortunately the YawMom doesn’t came out as expected.
Because the yaw acceleration has been constant the YawMom should be constant as well.
I tried all ready different values for the YawDamp value but without any success.
It still seems to be a free vibration of the actuator model.
Any help is much appreciated!
Best regards,
Matthias

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 Location: Boulder, CO
 Contact:
Re: Structural loads at pitch and yaw actuator
Dear Matthias,
Can you also plot YawVxn and YawAxn (i.e., the resulting yaw rate and yaw acceleration, which I suspect are different than the commanded yaw rate and acceleration)?
I suspect you've chosen values of YawSpr and YawDamp that are far too low to get the yaw motion to exactly track the desired yaw acceleration. The FAST User's Guide recommends that you set YawSpr = YawIner•ωn^2 and YawDamp = 2•ζ•YawIner•ωn, where YawIner is the nominal inertia of the nacelle and rotor about the yaw axis in kg·m^2, ωn is the desired yaw actuator natural frequency in rad/sec, and ζ is the desired yaw actuator damping ratio in fraction of critical. The natural frequency I see in your plot of YawMom is around 1.87 Hz, or ωn = 11.75 rad/s. From your values of YawSpr and YawDamp and the equations above, this must mean that YawIner = 7.24E+6 kg·m^2 and ζ = 5.87 E4 in your model. ζ should be set between 0.6 and 0.7 for optimal tracking of a desired yaw motion (increasing YawSpr may also help).
Best regards,
Can you also plot YawVxn and YawAxn (i.e., the resulting yaw rate and yaw acceleration, which I suspect are different than the commanded yaw rate and acceleration)?
I suspect you've chosen values of YawSpr and YawDamp that are far too low to get the yaw motion to exactly track the desired yaw acceleration. The FAST User's Guide recommends that you set YawSpr = YawIner•ωn^2 and YawDamp = 2•ζ•YawIner•ωn, where YawIner is the nominal inertia of the nacelle and rotor about the yaw axis in kg·m^2, ωn is the desired yaw actuator natural frequency in rad/sec, and ζ is the desired yaw actuator damping ratio in fraction of critical. The natural frequency I see in your plot of YawMom is around 1.87 Hz, or ωn = 11.75 rad/s. From your values of YawSpr and YawDamp and the equations above, this must mean that YawIner = 7.24E+6 kg·m^2 and ζ = 5.87 E4 in your model. ζ should be set between 0.6 and 0.7 for optimal tracking of a desired yaw motion (increasing YawSpr may also help).
Best regards,
Jason Jonkman, Ph.D.
Senior Engineer  National Wind Technology Center (NWTC)
National Renewable Energy Laboratory (NREL)
15013 Denver West Parkway  Golden, CO 80401
+1 (303) 384 – 7026  Fax: +1 (303) 384 – 6901
nwtc.nrel.gov
Senior Engineer  National Wind Technology Center (NWTC)
National Renewable Energy Laboratory (NREL)
15013 Denver West Parkway  Golden, CO 80401
+1 (303) 384 – 7026  Fax: +1 (303) 384 – 6901
nwtc.nrel.gov

 Posts: 14
 Joined: Tue Apr 20, 2010 1:34 am
 Organization: Institut für Mechatronik Chemnitz
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Re: Structural loads at pitch and yaw actuator
Hello Jason,
thanks for your response and the recommends in terms of YawSpr and YawDamp value.
Unfortunately the output result for YawMom is still not as expected.
Are the values YawVxn and YawAxn standard outputs of FAST?
If I do run a FAST job with this output channels FAST terminates with an error message.
Any help is much appreciated!
Best regards,
Matthias
thanks for your response and the recommends in terms of YawSpr and YawDamp value.
Unfortunately the output result for YawMom is still not as expected.
Are the values YawVxn and YawAxn standard outputs of FAST?
If I do run a FAST job with this output channels FAST terminates with an error message.
Any help is much appreciated!
Best regards,
Matthias

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 Location: Boulder, CO
 Contact:
Re: Structural loads at pitch and yaw actuator
Dear Matthias,
Sorry. I meant to say YawVzn and YawAzn, which are the nacelleyaw rate and acceleration.
Best regards,
Sorry. I meant to say YawVzn and YawAzn, which are the nacelleyaw rate and acceleration.
Best regards,
Jason Jonkman, Ph.D.
Senior Engineer  National Wind Technology Center (NWTC)
National Renewable Energy Laboratory (NREL)
15013 Denver West Parkway  Golden, CO 80401
+1 (303) 384 – 7026  Fax: +1 (303) 384 – 6901
nwtc.nrel.gov
Senior Engineer  National Wind Technology Center (NWTC)
National Renewable Energy Laboratory (NREL)
15013 Denver West Parkway  Golden, CO 80401
+1 (303) 384 – 7026  Fax: +1 (303) 384 – 6901
nwtc.nrel.gov

 Posts: 14
 Joined: Tue Apr 20, 2010 1:34 am
 Organization: Institut für Mechatronik Chemnitz
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 Contact:
Re: Structural loads at pitch and yaw actuator
Hello,
I now use a double precision FAST where I receive the expected results.
I increased the YawDamp value up to 1e9. The yaw acceleration (YawAzn)
and the YawMom now stays constant.
To me it seems to be as a problem of the solver stability.
What I still wonder is, that I do get NaN as output if I choose the YawDamp value above 1e10.
Kind regards,
Matthias
I now use a double precision FAST where I receive the expected results.
I increased the YawDamp value up to 1e9. The yaw acceleration (YawAzn)
and the YawMom now stays constant.
To me it seems to be as a problem of the solver stability.
What I still wonder is, that I do get NaN as output if I choose the YawDamp value above 1e10.
Kind regards,
Matthias

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Re: Structural loads at pitch and yaw actuator
Dear Matthias,
I'm glad you got the desired yaw response.
I've never needed to use double precision in FAST to get a desired output. Are you saying that you needed double precision with YawDamp = 1e9? What damping ratio, ζ, are you gettingbased on the equations belowwith YawDamp = 1e9 and YawDamp = 1e10? As I said before, you should ensure ζ is between 0.6 and 0.7 for optimal tracking of a desired yaw motion. Much higher damping may lead to a numerical instability in the model. I'm not sure where you are seeing NaN as output, but this is often the first sign of a numerical instability in the model.
Best regards,
I'm glad you got the desired yaw response.
I've never needed to use double precision in FAST to get a desired output. Are you saying that you needed double precision with YawDamp = 1e9? What damping ratio, ζ, are you gettingbased on the equations belowwith YawDamp = 1e9 and YawDamp = 1e10? As I said before, you should ensure ζ is between 0.6 and 0.7 for optimal tracking of a desired yaw motion. Much higher damping may lead to a numerical instability in the model. I'm not sure where you are seeing NaN as output, but this is often the first sign of a numerical instability in the model.
Best regards,
Jason Jonkman, Ph.D.
Senior Engineer  National Wind Technology Center (NWTC)
National Renewable Energy Laboratory (NREL)
15013 Denver West Parkway  Golden, CO 80401
+1 (303) 384 – 7026  Fax: +1 (303) 384 – 6901
nwtc.nrel.gov
Senior Engineer  National Wind Technology Center (NWTC)
National Renewable Energy Laboratory (NREL)
15013 Denver West Parkway  Golden, CO 80401
+1 (303) 384 – 7026  Fax: +1 (303) 384 – 6901
nwtc.nrel.gov

 Posts: 35
 Joined: Tue Jan 10, 2017 5:37 am
 Organization: Hochschule Aalen
 Location: Germany  Baden Wuerttemberg
Modelling pitch actuator; Re: Structural loads at pitch and yaw actuator
Dear Jason,
I'm trying to add a mechanical pitch actuator model to FAST as a bladedstyle DLL. For modelling the blade bearing I need several forces and moments at the blade root. Now I'm trying to use the userdefined records (120129) and other records of the DLLinterface to get the forces and moments from ElastoDyn to my bladedstyle DLL.
Is it possible to define the records with this variables in the Bladed Interface so I have access (for reading) in my bladedstyle DLL?
Thank you in anticipation for your help.
Best regards
René
I'm trying to add a mechanical pitch actuator model to FAST as a bladedstyle DLL. For modelling the blade bearing I need several forces and moments at the blade root. Now I'm trying to use the userdefined records (120129) and other records of the DLLinterface to get the forces and moments from ElastoDyn to my bladedstyle DLL.
Is it possible to define the records with this variables in the Bladed Interface so I have access (for reading) in my bladedstyle DLL?
Thank you in anticipation for your help.
Best regards
René
Last edited by Rene.Mebus on Sat Apr 22, 2017 3:27 am, edited 1 time in total.

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Re: Structural loads at pitch and yaw actuator
Dear René,
Yes, it is possible, and it sounds like you're on the right track to implementing it. I suggest that you look at how the DLL currently gets the blade root outofplane bending moments (records 3032) and blade root inplane bending moments (records 6971) and mimic the approach for the other load components you need.
Best regards,
Yes, it is possible, and it sounds like you're on the right track to implementing it. I suggest that you look at how the DLL currently gets the blade root outofplane bending moments (records 3032) and blade root inplane bending moments (records 6971) and mimic the approach for the other load components you need.
Best regards,
Jason Jonkman, Ph.D.
Senior Engineer  National Wind Technology Center (NWTC)
National Renewable Energy Laboratory (NREL)
15013 Denver West Parkway  Golden, CO 80401
+1 (303) 384 – 7026  Fax: +1 (303) 384 – 6901
nwtc.nrel.gov
Senior Engineer  National Wind Technology Center (NWTC)
National Renewable Energy Laboratory (NREL)
15013 Denver West Parkway  Golden, CO 80401
+1 (303) 384 – 7026  Fax: +1 (303) 384 – 6901
nwtc.nrel.gov

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 Joined: Fri Jan 04, 2019 1:08 am
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 Location: Spain
Re: Structural loads at pitch and yaw actuator
Dear Jason,
I am trying to estimate the values of YawSpr and Yaw Damp, when I came across with this post where these variables a defined as;
YawSpr = YawIner•ωn^2
YawDamp = 2•ζ•YawIner•ωn
I was doing some test trying to get the same values as are shown on NREL 5MW example and DOWEC 6MW PREDESIGN. According to both examples I have some differences between my calculations and the values posted. I would like to know the reason (I think the differences are too high to be caused by the decimals).
In case NREL 5MW example:
YawSpr = YawIner•ωn^2=2,607,890*(3*2*pi())^2=926,598,334 and the example is 9,028,320,000
YawDamp = 2•ζ•YawIner•ωn=2*0.2*2,607,890*(3*2*pi())= 19,663,027 and in the example is 19,160,000 N•m/(rad/s).
The example I am referring is NREL 5MW: https://www.nrel.gov/docs/fy09osti/38060.pdf, Section 4; "4 Hub and Nacelle Properties"
Besides I am having some issues too, with the calculation of the YawInertia to obtain the same values as in NREL 5MW example. From the information I read, I assume that the YawIner is calculated with the Nacelle (NacMass,NacCMxn) and with the rotor (Rotormass,OverHang). Am I missing anything? Is there any old post where I can see the development?
Thank you a lot for your time.
Kind regards
I am trying to estimate the values of YawSpr and Yaw Damp, when I came across with this post where these variables a defined as;
YawSpr = YawIner•ωn^2
YawDamp = 2•ζ•YawIner•ωn
I was doing some test trying to get the same values as are shown on NREL 5MW example and DOWEC 6MW PREDESIGN. According to both examples I have some differences between my calculations and the values posted. I would like to know the reason (I think the differences are too high to be caused by the decimals).
In case NREL 5MW example:
YawSpr = YawIner•ωn^2=2,607,890*(3*2*pi())^2=926,598,334 and the example is 9,028,320,000
YawDamp = 2•ζ•YawIner•ωn=2*0.2*2,607,890*(3*2*pi())= 19,663,027 and in the example is 19,160,000 N•m/(rad/s).
The example I am referring is NREL 5MW: https://www.nrel.gov/docs/fy09osti/38060.pdf, Section 4; "4 Hub and Nacelle Properties"
Besides I am having some issues too, with the calculation of the YawInertia to obtain the same values as in NREL 5MW example. From the information I read, I assume that the YawIner is calculated with the Nacelle (NacMass,NacCMxn) and with the rotor (Rotormass,OverHang). Am I missing anything? Is there any old post where I can see the development?
Thank you a lot for your time.
Kind regards

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Re: Structural loads at pitch and yaw actuator
Dear Pablo,
I agree with your calculations, except that:
Best regards,
I agree with your calculations, except that:
 The YawIner I used was 25,410,000 kg m^2. At the time, I had calculated this using the linearization functionality of FAST. This is very close the value reported in the following forum topic: viewtopic.php?f=3&t=842&p=3419. The inertia you are using is an order of magnitude too small.
 ζ in the equation for YawDamp should be 0.02, not 0.2.
Best regards,
Jason Jonkman, Ph.D.
Senior Engineer  National Wind Technology Center (NWTC)
National Renewable Energy Laboratory (NREL)
15013 Denver West Parkway  Golden, CO 80401
+1 (303) 384 – 7026  Fax: +1 (303) 384 – 6901
nwtc.nrel.gov
Senior Engineer  National Wind Technology Center (NWTC)
National Renewable Energy Laboratory (NREL)
15013 Denver West Parkway  Golden, CO 80401
+1 (303) 384 – 7026  Fax: +1 (303) 384 – 6901
nwtc.nrel.gov

 Posts: 6
 Joined: Fri Jan 04, 2019 1:08 am
 Organization: Self
 Location: Spain
Re: Structural loads at pitch and yaw actuator
Dear Jason,
Thank you very much for your quick response. The new value clarifies the calculation. Nevertheless the value of 2,607,890 kg•m2 posted on NREL 5MW, refers to Nacelle inertia about Yaw axis. This value is not calculated as only I=mr^2, isn't it? Which components contribute to this inertia? Only the nacelle mass (including the generator)?
I was trying to calculate by hand a preliminary value. I was taking into account the nacelle mass and rotor mass as the inertia of two puntual masses (I=m1*m2/(m1+m2)*x^2) and the apply the parallel axis theorem to obtain it at the Yaw axis. I think I was too naive. I will try to reproduce the value you told me, with the linearization functionality of FAST and understand better the process.
Thank you for your time.
Best regards,
Thank you very much for your quick response. The new value clarifies the calculation. Nevertheless the value of 2,607,890 kg•m2 posted on NREL 5MW, refers to Nacelle inertia about Yaw axis. This value is not calculated as only I=mr^2, isn't it? Which components contribute to this inertia? Only the nacelle mass (including the generator)?
I was trying to calculate by hand a preliminary value. I was taking into account the nacelle mass and rotor mass as the inertia of two puntual masses (I=m1*m2/(m1+m2)*x^2) and the apply the parallel axis theorem to obtain it at the Yaw axis. I think I was too naive. I will try to reproduce the value you told me, with the linearization functionality of FAST and understand better the process.
Thank you for your time.
Best regards,

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Re: Structural loads at pitch and yaw actuator
Dear Pablo,
The nacelleyaw inertia of NacYIner = 2,607,890 kgm^2 for the NREL 5MW baseline turbine includes contributions both from the nacelle mass center offset from the yaw axis and the distribution of mass around the nacelle center of mass. However, the value of YawIner in the equation for the yaw spring and damper should include not only the nacelleyaw inertia, but also the inertia of the rotor about the yaw axis. This latter inertia has contributions both from the rotor mass center offset from the yaw axis and the distribution of mass around the rotor center of mass.
Best regards,
The nacelleyaw inertia of NacYIner = 2,607,890 kgm^2 for the NREL 5MW baseline turbine includes contributions both from the nacelle mass center offset from the yaw axis and the distribution of mass around the nacelle center of mass. However, the value of YawIner in the equation for the yaw spring and damper should include not only the nacelleyaw inertia, but also the inertia of the rotor about the yaw axis. This latter inertia has contributions both from the rotor mass center offset from the yaw axis and the distribution of mass around the rotor center of mass.
Best regards,
Jason Jonkman, Ph.D.
Senior Engineer  National Wind Technology Center (NWTC)
National Renewable Energy Laboratory (NREL)
15013 Denver West Parkway  Golden, CO 80401
+1 (303) 384 – 7026  Fax: +1 (303) 384 – 6901
nwtc.nrel.gov
Senior Engineer  National Wind Technology Center (NWTC)
National Renewable Energy Laboratory (NREL)
15013 Denver West Parkway  Golden, CO 80401
+1 (303) 384 – 7026  Fax: +1 (303) 384 – 6901
nwtc.nrel.gov

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 Joined: Fri Oct 02, 2020 2:44 am
 Organization: self
 Location: Belgium
Re: Structural loads at pitch and yaw actuator
Dear Jason,
I'm coming back to what Pablo said about NacYIner, YawSpr and YawDamp numerical values. For NacYIner, it's NacYIner=2.60789E+06 kg.m^2 right? As for YawSpr and YawDamp, should we take the default values in the documentation which are :
9.02832E+09 YawSpr  Nacelleyaw spring constant (Nm/rad)
1.916E+07 YawDamp  Nacelleyaw damping constant (Nm/(rad/s))
Or take the values that respect the 3Hz natural nacelle frequency and a ratio damping of 0.02, as calculated by Pablo, which are:
9.2660e+08 YawSpr  Nacelleyaw spring constant (Nm/rad)
1.9663e+06 YawDamp  Nacelleyaw damping constant (Nm/(rad/s))
Or can we adjust the YawSpr and YawDamp freely with respect to 3Hz and a ratio damping of 0.65 for instance, which will be:
9.2660e+08 YawSpr  Nacelleyaw spring constant (Nm/rad)
6.3905e+07 YawDamp  Nacelleyaw damping constant (Nm/(rad/s))
Kindest regards
Younes
I'm coming back to what Pablo said about NacYIner, YawSpr and YawDamp numerical values. For NacYIner, it's NacYIner=2.60789E+06 kg.m^2 right? As for YawSpr and YawDamp, should we take the default values in the documentation which are :
9.02832E+09 YawSpr  Nacelleyaw spring constant (Nm/rad)
1.916E+07 YawDamp  Nacelleyaw damping constant (Nm/(rad/s))
Or take the values that respect the 3Hz natural nacelle frequency and a ratio damping of 0.02, as calculated by Pablo, which are:
9.2660e+08 YawSpr  Nacelleyaw spring constant (Nm/rad)
1.9663e+06 YawDamp  Nacelleyaw damping constant (Nm/(rad/s))
Or can we adjust the YawSpr and YawDamp freely with respect to 3Hz and a ratio damping of 0.65 for instance, which will be:
9.2660e+08 YawSpr  Nacelleyaw spring constant (Nm/rad)
6.3905e+07 YawDamp  Nacelleyaw damping constant (Nm/(rad/s))
Kindest regards
Younes
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