Author Topic: rotor blade axis  (Read 2785 times)

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methanolcat

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rotor blade axis
« on: July 26, 2007, 02:07:13 AM »



         Is the rotor blade axis in this picture just tilted to give clearance for the blades and tower or is there something more?


        For the most part does the wind blow more horizontal or does it blow more of a downward angle, does anyone know, has anyone tested this and would it make any kind of a significant difference?


       Matt

« Last Edit: July 26, 2007, 02:07:13 AM by (unknown) »

Nando

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Re: rotor blade axis
« Reply #1 on: July 25, 2007, 08:18:48 PM »
Yes common trick


Nando

« Last Edit: July 25, 2007, 08:18:48 PM by Nando »

disaray1

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Re: rotor blade axis
« Reply #2 on: July 26, 2007, 05:42:13 AM »
Blade clearance.


 David

« Last Edit: July 26, 2007, 05:42:13 AM by disaray1 »

Mary B

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Re: rotor blade axis
« Reply #3 on: July 26, 2007, 10:06:08 AM »
Many of the commercial designs have a tilt back plus they use a pivot that lets the generator head move up and down in response to different forces on the blades. Not sure how they dampen it but for bigger machines it could help with stresses on the machine.
« Last Edit: July 26, 2007, 10:06:08 AM by MaryAlana »

SparWeb

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Re: rotor blade axis
« Reply #4 on: July 26, 2007, 01:29:22 PM »
Mine is tilted up 5 degrees.

The cosine of 5 degrees is 0.996

The tilt costs me 1.5% of the available power.

« Last Edit: July 26, 2007, 01:29:22 PM by SparWeb »
No one believes the theory except the one who developed it. Everyone believes the experiment except the one who ran it.
System spec: 135w BP multicrystalline panels, Xantrex C40, DIY 10ft (3m) diameter wind turbine, Tri-Star TS60, 800AH x 24V AGM Battery, Xantrex SW4024
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methanolcat

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Re: rotor blade axis
« Reply #5 on: July 26, 2007, 03:36:52 PM »
in what way does it cost you power? and how do you know this?


   Matt

« Last Edit: July 26, 2007, 03:36:52 PM by methanolcat »

johnlm

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Re: rotor blade axis
« Reply #6 on: July 26, 2007, 04:58:20 PM »
Its the same principle as the power loss that happens during furling.  As the blades become non- perpendicular to the air flow, the swept area is reduced and it follows the cosine of the angle difference between perpendicular and the tilt.

This lowering in apparent swept area relative to the flow of the air reduces the power.


As for you initial questions, I believe the average airflow direction is parallel to the ground.  I say average as there may be some localized directional changes caused by trees, ground irregularities or other obsticles.  But in general the airflow is not downward toward the ground.  The tilt back on horizontal mills is usually for clearance reasons.

« Last Edit: July 26, 2007, 04:58:20 PM by johnlm »

Ungrounded Lightning Rod

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Re: rotor blade axis
« Reply #7 on: July 26, 2007, 06:54:23 PM »
The cosine of 5 degrees is 0.996

The tilt costs me 1.5% of the available power.


1-.996 = .004 * 100 = 0.4


Costs you 0.4%

« Last Edit: July 26, 2007, 06:54:23 PM by Ungrounded Lightning Rod »

Ungrounded Lightning Rod

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Re: rotor blade axis
« Reply #8 on: July 26, 2007, 07:05:00 PM »
As the blades become non- perpendicular to the air flow, the swept area is reduced and it follows the cosine of the angle difference between perpendicular and the tilt.

This lowering in apparent swept area relative to the flow of the air reduces the power.


Actually it's a tad different:


As you become non-perpendicular the component of the airflow along the axis is lower.  You've slowed the wind seen by the turbine by that cosine factor.


The available power is the CUBE of the airspeed, so the reduction in potential power is 1 - cos(angle)^3.


However it's not that simple for two reasons:

 - A windcharger does not load the turbine optimally, so the output power is not a cube function of the wind.  All that matters is current, which is proportional to torque (and to (gen voltage - (battery voltage + diode drop))/series resistance).  So it's pretty close to a first order function of (wind - cutin wind speed).

 - The cross-axis component of wind interacts with the blades in a complex way.


Still, a 5 degree tilt probably doesn't make enough difference to measure with ordinary test equipment.

« Last Edit: July 26, 2007, 07:05:00 PM by Ungrounded Lightning Rod »

Nando

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Re: rotor blade axis
« Reply #9 on: July 26, 2007, 09:40:47 PM »
You have one formula then you apply another to obtain the results


You said:

The available power is the CUBE of the airspeed, so the reduction in potential power is 1 - cos(angle)^3.


> 1-.996 = .004 * 100 = 0.4 %


Is this the correct calculation THEN ?


In one 1- cos(angle)^3 ( to the cube of the speed)


so 1 - 0.996^3 = 1-0.98805 = 0.01195206 % wise = 1.19952 %


Nando

« Last Edit: July 26, 2007, 09:40:47 PM by Nando »

SparWeb

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Re: rotor blade axis
« Reply #10 on: July 27, 2007, 12:58:47 PM »
Still wrong!


Not only is the velocity through the disk reduced by 0.996 to the power of 3, but the swept area is also reduced by 0.996.


cos(0.996) ^ 4 = 0.985


1-0.985 = 0.015 or 15%

« Last Edit: July 27, 2007, 12:58:47 PM by SparWeb »
No one believes the theory except the one who developed it. Everyone believes the experiment except the one who ran it.
System spec: 135w BP multicrystalline panels, Xantrex C40, DIY 10ft (3m) diameter wind turbine, Tri-Star TS60, 800AH x 24V AGM Battery, Xantrex SW4024
www.sparweb.ca

scottsAI

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Re: rotor blade axis
« Reply #11 on: July 27, 2007, 06:53:59 PM »
SparWeb,


You are joking about the wind speed decreasing by the cos of apparent angle?

Scott.

« Last Edit: July 27, 2007, 06:53:59 PM by scottsAI »

johnlm

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Re: rotor blade axis
« Reply #12 on: July 30, 2007, 08:32:15 PM »
I agree.  Please explain how the velocity decreases through the prop.

also when I was in school 0.015 was 1.5% not 15%

johnlm
« Last Edit: July 30, 2007, 08:32:15 PM by johnlm »

SparWeb

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Re: rotor blade axis
« Reply #13 on: July 31, 2007, 12:07:44 AM »
Sorry that was the pet monkey pushing buttons on the scientific calculator.  I'm also sorry for the glib second posting where I still didn't catch my mistake.


The plane of the disk is inclined to the airflow by 5 degrees.  Its swept area is reduced by 1-cos(5).  That's 0.4%.  Any other effects, like changes to the apparent angle of attack are also negligible, so ignore them unless the angle is much greater.


Boy I wish I could delete a posting today!

« Last Edit: July 31, 2007, 12:07:44 AM by SparWeb »
No one believes the theory except the one who developed it. Everyone believes the experiment except the one who ran it.
System spec: 135w BP multicrystalline panels, Xantrex C40, DIY 10ft (3m) diameter wind turbine, Tri-Star TS60, 800AH x 24V AGM Battery, Xantrex SW4024
www.sparweb.ca

scottsAI

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Re: rotor blade axis
« Reply #14 on: July 31, 2007, 07:45:23 AM »
SparWeb,


Your posts are excellent.

You had me scratching my head!


Looking forward to your future excellent post.

Thanks for letting us know:-)

Have fun,

Scott.

« Last Edit: July 31, 2007, 07:45:23 AM by scottsAI »