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WIND ENERGY SYSTEMS - Cd3wd

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Chapter 4—Wind Turbine Power 4–15<br />

These results illustrate the fact that the rated overall efficiency may be significantly lower than the<br />

maximum coefficient of performance of the turbine itself. This is not a major problem if the various<br />

efficiencies are high below the rated wind speed. For wind speeds at or above rated, the power in the<br />

wind is large enough that somewhat lower efficiencies do not prevent rated power from being reached.<br />

The rated overall efficiency just defined is only valid at rated wind speed. We need to<br />

know the overall efficiency at lower wind speeds to determine the energy production of the<br />

turbine, so we need to determine the individual efficiencies. We have already examined the<br />

variation of C p , so we shall now consider η m and η g .<br />

Transmission losses are primarily due to viscous friction of the gears and bearings turning<br />

in oil. At fixed rotational speed, the losses do not vary strongly with transmitted torque. It<br />

is therefore reasonable to assume that the transmission loss is a fixed percentage of the low<br />

speed shaft rated power. The actual percentage will vary with the quality of the transmission,<br />

but a reasonable value seems to be 2 percent of rated power per stage of gears. The maximum<br />

practical gear ratio per stage is approximately 6:1, so two or three stages of gears are typically<br />

required. Two stages would have a maximum allowable gear ratio of (6) 2 :1 = 36:1 so any<br />

design requiring a larger gear ratio than this would use three stages.<br />

Suppose that q is the number of gear stages. The transmission efficiency is then<br />

η m = P t<br />

= P m − (0.02)qP mR<br />

(17)<br />

P m P m<br />

where P mR is the rated turbine shaft power.<br />

This equation is plotted in Fig. 13 for one, two, and three stages. It can be seen that<br />

the transmission efficiency is not very good for low power inputs. It is therefore desirable to<br />

choose ratings such that the transmission is operating above the knee of the curve in Fig. 13<br />

as much as possible.<br />

Example<br />

How many gear stages are required in the transmission for the Sandia 17-m Darrieus to drive a<br />

1800 r/min generator for each of the proposed speeds of 42 and 52.5 r/min? Assume the maximum<br />

gear ratio for a single stage is 6:1.<br />

The overall gear ratio at 42 r/min is 1800/42 = 42.86:1, while at 52.5 r/min it is 1800/52.5 =<br />

34.29:1. Operating at 42 r/min requires a 3 stage transmission while a 2 stage transmission would be<br />

adequate at 52.5 r/min. The transmission for the 52.5 r/min system will therefore be more efficient<br />

and probably less expensive than the corresponding transmission for the 42 r/min system. This would<br />

encourage us to use the higher speed system, if possible.<br />

It should be mentioned that synchronous generators are also made to operate at 1200 r/min for<br />

only a small increase in cost over the 1800 r/min version. Therefore, the possibility of using a 1200<br />

r/min generator should be examined if the 42 r/min mode is selected. This would present an overall<br />

gear ratio of 1200/42 = 28.57:1, which could be accomplished with a two stage transmission.<br />

The generator losses may be considered in three categories: hysteresis and eddy current<br />

Wind Energy Systems by Dr. Gary L. Johnson November 21, 2001

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