planetmeister_2000 wrote:
> 
> Fellow group members:
> 
> I'm constructing a crossflow turbine for a high-flow
> low-head canal.  The head is about 5 feet, and the flow is
> 3-6 cubic feet per second.
> 
> I have designed a runner with a diameter of 20 inches and a
> length of 60 inches.  There are 25 blades with a central angle of 42
> degrees and a radius of 7.38 inches (following Aziz' design)
> 
> I want to construct a wide nozzle to capture all the flow -
> 
> could you help with some theoretical proportions for the nozzle?  I'd
> The literature isn't very clear on this...  I would
> greatly appreciate it!!
> 
> Thanks!
> 
> Mike Bishop
> [EMAIL PROTECTED] 

Mike,

For the crossflows we make, the width of the nozzle at maximum opening is 9.5%
of the runner diameter.  So for a 20 inch runner, the value is 1.9 inches. 
However, our design is a little different from yours - we use 18 blades and for
a 20 inch runner we would have a blade radius of 6.52 inches. Other members of
the group may be familiar with the particular design you have chosen and be able
to improve on the 9.5% value I have given - but even so, I would expect it to be
much the same. 

With a 1.9 inch nozzle width, using the values you have given, the turbine will
handle a maximum flow of 13.1 cubic feet per second.  So, the turbine will
always be operating at part flow.  Now, whilst the part flow efficiency of a
crossflow is good, the turbine is much bigger than you need.  If you are sure
that the maximum flow you want to cater for is 6 cubic feet per second then I
suggest you reduce the width and/or diameter to limit the maximum flow to 6 - 9
cubic feet per second.

I have crossflow design software, as an Excel spreadsheet, which I am happy to
provide, however it uses the metric system of units.  Contact me directly if you
would like a copy.

Regards,

Max Enfield
Planetary Power





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