Steve, in order to see how we can stuff radiators under the
cowl, Paul needs some measurements taken along the length of
the
cowl from the firewall to the spinner. Here is what he
needs:
Width and height every ten inches along the length
and a picture taken from 20 feet away directly from the side.
In other words perpendicular from a side view.
Jerry
Hi Jerry,
These are approximate at best:
At the fuselage: 38 wide by 23 1/4 tall
Fuselage + 10: 36 wide by 21.5 tall
Fuselage + 20: 34 wide by 19.75 tall
Fuselage +30: 32 wide by 18 tall
Spinner: 30 wide by 12 tall
This does not include the extra space for the Lycoming carb (I
think
thats what the thing on the bottom is).
Some pictures attached. I took a side shot at 20 and 10.
Cheers,
Steve
Thanks Steve and Jerry.
Looks like there is plenty of room to use a prop extension
three or four inches long, move the engine back 3 or four inches
in the stock cowl and have a lot more room for the coolant rads and
intercooler
up front. I will lay things out again in the next couple of days.
Moving
the engine back also improves the lower motor mount tube buckling
situation.
Also looks like they changed the shape of the Legacy cowl. The old
cowl has
more room inside for cooling rads.
Paul Lamar ...No rotor no motor.
Three inches back together with the 3 inch extension would be
o.k. I think you will have a problem if you move the engine back more
than 3 inches as it is then to close too the firewall to remove the
water pump. This is for the 13B, I don't if same applies to the
Renesis. Jerry
OK we will see what it looks like.
Paul Lamar ...No rotor no motor.
The Rotary Engine NewsLetter. Powered by Linux.
ACRE NL web site.
http://www.rotaryeng.net
Copyright 1998-2007 All world wide rights reserved.