Subject: My take....onerotor... { a useless exercise }
From: Paul
Date: 8/3/2000, 5:49 PM


Howard wrote:

Harry:
    My thought at first was the same as yours....... I wanted about the
power a one rotor would put out.... however the numbers stack up very
heavily against the one rotor.    You will eliminate only around 30 lbs
from
your engine over a two rotor...... strike one.....  You will need a
redrive
which adds probably at least that much weight..... strike two,   You
will
need probably the full flywheel weight plus some balance weights.....
strike
3..... You will need the same number of accessories at the same weights
as
the full engine... thus your power to weight ratio deterioriates.....
strike
5.

    If one looks at a two rotor 13B torque curve it is quite possible to
pull 50-70 hp at direct drive prop RPM... the low end torque curve is
very
flat.   My feeling is that a peripheral port housing with the ports
timed to
bring bottom end torque in rather than top end power would definitely
enhance direct drive possibilities.... unfortunately nobody I know of
does
this.
    Looking at direct drive.... eliminate 20 lbs flywheel weight.....
perhaps 25-30 lbs redrive weight..... My numbers say that a 2 rotor
direct
drive engine will be lighter, simpler and inherently more dependable
than a
single rotor engine with redrive...... so why bother????

                             H.W.

 "Castle, Ron" wrote:

Roger Hillyard did this on a dragonfly. Power output was between 60 and 70
hp. Prop only turned 2300 static.



The Aircraft Rotary Engine Newsletter.              Powered by Linux.

http://home.earthlink.net/~rotaryeng/            http://www.linux.org