Yes, George, unfortunately, approx ½ of
the total energy in our fuel goes out the exhaust - a turbocharger can capture
a very small part of that energy and drive additional air into the engine to
which you can additional fuel producing even more heat (and some additional
work – driving the prop).
Just think if you could recover 20% of
that exhaust energy and make it turn the prop. That would add 20% of (47880/2)
BTU/Min = 0.2 * 23940 = 4788 BTU/min more work energy = 112 HP more + 270 = 382
HP not a bad increase. If only.
The turbocompound approach does indeed
capture some of that energy – but, I’ve only seen it used on
pretty massive and large engines. . The figures I have seen have been around
6% energy recapture, which if you have a 2000 hp engine and 8000 HP of energy
is going out the exhaust then 0.06 * 8000 = 492 HP which can make it worthwhile.
Its not simply, light nor cheap and while it has been successfully used , it
seems to fade in and out of favor. But, with the advent of the turbo jet
engine – the turbo compound seems to have faded into history as far as
use in aircraft engines.
I would like to see it succeed on the
rotary but, I’m not holding my breath. I saw some photos back about 3-4
years ago of a project to try it on the Rotary but never heard if it ever ran
or the results. I presume if it had been a success, we would have heard about
it.
If it were practical and cost effective, I
think the automotive industry would have jumped on it with both feet. But, who
knows perhaps in the future.
In the meantime, I’ll just wait for
the 16X.
Ed
From: Rotary motors in aircraft
[mailto:flyrotary@lancaironline.net] On
Behalf Of George Lendich
Sent: Wednesday, January 06, 2010
5:44 PM
To: Rotary
motors in aircraft
Subject: [FlyRotary] Re: Waste
Heat was [Fly Rotary] Re: Air Flow Question
I see you have allowed for the exhaust etc. in your
calculations- I shouldn't rush in until I read everything fully.
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