Subject: HP per gallon burned
From: Rotary Engine
Date: 11/3/2010, 11:54 AM
To: AAA Put this in the To box



Paul,

Can you make sense of this posting... and how it compares to the fuel burn
of the rotary?

Mark S.

----------------------------------------------------------------
I have seen different conversions of fuel burned to horsepower generated so I went back to the GAMI wizards for the details.
John-Paul said:

Typically, the 8.5:1 compression ration engines use 14.9 hp/gph while
the 7.5:1 CR engines use 13.7 hp/gph.
The TSIO-550-E engines use 24° BTDC timing and are a little more efficient
that the typical 7.5:1 CR engines, though.
George speculates ~14.6 hp/gph.  Looking at the operation manual, it looks
more like 14.75 hp/gph. <<<

So there ya' go. Take your pick.

Robert M. Simon
ES-P N301ES
----------------------------------------------------------

Nothing like using a non standard fuel burn number to
bamboozle your customers. hp/gph :) Gami has been at this
misleading stuff for years.  All designed to sell
matched mechanical fuel injection injector orifices.

It is something hard to prove as nobody knows how much
HP their engine is really developing while in the air.
That is why I harp so often on built in torque meters.

BSFC not hp/gph is the world wide standard.
BSFC means Brake Specific Fuel Consumption given
in pounds of fuel burned per HP generated per hour.
Weight of fuel is used for a good reason. The energy
derived is a direct function of the weight of fuel
burned and not the volume of fuel burned.

1 gallon an hour is 6.25 pounds of fuel an hour
at some standard temperature.

This volume number varies widely with temperature
so take claimed BSFC or hp/gph with a grain of salt.

6.25 pounds of fuel for 14.9 HP for one hour is a BSFC
of .42. Possible but unlikely.  The best numbers
I have seen are more like .45.

The current rotary, properly
leaned, is .47. Mazda claims a breakthrough for
the 16X. That could be as low as .41 to.43 when
it appears is my guess. Diesels are typically .38.
The R3350 turbo compound got down to .34 or .35
at 20,000 feet or so.

Cessna claims my C182 with a Cont. O-470 carb is
.5 BSFC or so as I recall. The EGT's and CHT's are
all over the lot. It burns 11 to 12 gallons
an hour at 8000 feet and about 150 MPH.

What kind of cruise numbers are you seeing
and what are the EGT's?

Paul Lamar
-- 
The Rotary Engine NewsLetter. Powered by Linux.
ACRE NL web site. http://www.rotaryeng.net
Youtube key word PaulLamar2
Copyright 1998-2010 All world wide rights reserved.