REFLECTOR:Rotary 20B dyno Test

Ronnie Brown reflector@tvbf.org
Sat, 10 May 2003 18:28:01 -0400


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And congratulations to you too, JP!!!

A long road with light at the end - I know you are tickled with your new plane and diesel.

Ronnie Brown
173 Elite RG - Lycasaurus - 34 hours!


----- Original Message -----
From: J.P. Brooks
To: reflector@tvbf.org
Sent: Saturday, May 10, 2003 5:18 PM
Subject: Re: REFLECTOR:Rotary 20B dyno Test


Great news!
Best of luck.... seriously.
JP Brooks
DeltaHawk, Inc.


At 01:32 PM 5/9/2003 -0600, you wrote:

  Rock on, rotory guy.  Very impressive results, and I'm envious of how silky smooth it's going to be when you
get airborne.

  Dennis Martin
  Elite FG Chevy V-6



    I've completed dynamometer testing of my 3-rotor rotary engine.  Overall; I'm very pleased.  Great
performance from a normally aspirated engine where the all-up installation weighs maybe 45 lbs more than a 200
hp Lyc.  It should give me about 270 HP at my max operating point of 2900 prop speed.  The following is a post
to the rotary engine list (including a response from a rotary Guru), and a plot of sea level torque and HP.
More info will eventually be available on my website.

    Al Gietzen

    POWER AND TORQUE
    >
    > Wide open throttle power and torque curves were run after adjusting
    > the mixture correction table and the timing.  Mixture setting was
    > approximately for maximum power.  Data was initially gathered up to
    > about 6000 RPM, but looking at the data showed that the torque curve
    > was still flat, and hp increasing, so subsequent runs were made to
    > 7000 RPM. Still no break in the hp curve.  Given that the 2.17 redrive
    > ratio limits engine RPM to about 6300 (Prop @ 2900), there was no
    > point in pushing things further.
    >
    > The torque curve is distinguished by it's flatness; varying only by 10
    > ft-lbs from 210 ft-lbs at 4000 rpm to a peak of 220 ft-lbs at 5000 -
    > nearly constant from 4800 to 6800.  The 220 ft-lbs is not
    > extraordinary, and could be improved by 9.7 compression rotors vs the
    > stock 9.0 rotors that are in the engine.  Mazda's data indicates about
    > a 4% increase in power with 9.7 vs 9.0 at 5000 rpm.  It may also
    > improve some as the engine wears in - this is an engine with only a
    > couple of hours of running since overhaul.

    The 20B is going to make one hell of an aircraft engine.
    I can't wait to see one of these engines in an air race.
    The Lycoming weenies are going to wonder where the severe head wind came from :) And this is only 87 HP
per rotor at the benchmark RPM of 6000.

    Paul Lamar



    Attachment converted: Macintosh HD:power - torque1.gif (GIFf/ogle) (00022A41)

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<DIV><FONT size=3D2>And congratulations to you too, JP!!!</FONT></DIV>
<DIV><FONT size=3D2></FONT>&nbsp;</DIV>
<DIV><FONT size=3D2>A long road with light at the end - I know you are =
tickled=20
with your new plane and diesel.&nbsp; </FONT></DIV>
<DIV><FONT size=3D2></FONT>&nbsp;</DIV>
<DIV><FONT size=3D2>Ronnie Brown</FONT></DIV>
<DIV><FONT size=3D2>173 Elite RG - Lycasaurus - 34 hours!</FONT></DIV>
<DIV><FONT size=3D2></FONT>&nbsp;</DIV>
<DIV>&nbsp;</DIV>
<DIV style=3D"FONT: 10pt arial">----- Original Message -----=20
<DIV style=3D"BACKGROUND: #e4e4e4; font-color: black"><B>From:</B> <A=20
title=3Djp@cwebs.com href=3D"mailto:jp@cwebs.com">J.P. Brooks</A> </DIV>
<DIV><B>To:</B> <A title=3Dreflector@tvbf.org=20
href=3D"mailto:reflector@tvbf.org">reflector@tvbf.org</A> </DIV>
<DIV><B>Sent:</B> Saturday, May 10, 2003 5:18 PM</DIV>
<DIV><B>Subject:</B> Re: REFLECTOR:Rotary 20B dyno Test</DIV></DIV>
<DIV><BR></DIV>Great news!<BR>Best of luck.... seriously.<BR>JP=20
Brooks<BR>DeltaHawk, Inc.<BR><BR><BR>At 01:32 PM 5/9/2003 -0600, you =
wrote:<BR>
<BLOCKQUOTE class=3Dcite cite type=3D"cite">Rock on, rotory guy.&nbsp; =
Very=20
  impressive results, and I'm envious of how silky smooth it's going to =
be when=20
  you get airborne.<BR><BR>Dennis Martin<BR>Elite FG Chevy V-6<BR><BR>
  <BLOCKQUOTE class=3Dcite cite type=3D"cite"><FONT face=3DVerdana =
color=3D#0000ff=20
    size=3D2></FONT><BR><FONT color=3D#0000ff size=3D2>I've completed =
dynamometer=20
    testing of my 3-rotor rotary engine.&nbsp; Overall; I'm very =
pleased.&nbsp;=20
    Great performance from a normally aspirated engine where the all-up=20
    installation weighs maybe 45 lbs more than a 200 hp Lyc.&nbsp; It =
should=20
    give me about 270 HP at my max operating point of 2900 prop =
speed.&nbsp; The=20
    following is a post to the rotary engine list (including a response =
from a=20
    rotary Guru), and a plot of sea level torque and HP.&nbsp; More info =
will=20
    eventually be available on my website.</FONT><BR><FONT =
face=3DVerdana=20
    color=3D#0000ff size=3D2>&nbsp;</FONT><BR><FONT face=3DVerdana =
color=3D#0000ff=20
    size=3D2>Al Gietzen</FONT><BR><FONT face=3DVerdana color=3D#0000ff=20
    size=3D2>&nbsp;</FONT><BR><FONT size=3D2>POWER AND =
TORQUE</FONT><BR><FONT=20
    size=3D2>&gt;</FONT><BR><FONT size=3D2>&gt; Wide open throttle power =
and torque=20
    curves were run after adjusting</FONT><BR><FONT size=3D2>&gt; the =
mixture=20
    correction table and the timing.&nbsp; Mixture setting =
was</FONT><BR><FONT=20
    size=3D2>&gt; approximately for maximum power.&nbsp; Data was =
initially=20
    gathered up to</FONT><BR><FONT size=3D2>&gt; about 6000 RPM, but =
looking at=20
    the data showed that the torque curve</FONT><BR><FONT size=3D2>&gt; =
was still=20
    flat, and hp increasing, so subsequent runs were made =
to</FONT><BR><FONT=20
    size=3D2>&gt; 7000 RPM. Still no break in the hp curve.&nbsp; Given =
that the=20
    2.17 redrive</FONT><BR><FONT size=3D2>&gt; ratio limits engine RPM =
to about=20
    6300 (Prop @ 2900), there was no</FONT><BR><FONT size=3D2>&gt; point =
in=20
    pushing things further.</FONT><BR><FONT =
size=3D2>&gt;</FONT><BR><FONT=20
    size=3D2>&gt; The torque curve is distinguished by it's flatness; =
varying only=20
    by 10</FONT><BR><FONT size=3D2>&gt; ft-lbs from 210 ft-lbs at 4000 =
rpm to a=20
    peak of 220 ft-lbs at 5000 -</FONT><BR><FONT size=3D2>&gt; nearly =
constant=20
    from 4800 to 6800.&nbsp; The 220 ft-lbs is not</FONT><BR><FONT =
size=3D2>&gt;=20
    extraordinary, and could be improved by 9.7 compression rotors vs=20
    the</FONT><BR><FONT size=3D2>&gt; stock 9.0 rotors that are in the=20
    engine.&nbsp; Mazda's data indicates about</FONT><BR><FONT =
size=3D2>&gt; a 4%=20
    increase in power with 9.7 vs 9.0 at 5000 rpm.&nbsp; It may=20
    also</FONT><BR><FONT size=3D2>&gt; improve some as the engine wears =
in - this=20
    is an engine with only a</FONT><BR><FONT size=3D2>&gt; couple of =
hours of=20
    running since overhaul.</FONT><BR><FONT =
size=3D2>&nbsp;</FONT><BR><FONT=20
    size=3D2>The 20B is going to make one hell of an aircraft=20
    engine.</FONT><BR><FONT size=3D2>I can't wait to see one of these =
engines in=20
    an air race.</FONT><BR><FONT size=3D2>The Lycoming weenies are going =
to wonder=20
    where the severe head wind came from :) And this is only 87 HP per =
rotor at=20
    the benchmark RPM of 6000.</FONT><BR><FONT =
size=3D2>&nbsp;</FONT><BR><FONT=20
    size=3D2>Paul Lamar</FONT><BR><FONT size=3D2>&nbsp;</FONT><BR><FONT =
face=3DVerdana=20
    color=3D#0000ff size=3D2>&nbsp;</FONT><BR><BR>Attachment converted: =
Macintosh=20
    HD:power - torque1.gif (GIFf/ogle)=20
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