REFLECTOR:Re: Deltahawk Engine Progress

KeithHallsten reflector@tvbf.org
Sat, 10 May 2003 18:06:33 -0700


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Greg,  See http://www.deltahawkengines.com/object00.htm for the =
schedule.

See also the line drawings of the engines on the website.  You're right; =
the inverted V will easily fit in the standard cowl.

  ----- Original Message -----=20
  From: Greg Poole=20
  To: reflector@tvbf.org=20
  Sent: Saturday, May 10, 2003 4:40 PM
  Subject: REFLECTOR:Engine Progress


  JP,

  Just how much further along is the inverted 200HP Deltahawk =
realistically (ugh!) likely to be? ....and will it likely have a more =
streamlined cowl for the Velocity.

  Still interested,

  Greg in Sydney
  Std RG Velocity Down Under.
  Ph: 9899 2737  Fax: 9899 2726

    ----- Original Message -----=20
    From: Ronnie Brown=20
    To: reflector@tvbf.org=20
    Sent: Sunday, May 11, 2003 8:28 AM
    Subject: Re: REFLECTOR:Rotary 20B dyno Test


    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. =20

    Ronnie Brown
    173 Elite RG - Lycasaurus - 34 hours!


    ----- Original Message -----=20
    From: J.P. Brooks=20
    To: reflector@tvbf.org=20
    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.
        =20
        Al Gietzen
        =20
        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.
        =20
        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.
        =20
        Paul Lamar
        =20
        =20

        Attachment converted: Macintosh HD:power - torque1.gif =
(GIFf/ogle) (00022A41)
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<BODY bgColor=3D#ffffff>
<DIV><FONT face=3DArial size=3D2>Greg,&nbsp; See <A=20
href=3D"http://www.deltahawkengines.com/object00.htm">http://www.deltahaw=
kengines.com/object00.htm</A>&nbsp;for=20
the schedule.</FONT></DIV>
<DIV><FONT face=3DArial size=3D2></FONT>&nbsp;</DIV>
<DIV><FONT face=3DArial size=3D2>See also the line drawings of the =
engines on the=20
website.&nbsp; You're right; the inverted V will easily fit in the =
standard=20
cowl.</FONT></DIV>
<DIV><FONT face=3DArial size=3D2></FONT>&nbsp;</DIV>
<BLOCKQUOTE dir=3Dltr=20
style=3D"PADDING-RIGHT: 0px; PADDING-LEFT: 5px; MARGIN-LEFT: 5px; =
BORDER-LEFT: #000000 2px solid; MARGIN-RIGHT: 0px">
  <DIV style=3D"FONT: 10pt arial">----- Original Message ----- </DIV>
  <DIV=20
  style=3D"BACKGROUND: #e4e4e4; FONT: 10pt arial; font-color: =
black"><B>From:</B>=20
  <A title=3Dgpoole@zeta.org.au href=3D"mailto:gpoole@zeta.org.au">Greg =
Poole</A>=20
  </DIV>
  <DIV style=3D"FONT: 10pt arial"><B>To:</B> <A =
title=3Dreflector@tvbf.org=20
  href=3D"mailto:reflector@tvbf.org">reflector@tvbf.org</A> </DIV>
  <DIV style=3D"FONT: 10pt arial"><B>Sent:</B> Saturday, May 10, 2003 =
4:40=20
PM</DIV>
  <DIV style=3D"FONT: 10pt arial"><B>Subject:</B> REFLECTOR:Engine =
Progress</DIV>
  <DIV><BR></DIV>
  <DIV><FONT face=3DArial color=3D#800000>JP,</FONT></DIV>
  <DIV><FONT face=3DArial color=3D#800000></FONT>&nbsp;</DIV>
  <DIV><FONT face=3DArial color=3D#800000>Just how much further along is =
the=20
  inverted 200HP Deltahawk realistically (ugh!) likely to =
be?&nbsp;....and will=20
  it likely have a more streamlined cowl for the Velocity.</FONT></DIV>
  <DIV><FONT face=3DArial color=3D#800000></FONT>&nbsp;</DIV>
  <DIV><FONT face=3DArial color=3D#800000>Still interested,</FONT></DIV>
  <DIV><FONT face=3DArial color=3D#800000></FONT>&nbsp;</DIV>
  <DIV><FONT face=3DArial color=3D#800000>Greg in Sydney</FONT></DIV>
  <DIV>Std RG Velocity Down Under.<BR>Ph: 9899 2737&nbsp; Fax: 9899=20
  2726<BR></DIV>
  <BLOCKQUOTE dir=3Dltr=20
  style=3D"PADDING-RIGHT: 0px; PADDING-LEFT: 5px; MARGIN-LEFT: 5px; =
BORDER-LEFT: #800000 2px solid; MARGIN-RIGHT: 0px">
    <DIV style=3D"FONT: 10pt arial">----- Original Message ----- </DIV>
    <DIV=20
    style=3D"BACKGROUND: #e4e4e4; FONT: 10pt arial; font-color: =
black"><B>From:</B>=20
    <A title=3Dromott@adelphia.net =
href=3D"mailto:romott@adelphia.net">Ronnie=20
    Brown</A> </DIV>
    <DIV style=3D"FONT: 10pt arial"><B>To:</B> <A =
title=3Dreflector@tvbf.org=20
    href=3D"mailto:reflector@tvbf.org">reflector@tvbf.org</A> </DIV>
    <DIV style=3D"FONT: 10pt arial"><B>Sent:</B> Sunday, May 11, 2003 =
8:28=20
AM</DIV>
    <DIV style=3D"FONT: 10pt arial"><B>Subject:</B> Re: REFLECTOR:Rotary =
20B dyno=20
    Test</DIV>
    <DIV><BR></DIV>
    <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=3D"" 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=20
      when you get airborne.<BR><BR>Dennis Martin<BR>Elite FG Chevy =
V-6<BR><BR>
      <BLOCKQUOTE class=3Dcite cite=3D"" type=3D"cite"><FONT =
face=3DVerdana=20
        color=3D#0000ff size=3D2></FONT><BR><FONT color=3D#0000ff =
size=3D2>I've=20
        completed dynamometer testing of my 3-rotor rotary engine.&nbsp; =

        Overall; I'm very pleased.&nbsp; Great performance from a =
normally=20
        aspirated engine where the all-up installation weighs maybe 45 =
lbs more=20
        than a 200 hp Lyc.&nbsp; It should give me about 270 HP at my =
max=20
        operating point of 2900 prop speed.&nbsp; The following is a =
post to the=20
        rotary engine list (including a response from a rotary Guru), =
and a plot=20
        of sea level torque and HP.&nbsp; More info will eventually be =
available=20
        on my website.</FONT><BR><FONT face=3DVerdana color=3D#0000ff=20
        size=3D2>&nbsp;</FONT><BR><FONT face=3DVerdana color=3D#0000ff =
size=3D2>Al=20
        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=20
        torque curves were run after adjusting</FONT><BR><FONT =
size=3D2>&gt; the=20
        mixture correction table and the timing.&nbsp; Mixture setting=20
        was</FONT><BR><FONT size=3D2>&gt; approximately for maximum =
power.&nbsp;=20
        Data was initially gathered up to</FONT><BR><FONT size=3D2>&gt; =
about 6000=20
        RPM, but looking at the data showed that the torque=20
        curve</FONT><BR><FONT size=3D2>&gt; was still flat, and hp =
increasing, so=20
        subsequent runs were made to</FONT><BR><FONT size=3D2>&gt; 7000 =
RPM. Still=20
        no break in the hp curve.&nbsp; Given that the 2.17=20
        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=20
        only by 10</FONT><BR><FONT size=3D2>&gt; ft-lbs from 210 ft-lbs =
at 4000=20
        rpm to a peak of 220 ft-lbs at 5000 -</FONT><BR><FONT =
size=3D2>&gt; nearly=20
        constant from 4800 to 6800.&nbsp; The 220 ft-lbs is =
not</FONT><BR><FONT=20
        size=3D2>&gt; extraordinary, and could be improved by 9.7 =
compression=20
        rotors vs the</FONT><BR><FONT size=3D2>&gt; stock 9.0 rotors =
that are in=20
        the engine.&nbsp; Mazda's data indicates about</FONT><BR><FONT=20
        size=3D2>&gt; a 4% increase in power with 9.7 vs 9.0 at 5000 =
rpm.&nbsp; It=20
        may also</FONT><BR><FONT size=3D2>&gt; improve some as the =
engine wears in=20
        - this is an engine with only a</FONT><BR><FONT size=3D2>&gt; =
couple of=20
        hours of running since overhaul.</FONT><BR><FONT=20
        size=3D2>&nbsp;</FONT><BR><FONT size=3D2>The 20B is going to =
make one hell=20
        of an aircraft engine.</FONT><BR><FONT size=3D2>I can't wait to =
see one of=20
        these engines in an air race.</FONT><BR><FONT size=3D2>The =
Lycoming=20
        weenies are going to wonder where the severe head wind came from =
:) And=20
        this is only 87 HP per rotor at the benchmark RPM of=20
        6000.</FONT><BR><FONT size=3D2>&nbsp;</FONT><BR><FONT =
size=3D2>Paul=20
        Lamar</FONT><BR><FONT size=3D2>&nbsp;</FONT><BR><FONT =
face=3DVerdana=20
        color=3D#0000ff size=3D2>&nbsp;</FONT><BR><BR>Attachment =
converted:=20
        Macintosh HD:power - torque1.gif (GIFf/ogle)=20
    =
(00022A41)</BLOCKQUOTE></BLOCKQUOTE></BLOCKQUOTE></BLOCKQUOTE></BODY></HT=
ML>

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