REFLECTOR:Rotary Engine

Al Gietzen reflector@tvbf.org
Fri, 28 May 2004 18:29:26 -0700


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Subject: REFLECTOR:Rotary Engine

=20

Has anyone ever put a rotary in a Velocity?  Or has anyone researched
putting a rotary in a Velocity?  Any pros or cons?

=20

Thanks,

Joe

Why, yes they have.  I am nearing completion on the installation of a
3-rotor on a SE-RG.  I had researched just about every possible option; =
and
concluded it to be the best approach.  It has been quite a challenge =
with
lots of custom engineering.  The engine has tested out on the dyno, and =
will
deliver about 270 hp at max useable rpm.  The total firewall back =
weight,
including coolant (no prop) is 420 lbs.  The engine is normally =
aspirated,
and basically "stock" in terms of performance.  Most of the changes are =
in
the ancillary parts for packaging and weight reduction.  The C.G. is =
closer
to the firewall than a Lyc or Franklin, and I estimate the moment of the
engine package will be about the same as a Lyc 360.

=20

I utilizes electronic ignition and fuel injection that are both =
completely
redundant - 2-plugs per rotor; primary and secondary injections, set up =
to
be able to run on either set.  Should be smooth, reliable power.  You =
can
check it out at  <http://members.cox.net/alg3/airplane.htm>
http://members.cox.net/alg3/airplane.htm.

=20

Any custom engine installation involves a lot of "firsts".  After I have
flown 100 hours I will be able to tell you how successful it is.

=20

Al=20


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<p class=3DMsoNormal style=3D'margin-left:.5in'><b><font size=3D2 =
face=3DTahoma><span
style=3D'font-size:10.0pt;font-family:Tahoma;font-weight:bold'>Subject:</=
span></font></b><font
size=3D2 face=3DTahoma><span =
style=3D'font-size:10.0pt;font-family:Tahoma'> REFLECTOR:Rotary
Engine</span></font></p>

<p class=3DMsoNormal style=3D'margin-left:.5in'><font size=3D3 =
face=3D"Times New Roman"><span
style=3D'font-size:12.0pt'>&nbsp;</span></font></p>

<div>

<p class=3DMsoNormal style=3D'margin-left:.5in'><font size=3D2 =
face=3DArial><span
style=3D'font-size:10.0pt;font-family:Arial'>Has anyone ever put a =
rotary in a
Velocity?&nbsp; Or has anyone researched putting a rotary in a =
Velocity?&nbsp;
Any pros or cons?</span></font></p>

</div>

<div>

<p class=3DMsoNormal style=3D'margin-left:.5in'><font size=3D3 =
face=3D"Times New Roman"><span
style=3D'font-size:12.0pt'>&nbsp;</span></font></p>

</div>

<div>

<p class=3DMsoNormal style=3D'margin-left:.5in'><font size=3D2 =
face=3DArial><span
style=3D'font-size:10.0pt;font-family:Arial'>Thanks,</span></font></p>

</div>

<div>

<p class=3DMsoNormal style=3D'margin-left:.5in'><font size=3D2 =
face=3DArial><span
style=3D'font-size:10.0pt;font-family:Arial'>Joe</span></font></p>

</div>

<div>

<p class=3DMsoNormal><font size=3D2 color=3Dblue face=3DVerdana><span =
style=3D'font-size:
11.0pt;font-family:Verdana;color:blue'>Why, yes they have.&nbsp; I am =
nearing
completion on the installation of a 3-rotor on a SE-RG.&nbsp; I had =
researched just
about every possible option; and concluded it to be the best =
approach.&nbsp; It
has been quite a challenge with lots of custom engineering. &nbsp;The =
engine
has tested out on the dyno, and will deliver about 270 hp at max useable =
rpm. &nbsp;The
total firewall back weight, including coolant (no prop) is 420 lbs. =
&nbsp;The
engine is normally aspirated, and basically &#8220;stock&#8221; in terms =
of
performance.&nbsp; Most of the changes are in the ancillary parts for =
packaging
and weight reduction.&nbsp; The C.G. is closer to the firewall than a =
Lyc or
Franklin, and I estimate the moment of the engine package will be about =
the
same as a Lyc 360.</span></font></p>

<p class=3DMsoNormal><font size=3D2 color=3Dblue face=3DVerdana><span =
style=3D'font-size:
11.0pt;font-family:Verdana;color:blue'>&nbsp;</span></font></p>

<p class=3DMsoNormal><font size=3D2 color=3Dblue face=3DVerdana><span =
style=3D'font-size:
11.0pt;font-family:Verdana;color:blue'>I utilizes electronic ignition =
and fuel
injection that are both completely redundant &#8211; 2-plugs per rotor; =
primary
and secondary injections, set up to be able to run on either set.&nbsp; =
Should
be smooth, reliable power.&nbsp; You can check it out at =
</span></font><font
size=3D2 color=3Dblack face=3DVerdana><span =
style=3D'font-size:11.0pt;font-family:Verdana;
color:black'><a href=3D"http://members.cox.net/alg3/airplane.htm"><font
color=3Dblack><span =
style=3D'color:black'>http://members.cox.net/alg3/airplane.htm</span></fo=
nt></a>.</span></font></p>

<p class=3DMsoNormal><font size=3D2 color=3Dblue face=3DVerdana><span =
style=3D'font-size:
11.0pt;font-family:Verdana;color:blue'>&nbsp;</span></font></p>

<p class=3DMsoNormal><font size=3D2 color=3Dblue face=3DVerdana><span =
style=3D'font-size:
11.0pt;font-family:Verdana;color:blue'>Any custom engine installation =
involves
a lot of &#8220;firsts&#8221;.&nbsp; After I have flown 100 hours I will =
be
able to tell you how successful it is.</span></font></p>

<p class=3DMsoNormal><font size=3D2 color=3Dblue face=3DVerdana><span =
style=3D'font-size:
11.0pt;font-family:Verdana;color:blue'>&nbsp;</span></font></p>

<p class=3DMsoNormal><font size=3D2 color=3Dblue face=3DVerdana><span =
style=3D'font-size:
11.0pt;font-family:Verdana;color:blue'>Al </span></font></p>

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