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Date: Sat, 13 Aug 2011 16:10:38 -0500
Message-ID: <CAHh3jbNYOKX0WXR93A4LesBsfb2zxAQg5MqNDmFgxHgkpnQStw@mail.gmail.com>
Subject: Re: [FlyRotary] Re: Rotary Roster Spreadsheet Updated
From: Mark Steitle <msteitle@gmail.com>
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
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OK, thanks for the updates.  Anyone else have any updates/corrections,
please let me know.

Mark



On Tue, Aug 9, 2011 at 8:23 PM, Steven W. Boese <SBoese@uwyo.edu> wrote:

>  Mark:
>
>
>
> Please include any of the additions/corrections you think are appropriate.
>
>
>
> Steve (last name spelled) Boese
>
> Prop: Warp drive 3 blade 68 x 17*
>
> Ignition: LS1 coils
>
> Modifications:  dual alternators, Floscan and pulse width based (with
> injector dead time correction) fuel flow indicators and totalizers.  Engine
> and flight parameter data logging.   Injector dead time correction added to
> EC2 controller A.   Retained oil metering system but with separate oil
> supply and steel lines.  0.020" dia fuel bypass.  Fuel pressure regulator
> with return co-located with fuel pumps allowing single fuel line to fuel
> rails.
>
> Significant events:  SAG and abnormally short spark plug life probably due
> to over-advanced ignition timing.  RD1A prop shaft developed end play
> requiring shim installation and replacement of ball bearing and seal,
> partially attributed to Performance Propeller tip flutter.
>

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OK, thanks for the updates. =A0Anyone else have any updates/corrections, pl=
ease let me know.<div><br></div><div>Mark</div><div><br></div><div><br><br>=
<div class=3D"gmail_quote">On Tue, Aug 9, 2011 at 8:23 PM, Steven W. Boese =
<span dir=3D"ltr">&lt;<a href=3D"mailto:SBoese@uwyo.edu">SBoese@uwyo.edu</a=
>&gt;</span> wrote:<br>
<blockquote class=3D"gmail_quote" style=3D"margin:0 0 0 .8ex;border-left:1p=
x #ccc solid;padding-left:1ex;">




<div>
<div style=3D"direction:ltr;font-family:Tahoma;color:#000000;font-size:10pt=
">
<p><font size=3D"3" face=3D"Times New Roman">Mark:</font></p>
<p><font size=3D"3" face=3D"Times New Roman"></font>=A0</p>
<p><font size=3D"3" face=3D"Times New Roman">Please include any of the addi=
tions/corrections you think are appropriate.</font></p>
<p><font size=3D"3" face=3D"Times New Roman"></font>=A0</p>
<p><font size=3D"3" face=3D"Times New Roman">Steve (last name spelled) Boes=
e</font></p>
<p><font size=3D"3" face=3D"Times New Roman">Prop: Warp drive 3 blade 68 x =
17*</font></p>
<p><font size=3D"3" face=3D"Times New Roman">Ignition: LS1 coils</font></p>
<p><font size=3D"3" face=3D"Times New Roman">Modifications:=A0 dual alterna=
tors, Floscan and pulse width based (with injector dead time correction) fu=
el flow indicators and totalizers.=A0=A0Engine and flight parameter data lo=
gging.=A0=A0=A0Injector dead time correction added
 to EC2 controller A.=A0=A0=A0Retained oil metering system but with separat=
e oil supply and steel lines. =A00.020&quot; dia fuel bypass.=A0=A0Fuel pre=
ssure regulator with return=A0co-located with fuel pumps=A0allowing=A0singl=
e fuel line to fuel rails.=A0=A0</font></p>

<p><font size=3D"3" face=3D"Times New Roman">Significant events:=A0 SAG and=
 abnormally short spark plug life probably due to over-advanced ignition ti=
ming.=A0 RD1A prop shaft developed end play requiring shim installation and=
 replacement of ball bearing and seal, partially
 attributed to Performance Propeller tip flutter.=A0=A0=A0</font><br>
</p>
</div>
</div>

</blockquote></div><br></div>

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