X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from web83911.mail.sp1.yahoo.com ([69.147.92.117] verified) by logan.com (CommuniGate Pro SMTP 5.3.8) with SMTP id 4431477 for flyrotary@lancaironline.net; Sun, 15 Aug 2010 10:10:12 -0400 Received-SPF: none receiver=logan.com; client-ip=69.147.92.117; envelope-from=keltro@att.net Received: (qmail 167 invoked by uid 60001); 15 Aug 2010 14:09:36 -0000 DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=att.net; s=s1024; t=1281881376; bh=BgtKLvtC2envJ8rtZ+qYDW5ycpWGd2ctG1w3ZFxhQyY=; h=Message-ID:X-YMail-OSG:Received:X-Mailer:References:Date:From:Subject:To:In-Reply-To:MIME-Version:Content-Type; b=LTsdAxoBLKTsDCEQOORlcBjaVx2w0VJEjgNulK8t3N+HcXJJIH/9iWqO65X4phhD6sBtqxFcyypkA2rhnK2Gn0+FXJDv79qE5zKDKEaYXBOXu8MfLAO8maTFYFnnLdV40G4Sblh0HKR14WOBYi/yexpzfAa2A1K74GtFu6bLeFU= DomainKey-Signature:a=rsa-sha1; q=dns; c=nofws; s=s1024; d=att.net; h=Message-ID:X-YMail-OSG:Received:X-Mailer:References:Date:From:Subject:To:In-Reply-To:MIME-Version:Content-Type; b=pcSwWNShk9Of+8PzwequmQcf7FXoJsPBU8ufghTJvKKdOpB9ZDiOVBKdq7u1EJHX4U2KXa9BwjSUt7XYwWmWIkqbU8YwDb+RjQEKrqnrHdwW44AzgwjukQrNouswK8gUIRNvpR6TdEnm58OUL6WdshJy1tGqJss6k71AGpXWbV8=; Message-ID: <430268.98415.qm@web83911.mail.sp1.yahoo.com> X-YMail-OSG: AGJ2jd8VM1kCSw.6V3i3OmhTe4qi2mAn7TnNbNFkvd8RwYl TvTP5BIUXG0zbZvTuCm43SBHw8lZY45xd82Qho.k_aFCfi4LUpvKgZgFVuD_ FeptXokZ_aDHT313RPLDZszeTDf0Te2AocBHqpxFsYMe18s.42.H92w7Zoey P_ZlbdwjEpu18sLEK2h7Jfjs6eTHnioG74BZIMntPXIJ_QzoppJyH1czwcJa lArEZjq5vB3JphvnS1RfvFAyAxB9UglVDSEEyt2J96vKaU.MRoTF8FPEcIg7 COj53yQ02zQlaHVjs110ay.Zz0J5QE1DBLH0ZnEZVzd8PNpZkKSsp23Hvtpi x.VxdLQD4Pcs0uplYOB5Lx.q72ycDSpCe4C7x1qZ8dpOV Received: from [208.114.43.10] by web83911.mail.sp1.yahoo.com via HTTP; Sun, 15 Aug 2010 07:09:36 PDT X-Mailer: YahooMailRC/470 YahooMailWebService/0.8.105.279950 References: Date: Sun, 15 Aug 2010 07:09:36 -0700 (PDT) From: Kelly Troyer Subject: Re: Turbo Questions To: Rotary motors in aircraft In-Reply-To: MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="0-38560103-1281881376=:98415" --0-38560103-1281881376=:98415 Content-Type: text/plain; charset=iso-8859-1 Content-Transfer-Encoding: quoted-printable Good to hear you guys giving the group the benefit of your experience and "= Real =0AWorld"=0Ainfo and the "Pros' and=A0"Cons" for those of us still "Gr= oud Bound"=A0 trying to =0Adecide if we=0Awant to venture from NA to Turbo.= .........For those of the group (even Lurkers) =0Aout there=0Ain etherland = listening now is a good time to pick the brain of these Rotary =0A"Pioneers= " who=0Ahave risked both hardware and rears proving what works and what doe= s not =0Awork..........=0A=0AKeep the thread going !!................FWIW= =0AKelly Troyer=0A"Dyke Delta"_13B ROTARY Engine=0A"RWS"_RD1C/EC2/EM2=0A"Mi= stral"_Backplate/Oil Manifold =0A=0A=0A=0A=0A______________________________= __=0AFrom: John Slade =0ATo: Rotary motors in ai= rcraft =0ASent: Sun, August 15, 2010 8:39:59 A= M=0ASubject: [FlyRotary] Re: Turbo Questions=0A=0AOn 8/15/2010 9:03 AM, Ed = Anderson wrote:=0A> The engine doesn't know or care how this increase in pr= essure comes about - =0A>well, actually it does. If you use a turbo or supe= rcharger you are also heating =0A>the air through their compression process= (which is why you need an intercooler =0A>in many cases) thereby moving cl= oser to detonation. =0A>=0AEd, this sentence summarizes the advice I receiv= ed from the Aussie rotary =0Aexpert, Leon Promet (anyone know what became o= f him?) and others. The way he put =0Ait, using the non-turbo (9.7:1) rotor= s in a turbo installation gets you an extra =0A30 HP "for free" because thi= s part of the increased pressure doesn't involve =0Aheating the air via the= turbo. You still have to deal with the potential =0Adetonation either way = if mixture and timing are wrong.=0A=0AMy experience with detonation (or pre= -detonation) was much less severe than =0Ayours. I heard 'popping' at high = rpm during run-up at around 44MAP. Reduce the =0Athrottle a hair and the po= pping ceased. This was with a big fixed pitch prop =0Athat I could only tur= n at around 4900 rpm. I had the feeling that it was rather =0Alike flooring= a car in top gear on a hill. (remember in the old days before ECUs =0Aand = knock sensors when that would get you a popping sound?). I was able to fly = =0Amy first 40 hours with no issues from detonation by keeping the throttle= away =0Afrom the area that caused it during runup. I never experienced (or= at least =0Aheard) any popping once airborne, even during a high-speed run= at 44 MAP and =0A6300 rpm. I once tried hooking up a knock sensor to the i= ntercom without =0Asuccess. I never had any damage to the plugs.=0A=0AWhen = I installed the adjustable IVO prop my static rpm when from 4900 to 5600rpm= =0Aand the popping sound disappeared (analogous to changing gear on the hi= ll?). I =0Ahaven't experienced any popping since. I think Tracy's ECU does = a good job of =0Aproviding a rich mixture at high rpm to keep you away from= detonation.=0A=0ARegards,=0AJohn Slade=0ACozy IV, N96PM=0A=0A--=0AHomepage= :=A0 http://www.flyrotary.com/=0AArchive and UnSub:=A0 http://mail.lancairo= nline.net:81/lists/flyrotary/List.html=0A --0-38560103-1281881376=:98415 Content-Type: text/html; charset=iso-8859-1 Content-Transfer-Encoding: quoted-printable
=0A
Good to hear you guys giving the group the benefit = of your experience and "Real World"
info and the "Pros' and "Cons" = for those of us still "Groud Bound"  trying to decide if we
=0Awant to venture from NA to Turbo..........For those of the group (even L= urkers) out there
=0A
in etherland listening now is a good time to= pick the brain of these Rotary "Pioneers" who
=0A
have risked bot= h hardware and rears proving what works and what does not work..........=0A
 
=0A
Keep the thread going !!................FWIW=
=0A
 
Kelly Troyer
"Dyke Delta"_13B ROTARY Engine"RWS"_RD1C/EC2/EM2
"Mistral"_Backplate/Oil Manifold =0A

= =0A
=0A
=0AFrom: John Slade <jslade@canarda= viation.com>
To: Rota= ry motors in aircraft <flyrotary@lancaironline.net>
Sent: Sun, August 15, 2010 8:39:59 AM
= Subject: [FlyRotary] Re: Tu= rbo Questions

On 8/15/2010 9:03 AM, Ed Anderson wrote:
>= ; The engine doesn't know or care how this increase in pressure comes about= - well, actually it does. If you use a turbo or supercharger you are also = heating the air through their compression process (which is why you need an= intercooler in many cases) thereby moving closer to detonation.
Ed, th= is sentence summarizes the advice I received from the Aussie rotary expert,= Leon Promet (anyone know what became of him?) and others. The way he put i= t, using the non-turbo (9.7:1) rotors in a turbo installation gets you an extra 30 HP "for free" because this part of the increased pressure = doesn't involve heating the air via the turbo. You still have to deal with = the potential detonation either way if mixture and timing are wrong.
My experience with detonation (or pre-detonation) was much less severe tha= n yours. I heard 'popping' at high rpm during run-up at around 44MAP. Reduc= e the throttle a hair and the popping ceased. This was with a big fixed pit= ch prop that I could only turn at around 4900 rpm. I had the feeling that i= t was rather like flooring a car in top gear on a hill. (remember in the ol= d days before ECUs and knock sensors when that would get you a popping soun= d?). I was able to fly my first 40 hours with no issues from detonation by = keeping the throttle away from the area that caused it during runup. I neve= r experienced (or at least heard) any popping once airborne, even during a = high-speed run at 44 MAP and 6300 rpm. I once tried hooking up a knock sensor to the intercom without success. I never had any damage to th= e plugs.

When I installed the adjustable IVO prop my static rpm when= from 4900 to 5600rpm and the popping sound disappeared (analogous to chang= ing gear on the hill?). I haven't experienced any popping since. I think Tr= acy's ECU does a good job of providing a rich mixture at high rpm to keep y= ou away from detonation.

Regards,
John Slade
Cozy IV, N96PM
--
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