X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from mail-fx0-f213.google.com ([209.85.220.213] verified) by logan.com (CommuniGate Pro SMTP 5.2.16) with ESMTP id 3861458 for flyrotary@lancaironline.net; Mon, 21 Sep 2009 17:25:04 -0400 Received-SPF: pass receiver=logan.com; client-ip=209.85.220.213; envelope-from=msteitle@gmail.com Received: by fxm9 with SMTP id 9so2552955fxm.1 for ; Mon, 21 Sep 2009 14:24:28 -0700 (PDT) DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=gmail.com; s=gamma; h=domainkey-signature:mime-version:received:in-reply-to:references :date:message-id:subject:from:to:content-type; bh=laGGez5qJFOE855AwaoTiYK108oHkzBgueipudano8I=; b=QlBHgOo9P7m/Z9J3oIwFNb7itINr/sZ9GUn+ayyXV8HOWL8HT3c6HygShw2WqHnt1v /xkXvqrN2WiIrVyNzDjwZj7/4U3UE6EMvIRcUXPz38MqUij+Pbutoz6aBH27R6EAN9Vd SN4ROm6I1FOVIJZLyxrP6NsXB1LtyO6QBQtVY= DomainKey-Signature: a=rsa-sha1; c=nofws; d=gmail.com; s=gamma; h=mime-version:in-reply-to:references:date:message-id:subject:from:to :content-type; b=mWpYJ8uc+GcGlVjnf630ed/wr6IHEoMWAX5rR3Tqs2o1omEgdCvEXypo3WH9FCPPav ZJ4x2ifNyzRKGGFAaKMe11TTLFEF7r0yfmfaaR5y+/pNlJA7haIyK0N9upxW4euvNEo7 DUO8Pb7seBOHLblRbavgT4lSneFL7HG9+12og= MIME-Version: 1.0 Received: by 10.204.154.83 with SMTP id n19mr98424bkw.121.1253568268139; Mon, 21 Sep 2009 14:24:28 -0700 (PDT) In-Reply-To: References: Date: Mon, 21 Sep 2009 16:24:28 -0500 Message-ID: <5cf132c0909211424g36d1a964ocf420b04973ec9b9@mail.gmail.com> Subject: Re: [FlyRotary] Progress report from Houston From: Mark Steitle To: Rotary motors in aircraft Content-Type: multipart/alternative; boundary=0015175cac5652ff7404741d1b4f --0015175cac5652ff7404741d1b4f Content-Type: text/plain; charset=ISO-8859-1 Kelly, Yes, I TIG welded them to the inner liner, then used PL's sealing plates and Ultra Grey RTV to seal off the coolant. I plan to pressure test them prior to assembly. Mark On Mon, Sep 21, 2009 at 2:41 PM, Kelly Troyer wrote: > Mark, > Have you made any decisions on the retension/sealing method for your 20B > "P" port inserts ?? > -- > Kelly Troyer > "Dyke Delta"_13B ROTARY Engine > "RWS"_RD1C/EC2/EM2 > "Mistral"_Backplate/Oil Manifold > > -------------- Original message from Mark Steitle : > -------------- > > Bill, > > I'm not sure what's changed, but my oil temps are up from what I reported > earlier. I routinely see 220-225 on climbout, then they settle down to 200 > in cruise. Maybe I'm producing more hp now, or maybe the earlier > temperature report was not in mid-summer, or possibly my system is not > cooling as well as it did earlier. I'm just glad that I installed TES > o-rings throughout. > My cowl flap initially had an aluminum lip, that protruded into the > airstream about 1". This was a quick and dirty test to see the result. I > couldn't open or close it, it was open all the time. I have since replaced > the 1" lip with a servo-controlled door so I can open/close as desired. > When closed it is the same as a stock cowl. This is very helpful in cooler > climates, not so much during triple-digit Texas summer months. > > I also added an "airfoil shaped" piece on the firewall directly above the > cowl flap opening. This was done in the hope of helping coax the heated air > out of the cowl. But I didn't detect any great improvement in cooling. Oh, > well. Next thing I plan on adding is small air dams on each end of the flap > door. The idea here is to promote more efficient airflow out of the cowl > flap. I've heard that these make a big difference. We'll see. > If you are considering installing a cowl flap, you may want to consider > locating it on the side, or possibly install one on each side, back near the > firewall. This would allow you to make the opening larger, and this > location may be in a lower pressure area than the bottom, especially during > climbout. Just a thought. > > Cooling is still marginal in the Texas heat, and it will be worse with the > new P-port 20B engine. So, I may be forced to make some major changes to > get the more powerful engine to cool, or else be forced to throttle back > during climbout. I've been considering relocating the radiator from under > the engine to the cool side of the engine (fore/aft). This would allow me > to use a slightly larger radiator. It would clean up the plumbing and > significantly shorten the cooling lines too. > No, I haven't experienced SAG. But then I'm running Renesis type irridium > spark plugs. I'm at 143 hours now. Personally, I won't use anything else. > > > Mark > > > --0015175cac5652ff7404741d1b4f Content-Type: text/html; charset=ISO-8859-1 Content-Transfer-Encoding: quoted-printable
Kelly,
=A0
Yes, I TIG welded them to the inner liner, then used PL's sealing = plates and Ultra Grey RTV to seal off the coolant.=A0 I plan to=A0pressure = test them prior to assembly.
=A0
Mark

On Mon, Sep 21, 2009 at 2:41 PM, Kelly Troyer <keltro@att.net>= ; wrote:
Mark,
=A0 Have you made any decisions on the retension/sealing method for yo= ur 20B "P" port inserts ??
--
Kelly Troyer
"Dyke Delta"_13B ROTARY Engine
&q= uot;RWS"_RD1C/EC2/EM2
"Mistral"_Backplate/Oil Manifold <= /div>
-------------- Original message from Mark Steitle <msteitle@gmail.com>= ;: --------------

Bill,
=A0
I'm not sure what's changed, but my oil temps are up from what= I reported earlier.=A0 I routinely see 220-225 on climbout, then they sett= le down to 200 in cruise.=A0 Maybe I'm producing more hp now, or maybe = the earlier temperature report was not in mid-summer, or possibly my system= is not cooling as well as it did earlier.=A0 I'm just glad that I=A0in= stalled TES o-rings throughout.=A0
My cowl flap initially had an aluminum lip, that=A0protruded into the = airstream=A0about 1".=A0 This was a quick and dirty test to see the re= sult.=A0=A0I couldn't open or close it, it was open all the time.=A0 I = have since replaced the 1" lip with a servo-controlled=A0door so I can= open/close as desired.=A0 When closed it is the same as a stock cowl.=A0 T= his is very helpful in cooler climates, not so much during triple-digit Tex= as summer months.
=A0
I also added an "airfoil shaped" piece on the firewall direc= tly above the cowl flap opening.=A0 This was done=A0in the hope=A0of helpin= g coax=A0the heated air out of=A0the cowl.=A0 But I didn't detect any g= reat improvement in cooling.=A0 Oh, well.=A0=A0Next thing I plan on adding = is small air dams on each end of the flap door.=A0 The idea here is to prom= ote more efficient airflow out of the cowl flap.=A0 I've heard that the= se make a big difference.=A0 We'll see.=A0=A0=20
=A0
If you are considering installing a cowl flap, you may want to conside= r locating=A0it on the side, or=A0possibly install one on=A0each side, back= near the firewall.=A0 This would allow you to make=A0the opening=A0larger,= and this location=A0may=A0be=A0in a lower pressure area than=A0the bottom,= especially during climbout.=A0 Just a thought.
=A0
Cooling is still marginal in the Texas=A0heat, and=A0it will be worse = with=A0the new P-port 20B engine.=A0 So, I may be forced to make some major= changes to get the more powerful=A0engine to cool, or else be forced to th= rottle back during climbout.=A0 I've=A0been considering=A0relocating th= e radiator from under the engine to=A0the cool side of the engine (fore/aft= ).=A0 This would allow me to use a slightly larger radiator.=A0 It would cl= ean up the plumbing and significantly shorten the cooling lines too.=A0=A0= =A0
No, I haven't experienced SAG.=A0 But then I'm running Renesis= type irridium spark plugs.=A0 I'm at 143 hours now.=A0 Personally, I w= on't use anything else.=A0
=A0
Mark
=A0

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