Return-Path: <13brv3@bellsouth.net> Received: from imf17aec.mail.bellsouth.net ([205.152.59.65] verified) by logan.com (CommuniGate Pro SMTP 4.1.3) with ESMTP id 2583597 for flyrotary@lancaironline.net; Wed, 17 Sep 2003 21:12:42 -0400 Received: from rad ([68.212.12.251]) by imf17aec.mail.bellsouth.net (InterMail vM.5.01.05.27 201-253-122-126-127-20021220) with ESMTP id <20030918011241.FVVZ17943.imf17aec.mail.bellsouth.net@rad> for ; Wed, 17 Sep 2003 21:12:41 -0400 From: "Russell Duffy" <13brv3@bellsouth.net> To: "'Rotary motors in aircraft'" Subject: RE: [FlyRotary] Re: turbo performance? Date: Wed, 17 Sep 2003 20:12:40 -0500 Message-ID: <000001c37d81$f50eb1e0$0201a8c0@rad> MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_0001_01C37D58.0C38A9E0" X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook, Build 10.0.4510 Importance: Normal In-Reply-To: X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1165 This is a multi-part message in MIME format. ------=_NextPart_000_0001_01C37D58.0C38A9E0 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: quoted-printable Arn't you jumping the gun a little here?=20 =20 Don't worry, I haven't done anything yet. It's just in my nature to over-analyze every option, which is bad enough for me, but the real = victim is my poor wife :-) =20 =20 It's true that you're providing us all with a useful list of things = to avoid, and lots of good wholesome entertainment, =20 =20 Don't make me have to come down there mister :-) =20 =20 but you're also "experimenting" in the true sense of experimental. It = caught my attention when Ed mentioned that he was on his fifth intake, and = Tracy said he didn't love his rotary until 80 hours. Perhaps you're giving up = too early on this.=20 =20 I haven't given up yet, but I am trying to sort out the facts. Aside = from the performance issues, the plane is overweight, and very nose heavy. Losing the turbo, huge radiator, etc could net me 30-50 lbs of weight savings from the nose, which would do wonders for my CG. Lot's of = things to consider. =20 =20 Lets take a step back for a moment. Forget about altitude. On the = ground, and for say the first 3000 feet where you'll be doing most of your = climbing, its a known fact that the turbo 13B produces considerably more horses = than the NA version. =20 =20 The stock turbo only made about 20% more HP than the non-turbo, and that = was at 5.5 to 6.5 psi of boost. Ed's promising us all 15% with just some = tuning (and a dozen or so intakes ). =20 =20 The cars, running at the same altitude, don't blow their turbos and = engines to bits, even at much higher RPM than you're doing. So whats the = difference? =20 Cars have intercoolers, and lower compression rotors. They also = probably have about a hundred million yen worth of development to make sure they don't blow up. Even with all this, the stock 3rd gens, running 10 psi = of boost blow up all the time. In fact it's rare to ever see one with more than 100k miles on the engine. My 93 had it's engine replaced at 60k = due to a broken apex seal. I didn't own it at the time, but it's an all too familiar tale. Of course, you can blame this on the owners who may accidentally run a tank of regular, or the oil metering pump, or = whatever, but if that's all it takes to blow the engine under boost, it bears some concern. Of course altitude is the key factor, since cars are on the ground where it's safe. If I blow the FD engine, I roll to the side of = the road and call AAA :-) =20 =20 Why, at these altitudes, should you're engine perform worse than the one = in a car? =20 =20 I suspect that it isn't performing worse than a car. I just believe = that the turbo car engine doesn't surpass it's NA brother until it reaches = about 4 psi. I'm deciding if it's worth running that much pressure just to = break even. On one hand, Bruce scared me by guessing that I shouldn't exceed = 2-3 psi. On the other hand, 4-5 psi of boost means nothing if it's only producing NA power. The only real concern is the higher intake temps = down low, and the risk of pre-detonation. Bruce also told me of a customer running the exact same basic engine in a car, with 17 psi of boost, = who's putting out 350 HP on a chassis dyno. Believe me, I ask myself every = day why I'm worrying about 7 psi and 200 or so HP :-) =20 =20 I really DO want to keep the turbo, but only if I feel safe running it = hard enough to get some advantage out of it. =20 =20 Thanks for adding fuel to my dilemma :-) Rusty =20 ------=_NextPart_000_0001_01C37D58.0C38A9E0 Content-Type: text/html; charset="us-ascii" Content-Transfer-Encoding: quoted-printable Message
Arn't you jumping the gun a little here? 
 
Don't worry, I=20 haven't done anything yet.  It's just in my nature to = over-analyze=20 every option, which is bad enough for me, but the real victim is my poor = wife=20 :-)     
 
   It's true = that you're=20 providing us all with a useful list of things to avoid, and lots of good = wholesome entertainment,  
&nbs= p;
Don't make me have=20 to come down there mister :-)  
 
but=20 you're also "experimenting" in the true sense of experimental. It caught = my=20 attention when Ed mentioned that he was on his fifth intake, and Tracy = said he=20 didn't love his rotary until 80 hours. Perhaps you're giving up too = early on=20 this. 
 
I = haven't given up=20 yet, but I am trying to sort out the facts.  Aside from the = performance=20 issues, the plane is overweight, and very nose heavy.  Losing the = turbo,=20 huge radiator, etc could net me 30-50 lbs of weight savings from the = nose,=20 which would do wonders for my CG.  Lot's of things=20 to consider.   
 
Lets take a step back for a moment. Forget about altitude. = On the=20 ground, and for say the first 3000 feet where you'll be doing most = of your=20 climbing, its a known fact that the turbo 13B produces considerably more = horses=20 than the NA version.  
 
The = stock turbo=20 only made about 20% more HP than the non-turbo, and that was at 5.5 to = 6.5 psi=20 of boost.  Ed's promising us all 15% with just some tuning (and a = dozen or=20 so intakes <g>).    
 
 The cars, running at the same = altitude,=20 don't blow their turbos and engines to bits, even at much higher RPM = than you're=20 doing. So whats the difference? 
 
Cars have = intercoolers,=20 and lower compression rotors.  They also probably have about a = hundred=20 million yen worth of development to make sure they don't blow=20 up.  Even with all this, the stock 3rd gens, running 10 psi of = boost=20 blow up all the time.  In fact it's rare to ever see one with more=20 than 100k miles on the engine.  My 93 had it's engine replaced = at 60k=20 due to a broken apex seal.  I didn't own it at the time, but it's = an all=20 too familiar tale.  Of course, you can blame this on the = owners who=20 may accidentally run a tank of regular, or the oil metering pump, or = whatever,=20 but if that's all it takes to blow the engine under boost, it bears some = concern.   Of course altitude is the key factor, since cars = are on the=20 ground where it's safe.  If I blow the FD engine, I roll to = the side=20 of the road and call AAA=20  :-)    
 
Why, at these=20 altitudes, should you're engine perform worse than the one in a=20 car?  
 
I suspect = that it isn't=20 performing worse than a car.  I = just believe that the turbo=20 car engine doesn't surpass it's NA brother until it reaches about 4=20 psi.  I'm deciding if it's worth running that much = pressure just=20 to break even.  On one hand, Bruce scared me by guessing that = I=20 shouldn't exceed 2-3 psi.  On the other hand, 4-5 psi=20 of boost means nothing if it's only producing NA power.  = The only=20 real concern is the higher intake temps down low, and the risk of=20 pre-detonation.   Bruce also told me of a customer = running the=20 exact same basic engine in a car, with 17 psi of boost, who's = putting out=20 350 HP on a chassis dyno.  Believe me, I ask myself = every=20 day why I'm worrying about 7 psi and 200 or so HP=20 :-)  
 
I = really DO want to=20 keep the turbo, but only if I feel safe running it hard enough to = get some=20 advantage out of it.  
 
Thanks for = adding fuel=20 to my dilemma :-)
Rusty
  
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