X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from EXHUB003-3.exch003intermedia.net ([207.5.74.110] verified) by logan.com (CommuniGate Pro SMTP 5.3.2) with ESMTPS id 4118106 for flyrotary@lancaironline.net; Tue, 09 Feb 2010 15:13:01 -0500 Received-SPF: none receiver=logan.com; client-ip=207.5.74.110; envelope-from=jwhaley@datacast.com Received: from EXVMBX003-5.exch003intermedia.net ([207.5.74.45]) by EXHUB003-3.exch003intermedia.net ([207.5.74.110]) with mapi; Tue, 9 Feb 2010 12:12:24 -0800 From: Jeff Whaley To: Rotary motors in aircraft Date: Tue, 9 Feb 2010 12:14:37 -0800 Subject: RE: [FlyRotary] Re: rpm vs Power was : Throttle limits was Re: N.A. Renesis to turbo Thread-Topic: [FlyRotary] Re: rpm vs Power was : Throttle limits was Re: N.A. Renesis to turbo Thread-Index: AcqpmK2GWL39iahQRGOkx0V34txQzwAKTg+A Message-ID: References: In-Reply-To: Accept-Language: en-US Content-Language: en-US X-MS-Has-Attach: yes X-MS-TNEF-Correlator: acceptlanguage: en-US Content-Type: multipart/mixed; boundary="_004_C03ABB0A7362B84BB53D544B3C305E0E017931DE85B7EXVMBX0035e_" MIME-Version: 1.0 --_004_C03ABB0A7362B84BB53D544B3C305E0E017931DE85B7EXVMBX0035e_ Content-Type: multipart/alternative; boundary="_000_C03ABB0A7362B84BB53D544B3C305E0E017931DE85B7EXVMBX0035e_" --_000_C03ABB0A7362B84BB53D544B3C305E0E017931DE85B7EXVMBX0035e_ Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: quoted-printable Hi Mike, for reference my throttle body and intake are very similar to your= s; i.e., I copied Tracy's original dynamic intake and used the cut-down (3 = to 2 port) Mazda throttle body ... see attached. With my 2.85:1 reduction unit there is also a bit of travel left without fu= rther increase in power; however, it isn't 1/3 it's more like 1/5 or 1/6; i= .e. maybe the last 0.75" to 1" of travel out of 5" total. My installation differs from yours with regards to exhaust, prop and reduct= ion drive ... so again many variables and about all I can conclude is it's = not all attributed your throttle body or intake. Jeff From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Beh= alf Of Ed Anderson Sent: Tuesday, February 09, 2010 10:00 AM To: Rotary motors in aircraft Subject: [FlyRotary] Re: rpm vs Power was : Throttle limits was Re: N.A. Re= nesis to turbo Good point, Tracy I had one instance where I my static and top end rpm were essentially the s= ame. I had a static of 6000 rpm and a top end in flight of around 6100 rpm= . But, in my case, the cause was very obvious - my muffler of the time was= limiting the top end to my static rpm. Once I changed the muffler - top e= nd rpm was again up around 6800 rpm. Ed Ed Anderson Rv-6A N494BW Rotary Powered Matthews, NC eanderson@carolina.rr.com http://www.andersonee.com http://www.dmack.net/mazda/index.html http://www.flyrotary.com/ http://members.cox.net/rogersda/rotary/configs.htm#N494BW http://www.rotaryaviation.com/Rotorhead%20Truth.htm ________________________________ From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Beh= alf Of Tracy Crook Sent: Tuesday, February 09, 2010 8:21 AM To: Rotary motors in aircraft Subject: [FlyRotary] Re: rpm vs Power was : Throttle limits was Re: N.A. Re= nesis to turbo Ed's experience pretty much matches my own when changing gear drive ratios.= A little more top end. (Sun 100 results were 209 mph w/ 2.176 drive vs 2= 17.5 mph the next year with 2.85 drive.) Takeoff & climb performance impr= oved dramatically though. It's not an inexpensive change though. What does mystify me is the small difference between Mike's static & top en= d rpm. I got an 1100 rpm difference. 5200 vs 6300 with a 68 - 81 Performa= nce prop. Another detail I'm not certain about is whether Mike's manifold pressure is= or is not increasing during that last 1/3 - 1/2 throttle travel with no po= wer increase. Seems like he said it did go up but I'm not sure. If it is = going up, there is still something unexplained going on. What was the MP d= oing Mike? Was it at full ambient at the point where the rpm stopped incre= asing? Tracy On Tue, Feb 9, 2010 at 12:12 AM, Ed Anderson > wrote: Well, Mike, just for comparison, when I had a 2.17:1 and a 68 x72 Performance prop, 5200 -5400 rpm on a nominal 70deg day was what I got for static. While I don't claim my set up was the best in the land, I think it was a pretty fair set up. So I would say you are doing just fine. It does not matter how large a throttle body you have when the manifold air density hits ambient or as close as it can given any losses in the inductio= n system - that's it. You can continue to open the throttle body, but you will not get any more power. However, there is a way! Looking at some of the variables in the power equation we have: Power(HP) =3D Torque * rpm/ 5250, swapping some variables around we get: RPM =3D Power/torque. So this indicates the rpm can increase if either the power is increased or the torque is decreased. Well, it's difficult to increase the power by itself(unless you go to forced induction or nitrous oxide) But one way to get more rpm (and ultimately more power) is to lower the Torque load on the engine. Decreasing the Torque permits more engine rpm even if power did not increase. However we know that more rpm =3D more air= =3D more power. The torque load on the engine caused by the prop decreases as your gear ratio increases. By going to a 2.85:1 gear ratio that would reduce the load on the engine by approx 25% (assuming the same prop at the same static rpm). Now the rpm power relationship were linear (which it is not with a prop as the load) then I should have gotten around 6650 rpm with the new gear box - well not really - due to the cube root relationship between prop rpm and power, it will be much less of an increase and due to the fact I put on a larger diameter prop. But in any case, all this theory aside, with the 2.85 and 74 x88 prop I no= w get engine 6000 - 6200 rpm static or about an 13% increase in rpm. So that's using use the same intake, throttle body and engine for both. But now because the engine can turn faster (lesser prop load at any specific rpm). Now the fact the engine is turning faster means it takes more airflow to maintain the same (ambient) air density in the manifold. This is because th= e higher engine rpm can "suck" that manifold volume (which didn't change) dow= n faster than it did before. This in turn means that the throttle position has to be more open to let a sufficient increase in air flow need to achiev= e and maintain that (hopefully) ambient air density in the manifold. So from what you are reporting, I really don't see anything poor about your performance with your set up. In fact, it's pretty good. The new set up gave a noticeable benefit in take off performance (and I do mean noticeable). However, the top end was relatively unaffected - althoug= h I did measure an approx 4 mph increase in top aircraft speed. In any case, that is my experience. FWIW Ed Anderson Rv-6A N494BW Rotary Powered Matthews, NC eanderson@carolina.rr.com http://www.andersonee.com http://www.dmack.net/mazda/index.html http://www.flyrotary.com/ http://members.cox.net/rogersda/rotary/configs.htm#N494BW http://www.rotaryaviation.com/Rotorhead%20Truth.htm -----Original Message----- From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Mike Wills Sent: Monday, February 08, 2010 10:36 PM To: Rotary motors in aircraft Subject: [FlyRotary] Re: Throttle limits was Re: N.A. Renesis to turbo Thanks Ed. Mentioned this a few months ago and was convinced at least for the moment, to just fly the plane as is. So that's what I have been doing. To recap, my engine is an NA 13B built by Bruce Turrentine. It is a second gen engine with Turbo rotor housings (no exhaust splitter) and high compression NA rotors. The exhaust uses 1 3/4" x 32" primaries into a Burns merge collector, 2 1/2" outlet directly into my "muffler". My "muffler" is essentially a 4 1/2" x 30" tube with some spiral baffles and 2 1/2" inlet/outlet. The intake uses a modified 87 lower manifold casting port matched to the engine. The upper manifold uses 4 tubes (1 1/2" and 1 1/4" dia) over the top of the engine to a small dynamic chamber/plenum directly over the oil filler port in the center iron housing. The throttle body copies Tracy's original - a stock second gen 3 throat TB cut down to just 2 ports. The gearbox is Tracy's first RD-1 with 2.17 gears. Prop is a Warnke 68 x 80 (not sure the pitch number is meaningful - everyone seems to measure it differently). On the ground static RPM is about 5350 and is reached at abou= t 2/3 throttle opening. In flight max RPM I've seen is about 5750. The Warnke prop is unique due to the shape. The appearance gets a lot of comments. I'm really hesitant to mess with it and screw it up unless/until = I can say with certainty that there isnt something else I can do with tweakin= g (I'm thinking on the intake side) to improve airflow through the engine. Hard to believe that there isnt more HP to be had when a hacked 2 barrel TB is only 2/3 open and I've hit the limit. But like you say there are a lot o= f variables. Mike -------------------------------------------------- From: "Ed Anderson" > Sent: Monday, February 08, 2010 5:06 AM To: "Rotary motors in aircraft" > Subject: [FlyRotary] Throttle limits was Re: N.A. Renesis to turbo > Hi Mike, > > Several things could be causing the situation you see in advancing your > throttle but getting no increased engine rpm. This is not an uncommon > situation. Ok assuming we are talking naturally aspired engine (no forced > induction), fixed pitch prop and assuming your engine is basically OK (no= t > weak on compression, etc), > > then the most likely cause is you have simply reach the point at which > where the engine is producing all the power it can - given the prop load > it > sees at that moment. Once that point is reached, then advancing the > throttle more does not result in more air flow through the engine and > therefore no increase in power nor rpm. In fact, it can cause the engine > to > run leaner and actually produce less power than a partial closed throttle= . > > It's sort of the chicken and the egg in that you need more power to > produce > more rpm, but power is dependent on air flow - which is dependent on rpm > which dependent on power produced, etc. {:>). But to try to be a bit mor= e > helpful, look at it this way. > > > Basically for every throttle position (at a constant altitude, temp, air > density, etc) there is one associated manifold pressure(air density). > This > manifold pressure is a product of a number of variables, but the most > dominating ones involving the engine are volumetric efficiency, throttle > position and engine rpm. Now your volumetric efficiency is more or less > fixed by the intake/exhaust design so we'll eliminate that for the moment= . > That leaves throttle position and rpm as controllable variables and your > ambient air density as a fixed (for this discussion). > > > We know the engine is a positive displacement pump which displaces the > same > volume once each engine cycle. The power the engine produces in that cycl= e > is limited by the density of the air in the combustion chamber as the > volume > is always a constant (fixed by size of your combustion chamber). The air > density into the combustion chamber is dependent on the air density in th= e > intake manifold. > > So that leaves us with: More throttle =3D higher manifold air density = =3D > =3D more oxygen + More fuel(permits more fuel to be burnt) =3D more powe= r =3D > more rpm. That is until you hit the limit - what limit you say? > > The limit is that once you have opened the throttle plate sufficiently > that > the air density in the intake manifold is equal to ambient air density (o= r > as close as its going to get- given intake losses) - then it will not mak= e > any difference (in power) to advance the throttle further. Once you have > reached that limit, then advancing the throttle further does not further > increase the air density in the manifold and therefore limits the amount > of > fuel you can burn/power you can make. > > Clearly if you have a large throttle body you can reach that point with a > smaller opening of the throttle plate than if you have a small throttle > body. > > As I said - there can be other causes, but this is the one I think most > folks run into. You can find the same situation even on the ground, where > again once the manifold air density =3D ambient air density (or as close = as > your engine Ve will permit) you stop producing power increase even if you > have throttle travel left. > > Therefore if your throttle body is sized so you get max power at 100% > throttle opening a sea level, then with every increase in altitude, you > will > find you have additional throttle travel that produces no increase in > power. > The higher you go in altitude the more throttle travel will be available > that results in no power increase. This is because the ultimate limit is > based on the ambient air density. > > Hope this helped. > > Ed > > > > > Ed Anderson > > Rv-6A N494BW Rotary Powered > > Matthews, NC > > eanderson@carolina.rr.com > > http://www.andersonee.com > > http://www.dmack.net/mazda/index.html > > http://www.flyrotary.com/ > > http://members.cox.net/rogersda/rotary/configs.htm#N494BW > > http://www.rotaryaviation.com/Rotorhead%20Truth.htm > > -----Original Message----- > From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On > Behalf Of Mike Wills > Sent: Sunday, February 07, 2010 12:51 PM > To: Rotary motors in aircraft > Subject: [FlyRotary] Re: N.A. Renesis to turbo > > Don, > > I'm at about 23 hours and am seeing roughly the same performance on my > RV-4 > with a Bruce T built gen 2 13B. My temps are a little cooler. I'm pretty > happy with the performance, but like you say, its not possible to have to= o > much power. But I don't have room for a turbo and intercooler. > > I think there's more power in my NA engine. I'm still a little mystified > by > the fact that at about 1/2 - 2/3 throttle the engine stops making any mor= e > power. But I decided to take several people's advice and just fly it for = a > while. I also think there's more speed in it via some drag reduction. A > turbo would be nice to tame the noise though. > > I'll be interested in seeing how the Burns muffler works out for you. I'm > not willing to dive into any more muffler experiments for the moment sinc= e > my failed trial with the DNA muffler. But sooner or later, and one way or > another I have to quiet this thing down. > > Mike Wills > RV-4 N144MW > > -------------------------------------------------- > From: "Don Wallker" > > Sent: Saturday, February 06, 2010 6:21 PM > To: "Rotary motors in aircraft" > > Subject: [FlyRotary] N.A. Renesis to turbo > >> Dear list, Turbo flyers and especially David Leonard, >> I've 16 flying hours on my RV-8 with a Renesis and all of Tracy's >> stuff > >> and a Catto 76/88. The airplane flys great, just like an RV, no gliding >> time, and about 36 hours on the ground. SPECS >> Full throttle 8,000' 174 mph indicated, 2450 on the prop, water 185, >> oil > >> 205, >> Climb out 110 mph, rate of climb, 1250'/min. Field elevation 5046. >> >> These are not bad numbers, but I would like better. I've been influence= d >> by some of the the local jet jocks who say that there is no such thing a= s >> too much horsepower and they are right! N113BR seems to be performing >> about like a 160-170 HP RV. So I am investigating turboing it! The ide= a >> is to have a little better than sea level performance on take off >> (designed for 210HP N.A.) and turbo normalizing at cruise. Up to 12000' >> would be nice. >> During the air races this year, Dave Leonard showed up and I was very >> impressed by his airplane. He was able to turbo and inter cool it and >> have it all inside an RV cowl, so I'll likely base my installation on >> his. Plus, he has been through the learning curve of 3 or so turbos so >> he > >> knows what to do, what not to do and what would be better if he were to >> do > >> it all over again. >> >> I've spent the afternoon looking through the archives, reading as much a= s >> I can find about turbos, and downloading all the photos I can. Here is >> what I am tentatively planning on doing. >> Get one of Techwelding's Renesis exhaust flanges made from 304 SS and >> have > >> my local waterjet guy copy it and make one out of 321SS. I'll weld 321 >> SS > >> and manifold it together and run it into the bottom of the turbo that >> will sit right in front of the exhaust. The turbo will have additional >> support. Run the turbo outlet air from it through a stock RX-7 inter >> cooler sitting in front of the left cheek opening and then out to the >> right side of the engine, probably routing it under the PSRU and then up >> to a throttle body and manifold. Then four al tubes over the top of the >> engine into a cut down and welded up stock RX-8 intake manifold. The >> exhaust out of the turbo will run down and out in the usual center of th= e >> back of the cowl opening. I am thinking of trying one of Burns Stainles= s >> all SS mufflers. It is basically a glass pack, but instead of glass, >> they > >> are using stainless steel wool and they say it is holding up for the >> rotary racers. They make it any length you want and is about 4 lbs with >> their SS vs 9 lbs with the hushpower 2 I'm using now. The combustion ai= r >> intake to the turbo will be on the aft left side of the cowl via an NACA >> duct opening as Dave's is. >> The oil cooler will have to be moved to under the engine. I will build >> up > >> a fiberglass scoop, probably based on Van's scoop and modify it to have = a >> bigger opening and be farther forward, closer to the prop. I will >> probably have the oil cooler made a little larger (Techwelding) than th= e >> one I have now. >> >> That's the basic idea at this point. I'll finalize my plan, prebuild as >> much as possible before tearing the airplane apart and try for as little >> down time as possible. I'm looking for the list's critique here, plus >> questions that I will have missed. The following are a list of question= s >> that I have. >> 1. Which turbo should I use, which orientation and who should I use to d= o >> the work, plus what is the approximate price? TO4 hybrid? Dave and >> Steve Brooks mention BNR turbo as a modifier. Who manufactures the >> turbo? >> 2. What is the ideal situation with a waste gate? Full open or not, or, >> or? >> 3. I read about a N.O.oil line solenoid to the turbo bearings. I assume >> that if the Turbo fails, you turn it on to the N.C. position to prevent >> oil from being pumped down your exhaust? I assume the oil that is used >> is > >> routed back to the sump. >> 4. What size exhaust is optimum? It seems Dave is running 2.5 inch. >> 5. What size throttle body should I use and what would be a good one? >> One > >> throttle body or two? 4. What size injectors should I use, and where >> should the secondaries be placed? Dave is using 480cc and staging is a= t >> 32 inches. Are you using the same for the primaries and is there an idl= e >> problem with the larger injectors? >> 5. Anyone out there turboing a Renesis? Anyone flying one? >> 6. My compression is 9.7 to 1. Any problems with this higher >> compression ratio as long as I use an inter cooler and keep the boost no >> higher than 35"? >> And lot more questions, but that's all I can think of now. >> So If any of you can add any thought, let me know. >> >> Don Walker >> >> -- >> Homepage: http://www.flyrotary.com/ >> Archive and UnSub: >> http://mail.lancaironline.net:81/lists/flyrotary/List.html >> > > > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: > http://mail.lancaironline.net:81/lists/flyrotary/List.html > > __________ Information from ESET NOD32 Antivirus, version of virus > signature > database 3267 (20080714) __________ > > The message was checked by ESET NOD32 Antivirus. > > http://www.eset.com > > > > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: > http://mail.lancaironline.net:81/lists/flyrotary/List.html > -- Homepage: http://www.flyrotary.com/ Archive and UnSub: http://mail.lancaironline.net:81/lists/flyrotary/List.html __________ Information from ESET NOD32 Antivirus, version of virus signatur= e database 3267 (20080714) __________ The message was checked by ESET NOD32 Antivirus. http://www.eset.com -- Homepage: http://www.flyrotary.com/ Archive and UnSub: http://mail.lancaironline.net:81/lists/flyrotary/List.= html This message, and the documents attached hereto, is intended only for the a= ddressee and may contain privileged or confidential information. 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Hi Mike, for reference my throttle body and intak= e are very similar to yours; i.e., I copied Tracy's original dynamic intake= and used the cut-down (3 to 2 port) Mazda throttle body … see attach= ed.

With my 2.85:1 reduction unit there is also a bit= of travel left without further increase in power; however, it isn't 1/3 it= 's more like 1/5 or 1/6; i.e. maybe the last 0.75” to 1" of trav= el out of 5" total.

My installation differs from yours with regards t= o exhaust, prop and reduction drive ... so again many variables and about a= ll I can conclude is it’s not all attributed your throttle body or in= take.

Jeff

 

 

 

From: Rotary m= otors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Ed Anderson
Sent: Tuesday, February 09, 2010 10:00 AM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: rpm vs Power was : Throttle limits was Re: = N.A. Renesis to turbo

 

Good point, Tracy

 

I had one instance where I my static and top end rpm were essen= tially the same.  I had a static of 6000 rpm and a top end in flight o= f around 6100 rpm.  But, in my case, the cause was very obvious – my muffler of the time was lim= iting the top end to my static rpm.  Once I changed the muffler - top = end rpm was again up around 6800 rpm.

 

Ed

 

From: Rotary m= otors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Tracy Crook
Sent: Tuesday, February 09, 2010 8:21 AM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: rpm vs Power was : Throttle limits was Re: = N.A. Renesis to turbo

 

Ed's experience prett= y much matches my own when changing gear drive ratios.  A little more = top end.  (Sun 100 results were 209 mph w/ 2.176 drive vs 217.5 mph th= e next year with 2.85 drive.)   Takeoff & climb performance improved dramatically though.  It's not an inexpensive ch= ange though.

What does mystify me is the small difference between Mike's static & to= p end rpm.  I got an 1100 rpm difference.  5200 vs 6300 with a 68= - 81 Performance prop.

Another detail I'm not certain about is whether Mike's manifold pressure is= or is not increasing during that last 1/3 - 1/2 throttle travel with no po= wer increase.  Seems like he said it did go up but I'm not sure. = If it is going up, there is still something unexplained going on.  What was the MP doing Mike?  Was it at fu= ll ambient at the point where the rpm stopped increasing?

Tracy

On Tue, Feb 9, 2010 at 12:12 AM, Ed Anderson <eanderson@carolina.rr.com>= wrote:

Well, Mike, just for comparison, when I had a 2.17:1= and a 68 x72
Performance prop, 5200 -5400 rpm on a nominal 70deg day was what I got for<= br> static.

While I don't claim my set up was the best in the land, I think it was a pretty fair set up.  So I would say you are doing just fine.

It does not matter how large a throttle body you have when the manifold air=
density hits ambient or as close as it can given any losses in the inductio= n
system - that's it.  You can continue to open the throttle body, but y= ou
will not get any more power. However, there is a way!

Looking at some of the variables in the power equation we have:

Power(HP) =3D Torque * rpm/ 5250, swapping some variables around we get:
RPM =3D Power/torque.  So this indicates the rpm can increase if eithe= r the
power is increased or the torque is decreased. Well, it's difficult to
increase the power by itself(unless you go to forced induction or nitrous oxide)

But one way to get more rpm (and ultimately more power)  is to lower t= he
Torque load on the engine.  Decreasing the Torque permits more engine = rpm
even if power did not increase.  However we know that more rpm =3D mor= e air =3D
more power. The torque load on the engine caused by the prop decreases as your gear ratio increases.


By going to a 2.85:1 gear ratio that would reduce the load on the engine by=
approx 25% (assuming the same prop at the same static rpm).  Now the r= pm
power relationship were linear (which it is not with a prop as the load) then I should have gotten around 6650 rpm with the new gear box - well not<= br> really - due to the cube root relationship between prop rpm and power, it will be much less of an increase and due to the fact I put on a larger
diameter prop.

But in any case, all this theory aside,  with the 2.85 and 74 x88 prop= I now
get engine 6000 - 6200 rpm static or about an 13% increase in rpm.   S= o
that's using use the same intake, throttle body and engine for both.  = But
now because the engine can turn faster (lesser prop load at any specific rpm).

Now the fact the engine is turning faster means it takes more airflow to maintain the same (ambient) air density in the manifold. This is because th= e
higher engine rpm can "suck" that manifold volume (which didn't c= hange) down
faster than it did before.  This in turn means that the throttle posit= ion
has to be more open to let a sufficient increase in air flow need to achiev= e
and maintain that (hopefully) ambient air density in the manifold.

So from what you are reporting, I really don't see anything poor about your=
performance with your set up. In fact, it's pretty good.

The new set up gave a noticeable benefit in take off performance (and I do<= br> mean noticeable).  However, the top end was relatively unaffected - al= though
I did measure an approx 4 mph increase in top aircraft speed.

In any case, that is my experience.

FWIW

Ed Anderson

Rv-6A N494BW Rotary Powered

Matthews, NC

eanderson@carolina.rr.com<= br>
http://www.anderson= ee.com

http://= www.dmack.net/mazda/index.html

http://www.flyrotar= y.com/

http://members.cox.net/rogersda/rotary/configs.htm#N494BW<= br>
http://www.rotaryaviation.com/Rotorhead%20Truth.htm

-----Original Message-----
From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On
Behalf Of Mike Wills
Sent: Monday, February 08, 2010 10:36 PM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: Throttle limits was Re: N.A. Renesis to turbo

Thanks Ed. Mentioned this a few months ago and was convinced at least for the moment, to just fly the plane as is. So that's what I have been doing.<= br>
To recap, my engine is an NA 13B built by Bruce Turrentine. It is a second<= br> gen engine with Turbo rotor housings (no exhaust splitter) and high
compression NA rotors. The exhaust uses 1 3/4" x 32" primaries in= to a Burns
merge collector, 2 1/2" outlet directly into my "muffler". M= y "muffler" is
essentially a 4 1/2" x 30" tube with some spiral baffles and 2 1/= 2"
inlet/outlet. The intake uses a modified 87 lower manifold casting port
matched to the engine. The upper manifold uses 4 tubes (1 1/2" and 1 1= /4"
dia) over the top of the engine to a small dynamic chamber/plenum directly<= br> over the oil filler port in the center iron housing. The throttle body
copies Tracy's original - a stock second gen 3 throat TB cut down to just 2=
ports.

The gearbox is Tracy's first RD-1 with 2.17 gears. Prop is a Warnke 68 x 80=
(not sure the pitch number is meaningful - everyone seems to measure it
differently). On the ground static RPM is about 5350 and is reached at abou= t

2/3 throttle opening. In flight max RPM I've seen is about 5750.

The Warnke prop is unique due to the shape. The appearance gets a lot of comments. I'm really hesitant to mess with it and screw it up unless/until = I

can say with certainty that there isnt something else I can do with tweakin= g

(I'm thinking on the intake side) to improve airflow through the engine.
Hard to believe that there isnt more HP to be had when a hacked 2 barrel TB=
is only 2/3 open and I've hit the limit. But like you say there are a lot o= f

variables.

Mike

--------------------------------------------------
From: "Ed Anderson" <eanderson@carolina.rr.com>
Sent: Monday, February 08, 2010 5:06 AM
To: "Rotary motors in aircraft" <flyrotary@lancaironline.net>
Subject: [FlyRotary] Throttle limits was  Re: N.A. Renesis to turbo
> Hi Mike,
>
> Several things could be causing the situation you see in advancing you= r
> throttle but getting no increased engine rpm.  This is not an unc= ommon
> situation. Ok assuming we are talking naturally aspired engine (no for= ced
> induction), fixed pitch prop and assuming your engine is basically OK = (not
> weak on compression, etc),
>
> then the most  likely cause is you have simply reach the point at= which
> where the engine is producing all the power it can - given the prop lo= ad
> it
> sees at that moment.  Once that point is reached, then advancing = the
> throttle more does not result in more air flow through the engine and<= br> > therefore no increase in power nor rpm.  In fact, it can cause th= e engine
> to
> run leaner and actually produce less power than a partial closed throt= tle.
>
> It's sort of the chicken and the egg in that you need more power to > produce
> more rpm, but power is dependent on air flow - which is dependent on r= pm
> which dependent on power produced, etc. {:>).  But to try to b= e a bit more
> helpful, look at it this way.
>
>
> Basically for every throttle position (at a constant altitude, temp, a= ir
> density, etc) there is one associated manifold pressure(air density).<= br> > This
> manifold pressure is a product of a number of variables, but the most<= br> > dominating ones involving the engine are volumetric efficiency,  = throttle
> position and engine rpm.  Now your volumetric efficiency is more = or less
> fixed by the intake/exhaust design so we'll eliminate that for the mom= ent.
> That leaves throttle position and rpm as controllable variables and yo= ur
> ambient air density as a fixed (for this discussion).
>
>
> We know the engine is a positive displacement pump which displaces the=
> same
> volume once each engine cycle. The power the engine produces in that c= ycle
> is limited by the density of the air in the combustion chamber as the<= br> > volume
> is always a constant (fixed by size of your combustion chamber).  = ;The air
> density into the combustion chamber is dependent on the air density in= the
> intake manifold.
>
> So that leaves us with:  More throttle =3D higher manifold air de= nsity =3D
>  =3D more oxygen + More fuel(permits more fuel to be burnt) = =3D more power =3D
> more rpm.  That is until you hit the limit - what limit you say?<= br> >
> The limit is that once you have opened the throttle plate sufficiently=
> that
> the air density in the intake manifold is equal to ambient air density= (or
> as close as its going to get- given intake losses) - then it will not = make
> any difference (in power) to advance the throttle further.  Once = you have
> reached that limit, then advancing the throttle further does not furth= er
> increase the air density in the manifold and therefore limits the amou= nt
> of
> fuel you can burn/power you can make.
>
> Clearly if you have a large throttle body you can reach that point wit= h a
> smaller opening of the throttle plate than if you have a small throttl= e
> body.
>
> As I said - there can be other causes, but this is the one I think mos= t
> folks run into. You can find the same situation even on the ground, wh= ere
> again once the manifold air density =3D ambient air density (or as clo= se as
> your engine Ve will permit) you stop producing power increase even if = you
> have throttle travel left.
>
> Therefore if your throttle body is sized so you get max power at 100%<= br> > throttle opening a sea level, then with every increase in altitude, yo= u
> will
> find you have additional throttle travel that produces no increase in<= br> > power.
> The higher you go in altitude the more throttle travel will be availab= le
> that results in no power increase.  This is because the ultimate = limit is
> based on the ambient air density.
>
> Hope this helped.
>
> Ed
>
>
>
>
> Ed Anderson
>
> Rv-6A N494BW Rotary Powered
>
> Matthews, NC
>
> eanderson@carolina.rr.com=
>
> http://www.and= ersonee.com
>
> ht= tp://www.dmack.net/mazda/index.html
>
> http://www.fly= rotary.com/
>
> http://members.cox.net/rogersda/rotary/configs.htm#N494BW
>
> http://www.rotaryaviation.com/Rotorhead%20Truth.htm
>
> -----Original Message-----
> From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On
> Behalf Of Mike Wills
> Sent: Sunday, February 07, 2010 12:51 PM
> To: Rotary motors in aircraft
> Subject: [FlyRotary] Re: N.A. Renesis to turbo
>
> Don,
>
> I'm at about 23 hours and am seeing roughly the same performance on my=
> RV-4
> with a Bruce T built gen 2 13B. My temps are a little cooler. I'm pret= ty
> happy with the performance, but like you say, its not possible to have= too
> much power. But I don't have room for a turbo and intercooler.
>
> I think there's more power in my NA engine. I'm still a little mystifi= ed
> by
> the fact that at about 1/2 - 2/3 throttle the engine stops making any = more
> power. But I decided to take several people's advice and just fly it f= or a
> while. I also think there's more speed in it via some drag reduction. = A
> turbo would be nice to tame the noise though.
>
> I'll be interested in seeing how the Burns muffler works out for you. = I'm
> not willing to dive into any more muffler experiments for the moment s= ince
> my failed trial with the DNA muffler. But sooner or later, and one way= or
> another I have to quiet this thing down.
>
> Mike Wills
> RV-4 N144MW
>
> --------------------------------------------------
> From: "Don Wallker" <drwalker@gbis.com>
> Sent: Saturday, February 06, 2010 6:21 PM
> To: "Rotary motors in aircraft" <flyrotary@lancaironline.net>
> Subject: [FlyRotary] N.A. Renesis to turbo
>
>> Dear list, Turbo flyers and especially David Leonard,
>>    I've 16 flying hours on my RV-8 with a Renesis and al= l of Tracy's
>> stuff
>
>> and a Catto 76/88.  The airplane flys great, just like an RV,= no gliding
>> time, and about 36 hours on the ground. SPECS
>> Full throttle 8,000'   174 mph indicated, 2450 on the prop, w= ater 185,
>> oil
>
>> 205,
>> Climb out 110 mph, rate of climb, 1250'/min.  Field elevation= 5046.
>>
>> These are not bad numbers, but I would like better.  I've bee= n influenced
>> by some of the the local jet jocks who say that there is no such t= hing as
>> too much horsepower and they are right!   N113BR seems to be = performing
>> about like a 160-170 HP RV.  So I am investigating turboing i= t!  The idea
>> is to have a little better than sea level performance on take off<= br> >> (designed for 210HP N.A.) and turbo normalizing at cruise.  U= p to 12000'
>> would be nice.
>> During the air races this year, Dave Leonard showed up and I was v= ery
>> impressed by his airplane.  He was able to turbo and inter co= ol it and
>> have it all inside an RV cowl, so I'll  likely base my instal= lation on
>> his.  Plus, he has been through the learning curve of 3 or so= turbos so
>> he
>
>> knows what to do, what not to do and what would be better if he we= re to
>> do
>
>> it all over again.
>>
>> I've spent the afternoon looking through the archives, reading as = much as
>> I can find about turbos, and downloading all the photos I can. &nb= sp;Here is
>> what I am tentatively planning  on doing.
>> Get one of Techwelding's Renesis exhaust flanges made from 304 SS = and
>> have
>
>> my local waterjet guy copy it and make one out of 321SS.  I'l= l weld 321
>> SS
>
>> and  manifold it together and run it into the bottom of the t= urbo that
>> will sit right in front of the exhaust.  The turbo will have = additional
>> support.  Run the turbo outlet air from it through a stock RX= -7 inter
>> cooler sitting in front of the left cheek opening and then out to = the
>> right side of the engine, probably routing it under the PSRU and t= hen up
>> to a throttle body and manifold.  Then four al tubes over the= top of the
>> engine into a cut down and welded up stock RX-8  intake manif= old.  The
>> exhaust out of the turbo will run down and out in the usual center= of the
>> back of the cowl opening.  I am thinking of trying one of Bur= ns Stainless
>> all SS mufflers.  It is basically a glass pack, but instead o= f glass,
>> they
>
>> are using stainless steel wool and they say it is holding up for t= he
>> rotary racers.  They make it any length you want and is about= 4 lbs with
>> their SS vs 9 lbs with the hushpower 2 I'm using now.  The co= mbustion air
>> intake to the turbo will be on the aft left side of the cowl via a= n NACA
>> duct opening as Dave's is.
>> The oil cooler will have to be moved to under the engine.  I = will build
>> up
>
>> a fiberglass scoop, probably based on Van's scoop and modify it to= have a
>> bigger opening and be farther forward, closer to the prop.  I= will
>> probably  have the oil cooler made a little larger (Techweldi= ng) than the
>> one I have now.
>>
>> That's the basic idea at this point.  I'll finalize my plan, = prebuild as
>> much as possible before tearing the airplane apart and try for as = little
>> down time as possible.  I'm looking for the list's critique h= ere, plus
>> questions that I will have missed.  The following are a list = of questions
>> that I have.
>> 1. Which turbo should I use, which orientation and who should I us= e to do
>> the work, plus what is the approximate price?   TO4 hybrid? &= nbsp;Dave and
>> Steve Brooks mention BNR turbo as a modifier.  Who manufactur= es the
>> turbo?
>> 2. What is the ideal situation with a waste gate?  Full open = or not, or,
>> or?
>> 3. I read about a N.O.oil line solenoid to the turbo bearings. &nb= sp;I assume
>> that if the Turbo fails, you turn it on to the N.C. position to pr= event
>> oil from being pumped down your exhaust?  I assume the oil th= at is used
>> is
>
>> routed back to the sump.
>> 4. What size exhaust is optimum?  It seems Dave is running 2.= 5 inch.
>> 5.  What size throttle body should I use and what would be a = good one?
>> One
>
>> throttle body or two? 4.  What size injectors should I use, a= nd where
>> should the secondaries be placed?   Dave is using 480cc and s= taging is at
>> 32 inches.  Are you using the same for the primaries and is t= here an idle
>> problem with the larger injectors?
>> 5.  Anyone out there turboing a Renesis?  Anyone flying = one?
>> 6.  My compression is 9.7 to 1.   Any problems with this= higher
>> compression ratio as long as I use an inter cooler and keep the bo= ost no
>> higher than 35"?
>> And lot more questions, but that's all I can think of now.
>> So If any of you can add any thought, let me know.
>>
>> Don Walker
>>
>> --
>> Homepage:  http://www.flyrotary.com/
>> Archive and UnSub:
>> http://mail.lancaironline.net:81/lists/flyrotary/List.html
>>
>
>
> --
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