X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from smtp101.sbc.mail.re3.yahoo.com ([66.196.96.84] verified) by logan.com (CommuniGate Pro SMTP 5.3.2) with SMTP id 4124328 for flyrotary@lancaironline.net; Sat, 13 Feb 2010 19:05:56 -0500 Received-SPF: none receiver=logan.com; client-ip=66.196.96.84; envelope-from=bryanwinberry@bellsouth.net Received: (qmail 95486 invoked from network); 14 Feb 2010 00:05:21 -0000 Received: from acer7fbfa7e2f7 (bryanwinberry@74.232.110.180 with login) by smtp101.sbc.mail.re3.yahoo.com with SMTP; 13 Feb 2010 16:05:19 -0800 PST X-Yahoo-SMTP: OSuEAS2swBAaBd4uKxevNivslbMG7JXpWjAWZVmoYyRm6qcW_W2VUA-- X-YMail-OSG: _8JcRx4VM1lkDsE6xVJMKnWWLsxLA_SXtzplOoUeVGyYt1N1csdonjPa4ruITiYqwJpiCnYH0N7LmIAx3piSvbtoRQEu_UGtuvHcp.jW0yRDv_OU8SLSAzfYFyBLcydQhw5mL4QQCsjBRlCmuLPz0dybIIZbvEKGhcTqYyeKRkT4.gd.EwHSeUkesguq6rCw6.YuMXxh4X_pwv_lccX2K5Kw4nf6k3r9PXh2wekGBMHKAGFlnjMxg0ipmWSARTVeGDI7inQPJbzFOTeaZ6OWJjA1tVA8Yi_.nCDVYz.Q8X91T1yseeT1NePA_Hfp5c4QiaJdw2oaKiH7kj0Q2NIeI6QRC1X6huiS18YSGTeaUO9wtTHOxbPMqTg04zW8Tz_QwbOcKalBkNrYs7Oi4F.navhgWsNgdhcvn_WJ1vw- X-Yahoo-Newman-Property: ymail-3 From: "Bryan Winberry" To: "'Rotary motors in aircraft'" References: Subject: RE: [FlyRotary] Throttle limits was Re: N.A. Renesis to turbo Date: Sat, 13 Feb 2010 19:05:18 -0500 Message-ID: <9E5B5482B5984B1AB54BD166A0B97266@acer7fbfa7e2f7> MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_0057_01CAACDF.7BF1F760" X-Mailer: Microsoft Office Outlook 11 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.5579 Thread-Index: AcqsK7L92hUeW3Z5QJeZCJs4Y1pKNAA3WvzA In-Reply-To: This is a multi-part message in MIME format. ------=_NextPart_000_0057_01CAACDF.7BF1F760 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable Ed, Excellent take on throttle travel. You have a good knack for explaining things that simple minds can grasp. Oh, and a belated Happy Birthday from Georgia! Bryan=20 =20 _____ =20 From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Ed Anderson Sent: Friday, February 12, 2010 4:38 PM To: Rotary motors in aircraft Subject: [FlyRotary] Throttle limits was Re: N.A. Renesis to turbo =20 Bill, if Dennis had a TB just big enough that it exactly provided 100% power at sea level, then as he increases in altitude, he will find more = and more throttle travel that does nothing to increase power. This is = because it takes less and less throttle plate opening to provide sufficient = airflow for the pressure/air density in the manifold to reach the ambient pressure/air density (ambient density is decreasing with altitude). = Since that air density is less than at sea level, it requires less throttle opening to reach than at sea level. =20 The position of the throttle plate affects only the air flow volume (not = the density of that air airflow), but the amount of air flow volume does determine the air density in the manifold. The external atmospheric pressure is of course what is forcing the air through the throttle body = =96 The less air pressure at altitude means less air is flowing through the = TB as you gain altitude. Remember even though to simply the verbiage - we often talk of the engine =93sucking=94 but of course it does not. The = engine simply opens its ports and whatever pressure is in the manifold forces = that air into the essentially empty combustion chamber.=20 =20 Think of it this way, there are two ways you can have ambient air = density in your intake manifold. Those two ways are with the throttle open or the throttle closed =96 a contradiction? Not, so. You may have ambient air pressure/density in the manifold when the engine is running and TB open sufficiently to provide ambient pressure in the manifold OR when the = engine is not running. =20 When the engine is stopped - you also have ambient pressure in your = intake even with your throttle 99.99 % closed because the engine is not = =93sucking=94 any air out of the manifold when stopped. So a small leak in the = throttle bottle is sufficient for the manifold pressure to reach and maintain = ambient when the engine is not running.=20 =20 What Dennis has done with his DIE intake does not change this factor, = but what the pulse in the intake does when it reaches the other end of the intake manifold (note how his intakes are tied together so the pulse can travel from one intake port of one rotor to the intake port of the = second rotor) is briefly create a localized pressure increase in the intake manifold right at the intake port as it is open. This in effect shoves = more mixture into the combustion chamber =96 in effect it is a very brief supercharger effect. It only lasts for milliseconds and therefore you = don=92t get the same power increase that you would if you had a turbocharger = pushing in denser air the entire time the intake is open. On the other hand = you don=92t have 30-50 lbs more weight and for basically no more than = fabricating your intake different =96 it=92s basically a free lunch.=20 =20 But, as Dennis will tell you - doing the analysis to get the equations = so you get dimension correct for the effect =96 can give you a headache = {:>) =96 right Dennis??. =20 So, anyhow, back the throttle travel, if your TB is larger than needed = to reach 100% power at sea level, then you would also find =93excess=94 = throttle travel sitting on the ground with the engine running at WOT. Once the throttle is opened sufficient for manifold pressure to reach ambient, = then opening it further will provide no increase in power. You have in the vernacular- =93Maxed Out!=94 {:>) =20 Once the throttle plate is open sufficient to permit the manifold pressure/air density to reach ambient conditions =96 no further opening = will produce any more power even though you may have 5=94 of throttle travel = and 50% more throttle plate opening to go. =20 =20 =20 Ed =20 =20 =20 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 =20 _____ =20 From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Bill Bradburry Sent: Friday, February 12, 2010 3:33 PM To: Rotary motors in aircraft Subject: [FlyRotary] Re: rpm vs Power was : Throttle limits was Re: N.A. Renesis to turbo =20 Thanks, Dennis, It sounds like you still have a little unused throttle travel even with = the new intake. Can you provide design measurements for your new intake? I ask only if = you have no plans to make and sell it. =20 Bill B=20 =20 _____ =20 From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Dennis Haverlah Sent: Friday, February 12, 2010 2:20 PM To: Rotary motors in aircraft Subject: [FlyRotary] Re: rpm vs Power was : Throttle limits was Re: N.A. Renesis to turbo I used the same 65 mm Mustang throttle body on both my original and new intakes. If I remember correctly, I believe I had a longer unused throttle travel with the original intake but I never measured it. I = don't know the static rpm increase with the new intake - probably have that in = my notes some where but my max. rpm at high altitude (8,000 - 10,000) = increased 400-500 rpm. I estimated I went from 165 -170 HP with the old intake to about 185 HP with the new intake. This in in line with Ed Anderson's = recent note that Mazda got about a 16% power increase at 6000 rpm with the DIE effect. I felt much improved acceleration the first time I took off = with the new intake.=20 the new intake is based on dynamic intake effect (DIE) where the = closing of an intake valve caused the moving intake air to bounce off the valve creating a pressure wave. The wave travels at the speed of sound to the other intake valve and arrives there just before that valve closes. = This increases the amount of air and fuel that enters the combustion chamber. (As we know the rotary has no valves but uses the sides of the rotor for opening and closing the intakes.) I designed my intake to give max. performance at 6300 rpm. If I had cut down my prop to 74" it would give me more clearance for the prop on my RV-7A and increase my top end rpm. Max rpm is about 6400 = rpm with the new intake and the 76" prop. I'm really not needing higher RPM now. Dennis Haverlah Bill Bradburry wrote: Dennis, Did your static rpm increase with the new manifold? How much? Did you before and do you now have any unused throttle travel like Mike = describes? Are you using the same throttle body on the new manifold? What is the = MM opening of the Mustang body? My manifold is very similar to your old one. My tubes are cut just = above the injector bosses, which makes them a little (maybe an inch) shorter = than your old ones. I have a 76 X 88 Performance prop which I am considering having cut down to 74=94 like Tracy and Ed when I send it in for final = finish. I am using an aftermarket throttle body that is 75MM in throat diameter. This is the same size as the stock Renesis throttle body which is why I picked it. I had intended to use the Renesis body, but didn=92t wait = for Tracy to get the fly by wire done. I am not flying, but my static is 52-5300 rpm and I have a lot of throttle left at that rpm. The last probably =BC of the travel is not used. Bill B =20 _____ =20 =20 =20 __________ Information from ESET NOD32 Antivirus, version of virus = signature database 3267 (20080714) __________ The message was checked by ESET NOD32 Antivirus. http://www.eset.com ------=_NextPart_000_0057_01CAACDF.7BF1F760 Content-Type: text/html; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable

Ed,

Excellent take on throttle travel. = =A0You have a good knack for explaining things that simple minds can = grasp.

Oh, and a belated Happy Birthday = from Georgia!

Bryan

 

From: Rotary motors in = aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Ed Anderson
Sent: Friday, February = 12, 2010 4:38 PM
To: Rotary motors in aircraft
Subject: [FlyRotary] = Throttle limits was Re: N.A. Renesis to turbo

 

Bill, if Dennis had a TB just big enough  that it = exactly provided 100% power at sea = level, then as he increases in altitude, he will find more and more throttle = travel that does nothing to increase power.  This is because it takes less = and less throttle plate opening to provide sufficient airflow for the = pressure/air density in the manifold to reach the ambient pressure/air density = (ambient density is decreasing with altitude).  Since that air density is = less than at sea level, it requires less throttle opening to reach than at sea = level.

 

The position of the throttle plate = affects only the air flow volume (not the density of that air airflow), but the = amount of air flow volume does determine the air density in the manifold.  = The external atmospheric pressure is of course what is forcing the air through the = throttle body – The less air pressure at altitude means less air is flowing through the TB as you gain altitude.  Remember even though to = simply the verbiage - we often talk of the engine “sucking” but of = course it does not.  The engine simply opens its ports and whatever pressure = is in the manifold  forces that air into the essentially empty combustion chamber.

 

Think of it this way, there are two = ways you can have ambient air density in your intake manifold. Those two ways = are with the throttle open or the throttle closed – a = contradiction?  Not, so.  You may have ambient air pressure/density in the manifold = when the engine is running and TB open sufficiently to provide ambient = pressure in the manifold OR when the = engine is not running.

 

When the engine is stopped - you = also have ambient pressure in your intake even with your throttle 99.99 % closed = because the engine is not “sucking” any air out of the manifold when stopped.  So a small leak in the throttle bottle is sufficient for = the manifold pressure to reach and maintain ambient when the engine is not = running.

 

What Dennis has done with his DIE = intake does not change this factor, but what the pulse in the intake does when = it reaches the other end of the intake manifold (note how his intakes are = tied together so the pulse can travel from one intake port of one rotor to = the intake port of the second rotor) is briefly create a localized pressure increase in the intake manifold right at the intake port as it is = open.  This in effect shoves more mixture into the combustion chamber – = in effect it is a very brief supercharger effect.  It only lasts for milliseconds and therefore you don’t get the same power increase = that you would if you had a turbocharger pushing in denser air the entire time = the intake is open.   On the other hand you don’t have 30-50 = lbs more weight and for basically no more than fabricating your intake = different – it’s basically a free lunch.

 

 But, as Dennis will tell you = - doing the analysis to get the equations so you get dimension correct for the = effect – can give you a headache {:>) – right = Dennis??.

 

So, anyhow, back the throttle = travel, if your TB is larger than = needed to reach 100% power at sea = level, then you would also find “excess” throttle travel sitting on the = ground with the engine running at WOT.  Once the throttle is opened = sufficient for manifold pressure to reach ambient, then opening it further will = provide no increase in power.  You have in the vernacular- “Maxed Out!” = {:>)

 

Once the throttle plate is open = sufficient to permit the manifold pressure/air density to reach ambient conditions = – no further opening will produce any more power even though you may have 5” of throttle travel and 50% more throttle plate opening to = go.

 

 

 

Ed

 

 

 

From: Rotary motors in = aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Bill Bradburry
Sent: Friday, February = 12, 2010 3:33 PM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: = rpm vs Power was : Throttle limits was Re: N.A. Renesis to = turbo

 

Thanks, Dennis,

It sounds like you still have a little unused = throttle travel even with the new intake.

Can you provide design measurements for your = new intake?  I ask only if you have no plans to make and sell = it.

 

Bill B 

 

From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Dennis Haverlah
Sent: Friday, February = 12, 2010 2:20 PM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: = rpm vs Power was : Throttle limits was Re: N.A. Renesis to = turbo

I used the = same 65 mm Mustang throttle body on both my original and new intakes.  = If  I remember correctly, I believe I had a longer  unused throttle = travel with the original intake but I never measured it.  I don't know the = static rpm increase with the new intake - probably have that in my notes some where = but my max. rpm at high altitude (8,000 - 10,000) increased 400-500 rpm.  = I estimated I went from 165 -170 HP with the old intake to about 185 HP = with the new intake.  This in in line with Ed Anderson's recent note that = Mazda got about a 16% power increase at 6000 rpm with the DIE effect.  I felt = much improved acceleration the first time I took off with the new intake. =

the new intake is based on dynamic = intake effect  (DIE) where the closing of an intake valve = caused the moving intake air to bounce off the valve creating a pressure = wave.  The wave travels at the speed of sound to the other intake valve and arrives = there just before that valve closes.  This increases the amount of air = and fuel that enters the combustion chamber.  (As we know the rotary has no = valves but uses the sides of the rotor for opening and closing the = intakes.)  I designed my intake to give max. performance at 6300 rpm.

If I had cut down my prop to 74" it would give me more clearance = for the prop on my RV-7A and increase my top end rpm.   Max rpm is = about 6400 rpm with the new intake and the 76" prop.  I'm really not = needing higher RPM now.

Dennis Haverlah

Bill Bradburry wrote:

Dennis,<= /font>

Did your static rpm increase with the new manifold?  How much?  Did you before and do you now have any = unused throttle travel like Mike describes?   Are you using the same throttle body on the new manifold?  What is the MM opening of the = Mustang body?

My manifold is very similar to your old = one.  My tubes are cut just above the injector bosses, which makes them a little = (maybe an inch) shorter than your old ones.  I have a 76 X 88 Performance = prop which I am considering having cut down to 74” like Tracy and Ed = when I send it in for final finish.  I am using an aftermarket throttle = body that is 75MM in throat diameter.  This is the same size as the stock = Renesis throttle body which is why I picked it.  I had intended to use the = Renesis body, but didn’t wait for Tracy to get the fly by wire done.  I am not flying, but my static is = 52-5300 rpm and I have a lot of throttle left at that rpm.  The last = probably =BC of the travel is not used.

Bill B

 

 



__________ Information from ESET NOD32 Antivirus, version of virus = signature database 3267 (20080714) __________

The message was checked by ESET NOD32 Antivirus.

http://www.eset.com

------=_NextPart_000_0057_01CAACDF.7BF1F760--