Mailing List flyrotary@lancaironline.net Message #50563
From: George Lendich <lendich@aanet.com.au>
Subject: Re: [FlyRotary] Re: Turbo Planning
Date: Fri, 26 Mar 2010 15:25:27 +1000
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Mike,
Your a hard man, however I do agree with both the Mazdatrix and Powersport results and would expect their operating at optimum configuration and 100% VE.
 
The question in my mind will we all achieve this in our less than perfect installations - probably not.
 
I can't remember exactly but powersport was running two PP sizes, 38mm or 40mm early version and the later 44mm. I believe Bill Jepson is awaiting the results of a more recent 44mm dyno run. That 210hp may be the old 44mm HP numbers - can't remember exactly. Then again it may be the smaller inlet as they were running 6,000 for take-off RPM. A smaller PP will give greater inlet speeds reflecting in VE.
George ( down under)
Sorry, not buying it Bill. If you are going to quote speeds here, quote speeds, not calculated speeds based on so many variables that the end result is meaningless. That sounds like something we'd see on the other list, not here. As far as I know, Don's best reported speed is 174 IAS (and IAS is not all that meaningful either). Based on performance that Don has actually reported his performance is roughly equivalent to mine (and I'm both prop and gearing limited). His performance may have improved since he reported those numbers. In any case I'd prefer to stick to facts.
 
Speaking of the other list, Paul has video of a PP Renesis on a dyno  at Mazdatrix cranking out near 250HP @7500RPM. And he had the dyno sheet to prove it. Powersport claimed 210HP at 2700 prop RPM (their reduction ratio was around 2.2; roughly 6000 engine RPM). I believe they also had dyno data to prove it. I'm anxious to hear how Mark Stietle's PP 20B performs.
 
Mike Wills

Sent: Thursday, March 25, 2010 6:25 AM
Subject: [FlyRotary] Re: Turbo Planning

Mike,

Don didn’t report speed.  I took his pitch and rpm and figured it.  That speed at cruise is what he would get with no slippage or “lift” from the prop.  Most of the folks with the Catto are actually getting higher speeds than would be calculated which indicates that the prop is producing “lift”, not slippage. 

 

But his engine rpm with that big prop are higher than any I have seen.  With the rotary, rpm = horsepower.  If you aint making the rpm, you aint making the horsepower.  It doesn’t seem to matter what you have done to the engine…ported, PP, turbo, supercharger.  If you look at the dyno charts that are all over the web, you will see that torque is pretty flat after about 4K, about 150 ft lbs.  The horsepower is around 150 at 6K, maybe 180 at 7K, and 200 at 7.5K.  You can get more horsepower than that, but only if you scream it up to 8K  or 8.5K.  All the charts I have seen are within 10 horsepower of each other at all rpms.  The difference in total horsepower is always a higher max rpm.

 

We all talk about wanting to cruise at 5800 and make 200 horsepower…it aint happening!  Not with the rotary.

 

Bill B

 


From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Mike Wills
Sent: Thursday, March 25, 2010 1:17 AM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: Turbo Planning

Bill,

 

I went back and looked at Don's previous post. Saw reference to climb performance, RPMs, and temps, but no speed numbers. Has he previously reported cruise speeds over 200? Last post from him that I saw with any speed numbers reported 174MPH IAS at 8000. If he's over 200 now, wow those are good numbers!

 

Mike Wills

 

Sent: Wednesday, March 24, 2010 9:15 PM

Subject: [FlyRotary] Re: Turbo Planning

 

Those are the best numbers I have seen with anyone with a Renesis so far.  In fact, I have not heard of numbers that good on any 13B.  Don is getting over 200 MPH with a cruise prop and climbing at over 1400 fpm with it.  The only way he is going to do better is either with an electric CS prop and/or turbo.  If he shaves the prop off to say, 74”, he will get a couple hundred more rpm, but will probably lose in total thrust.  Diameter is a big determiner in thrust. 

 

I would like more pictures of Dons intake and exhaust!

 

Bill B

 


From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Al Gietzen
Sent: Wednesday, March 24, 2010 3:05 AM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: Turbo Planning

1. When I read your stats in your first paragraph, the first thought that

comes to mind is that there is too much prop. 

 

Ditto.

 

Al G

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