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
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!
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