WOW! Bobby!
Those are great numbers! Do you have any pictures
of your cooling installation?
Bill B
From:
Rotary motors in aircraft
[mailto:flyrotary@lancaironline.net] On
Behalf Of Bobby J. Hughes
Sent: Sunday, November 30, 2008 8:02
PM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: : First Flight,
short and hot
Jeff,
What's your water temp
during extended ground runs with your cowling off? With OAT <70F
I have only been able to get my water to 177 and oil to 144 during extended
ground runs up to 7500 rpm.
Any pic you can
share?
Bobby
Renesis
From:
Rotary motors in aircraft
[mailto:flyrotary@lancaironline.net] On
Behalf Of Jeff Whaley
Sent: Sunday, November 30, 2008 9:03
AM
To: Rotary motors in aircraft
Subject: [FlyRotary] : First Flight, short
and hot
I was in the right
seat (flight engineer) when my homebuilt 2+2 made its first flight yesterday
with the 13B Mazda engine, but not without problems. The coolant temperature
reached 230F by circuit altitude; after throttle back and approach it had only
dropped to about 225F; the oil temperature was indicating only 160F (this could
be a mounting-point issue or real I’m not sure … oil temp measure point is from
a small manifold bolted to the PSRU mounting plate, with oil flowing from engine
to PSRU) outside air temperature was about 32-33F. The coolant pressure pegged
the gauge beyond 20 psi, which was a surprise as the pressure cap is rated for
20 psi … I expected the engine to burp itself out and maintain 20
psi.
I tightened up the
cowling around the radiator and removed the thermostat in an attempt to make a
second flight but while removing the thermostat I noticed one of the alternator
V-belts was broken … got another belt only to find it didn’t match the other …
these belts really need to be a matched-pair. Prior to flight, I noticed the
outside belt (which broke) did not have the same tension as the inside belt; it
must have climbed out of the pulley groove and got sliced by the pulley.
Previously I bought a double alternator pulley from Racing Beat but never
installed it, due to difficulty with removing the nut … thought it best to leave
well enough alone … I will now put on that new
pulley.
Hope to make
another flight next weekend if the test pilot is in
agreement.
Any
comments/experience on thermostat Vs no thermostat?
Why would the
pressure cap hold beyond its rating?
Jeff
Whaley
C-FJWW
From:
Rotary motors in aircraft
[mailto:flyrotary@lancaironline.net] On
Behalf Of Tracy Crook
Sent: Saturday, November 29, 2008 3:10
PM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: Renesis fuel
burn
If you haven't calibrated the EM2 fuel flow
yet, the GPH reading does not mean anything. Don't make any decisions
based on that reading. Calibrating the fuel flow is the most
difficult and time consuming parts of EM2 setup. That's the down
side of doing it with such an inexpensive flow sensor ($0.00) since it has
none. The other option is to use a Floscan flow sensor with the
EM2 but they are pricy.
At 30" of manifold pressure and best
power mixture setting and 6400 RPM you should get a fuel burn somewhere around
15 - 18 GPH. The exact amount will depend on other factors like exact
mixture setting, your intake manifold, exhaust system, air temp,
etc.
Tracy Crook
On Thu, Nov 27, 2008 at 6:32 PM, Rino <lacombr@nbnet.nb.ca>
wrote:
Where can I get information on fuel
burn and power for the renesis?
The maximum fuel burn I can get on
takeoff is 11.7 gph (reading on the EM2) at 64 00 rpm. The EM2 is
not fully calibrated yet! I think I should be able to get a higher
fuel burn than that.
The other part of the problem.
What should be the intake manifold runner length on the Renesis. Best
power has to be between 6000 and 6500 rpm limited by the propeller and
redrive configuration. I cannot use more than 65" dia.
prop.
The present runner length is 17" and
I think it is not enough.
Renesis powered
Glass Goose