Ed, You are good at this kind of thing..
The Renesis primary (red) injectors are
295 cc/min flow rate. At say, 80% duty cycle, what HP would these
injectors support if you moved the staging point to higher RPMs?
Bill B
From: Rotary motors in aircraft
[mailto:flyrotary@lancaironline.net] On
Behalf Of sboese
Sent: Wednesday, February 18, 2009
12:07 PM
To: Rotary
motors in aircraft
Subject: [FlyRotary] staging
Tracy and all,
Looking back at the data I was using when
thinking about my “staging bog”, I realize that the manifold
pressures I am looking at are values I calculate from the EC2 data. My
conversion to units of inches Hg may not be correct. Either my EC2
manifold pressure sensor may have changed calibration or I may have never had
this conversion correct to begin with. I have only one program to do this
and may not have it right. How Tracy
keeps track of all the versions of EC’s is beyond me.
In any case, I can NOT say with certainty
that my EC2 is internally inconsistent as I stated in my previous
message. I apologize if this has caused you to waste any of your valuable
time and energy over this.
The reason I am concerned with staging
more than many others might be is that at the ground level density altitudes of
my home airport, the maximum manifold pressure I see is about 23 inches and of
course it gradually drops off from there as I climb. This results in
staging taking place during critical flight regimes. Encountering an
extended “bog” right after take off is not my idea of fun. If
I cannot get the staging to work well using mode 6, I am considering David
Leonard’s suggestion of moving the staging point to a higher manifold
pressure where I will not normally encounter it. In my case this is need
not be much of a change. The manual indicates that some modes are active
only when the engine is running. Is this the case with mode 7?
I’m trying to make sure I can set the staging point with a pressure
source other than the engine.
This does generate the potential for my
next trip to lower altitudes to be memorable. I just have to remember
that this is venturing into unknown territory again and that full throttle
operation may not be reliable until tuning at the higher power settings
accessible at lower altitudes has been accomplished.
Again, my apologies to especially to Tracy and also the rest
of you.
Steve Boese