I've embedded some
comments below:
I am
a little confused as to what may be going on with my EC-2.
I
recently had an incident where the engine went very lean just after take off
and during the climb out to pattern altitude. The power to the secondary injectors may have been
lost causing the engine to go lean above staging threshold MAP. I didn’t do any
troubleshooting. I just set the mixture control to as rich as possible
and continued in the pattern to land. Depending on the size of the primary injectors, setting the
mixture richer would at least partially compensate for the loss of the
secondary injectors.
On
the ground, I could find no problems with fuel, either tank, fuel pressure,
etc. I would have expected
the mixture to go somewhat rich when the MAP went below the staging threshold
if the mixture control had been left in the richer position.
I decided to follow
Steve’s procedure below. After doing this procedure, the engine ran
smoothly from idle to 22 inches on the ground. I put it into mode 9 and
let it change a few spots on the MAP. Almost all the MAP table was still
set at zero. The there may have been
no power to the secondary injectors during this procedure so the mixture would
have correct above the staging threshold MAP within the flow capacity of the
primary injectors as a result of the tuning.
At this
point the controller is set to maintain a reasonable mixture using just the
primary injectors. I taxied out to
fly and during the takeoff run, at about 29 inches and 7100 rpm, the engine
went very rich, 10:1. This is
what would happen if the power to the secondary injectors was restored at the
time the engine went rich. I
adjusted the mixture knob during the takeoff run to about 9-9:30
o’clock. This compensated for
using all 4 injectors now. At about 200 feet of altitude, the mixture suddenly went to about
17:1. This is what would
happen if the secondary injector power was lost again. I moved the mixture knob to about 3 o’clock, but it
really didn’t help much. At the high MAP, the primary injectors alone may have not been
able to supply enough fuel so trying to make the mixture richer with the manual
control would have been ineffective. When I got to pattern altitude and pulled the power back,
the mixture seemed to stabilize at around 13 or so. When the MAP was decreased below the staging threshold MAP, the
controller would have been using just the primary injectors which it had
been tuned to do correctly. I
made the landing and back to the hangar with no incident. Most likely all at MAP below the staging threshold MAP.
On the ground again I
checked the MAP and the table was at zero at all the places the engine had been
operating during the climb out. No corruption of the MAP table had occurred.
The comments are just a
guess as to what may have been going on, but they seem to fit your
observations. It would seem to me that the problem would more likely be
in the power path to the secondary injectors rather than a problem with the
cold start function. The cold start function would affect the both
the primary and secondary injector operation.
Steve Boese
From: Rotary motors in aircraft
<flyrotary@lancaironline.net> on behalf of Bill Bradburry
<flyrotary@lancaironline.net>
Sent: Friday, January 15, 2016
11:27 AM
To: Rotary
motors in aircraft
Subject: [FlyRotary] Re: What do
you think may be happening?
Steve,
I suppose that would be
the secondary injector disable switch. That would explain the engine
going lean, I am not certain how the engine going rich would play in unless the
problem somehow involved the cold start function. That could be somehow
possible since the same switch would be involved in both functions.
I will check that circuit out and see if I can find a bad connection or
switch.
Bill