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More temperatures from N6Q
Hi All!
Before todays third flight, I installed additional
thermocouples on the Franklin engine at the oil inlet
and outlet. My primary monitor is a RMI micro-monitor
which uses an AD590 PN junction to measure oil temperature.
The RMI's sensor is installed in the nose-mounted oil
cooler exit line --i.e. I measure the return oil
temperature to the engine. Simon and Duane had
expressed concern that this was not the correct
place to make the measurement.
Today, I was also going raise the gear and open up
the speed envelope. Unfortunately, the Grear retract
sequence valve failed to close the nose gear doors.
So speeds are still slow but with most of the gear
parts up<g>
The observation for 110 and 130 kts
at 9,500 ft are as follows:
--- oil temps----
OAT IAS MP RPM outlet Cooler inlet Cyl's
C Kts " C C C C
12 108 17.7 2100 93 72 76 90-120
13 126 17.6 2520 97 77 79 100-140
I believe the 17C Delta temperature between the
engine in and out oil temperatures. However,
the absolute thermocouple temperatures are not as
reliable as the micro monitor's. Obviously, the
oil cooler's oil exhaust temperature should be
between what is coming to and from the engine.
Regardless, I now trust the RMI's reported
temperature as reasonable. Please note, so far
this engine has not worked hard and these
temperatures will go up at high power settings.
While looking at various Velocity static ports,
I had noticed all had aerodynamic fences in
front of the static port to reduce sensed static
pressure (or to make the aircraft go faster).
As a result, I moved my static ports down & back
to just in front of the door. I expected this
would be a lower static pressure region.
At 110 kt my airspeed reads 5 kts slow but
1kt fast at 130 kts. Also, today there was
a lot of wind, so my error estimates may be poor.
Regardless, I think I have found another
complicated problem. Any other experience
out there?
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>-} Tim {-<
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Long EZ N3R Velocity N6Q