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Posted for bob mackey <n103md@yahoo.com>:
Jeff:
If the engine (including injectors, fuel servo, etc)
only works when fed fuel of just the right pressure, then
the airframe's fuel system must supply fuel of just that
pressure.
To my way of looking at the system... The IO-550/Lancair system
as describe here has both an engine problem and a fuel delivery
problem.
As an example of fuel-system responsibility consider the
cases in which stagnant hot fuel and vaporizes
causing vapor lock ar least insufficient fuel delivery.
The simple solution to that problem is to pump the fuel
from the tank to a pressure regulator near the injector servo,
and return the regulator excess to the tank. It works in your
car, even with much more volatile fuel.
As an example of engine fuel injection problems, I submit
that if changes in the fuel pressure delivered to the injector
servo cause the engine to run unacceptably rich or lean,
then the injector servo is not doing its job. I don't have
a Continental IO-550, and I am not familiar with its operation
other than what I've read here. What I have read here makes me
think that the fuel injection is overly sensitive to fuel
pressure variation.
For comparison, the carbureted Lycoming O-320 in my LNC2
changes fuel flow by about 4% (13gph max vs 12.5).
Not enough for a noticeable change when ROP,
At 12500 ft, I cruise LOP at about 6.5 gph, Again, changing
the fuel pressure by switching the pump on has little effect.
If I remember correctly, the fuel pressure varies from about
20 to 35 psi (or whatever units the EI FP-5L reports).
The system works because the carburetor's bowl, float, and needle
regulate out the pressure changes. I did just replace a leaking
needle/seat, so the 4% variation might have gone away.
For further comparison, the engine in my Toyota MR2 hasn't run
noticeabley rich or lean for the last 175,000 miles.
There has been no service of the fuel system for 17 years.
"""
Are you certain it is an engine issue and not a fuel system issue?
Regards,
Jeff Edwards
LIVP N619SJ
"""
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