I am a bit confused by Bob M. and Jeff E.
In a carbureted aircraft engine configuration, the only use of an
adjunct pump (hand or electric) is to supply some priming fuel
directly to the intake side of a cold engine before start. The engine
driven pump generally provides a constant pressure fuel supply at about 4-6
psi (maybe less) to the bowl until the float says stop. The carb doesn't
care if the fuel is sputtering into the bowl with vapors since the fuel
level in the bowl is all that counts and that level is kept ahead of the
actual carb's needs. Oh yeah, gravity supplied fuel to a carb works too -
as long as there is fuel in the bowl.
On the other hand, a fuel injected engine, say a Lyc 320 with an RSA style
fuel system, generally requires that some level of fuel pressure must be
maintained so the stinking throttle body can match it to the air
via pressure measured by some weenie tubes in the induction stream so
that ultimately it can deliver the correct fuel flow to the
injectors. The ideal pressure is about 26 psi, but the system only
gets upset if the pressure drops below 12 psi (fluctuations between those values
don't seem to make much difference). How can such
variation happen? Well, one way is vaporization of the fuel because
of heat and thus cavitation in the engine driven pump, especially if that
pump is also heat saturated from the engine operation.
How can that be fixed? Cool fuel could help or maybe raise the system
fuel pressure (read boost pump) to try to keep the fuel from vaporizing before
you actually would like it to vaporize, like near the intake valve. The
"hi" boost pump in my airplane could maybe get the fuel pressure up to 28 psi,
not much higher than the engine pump operating on cool fuel but high enough to
get the fuel back to a liquid state.
Another way to solve a pressure problem traced to the engine
pump might be to duct some cool intake air over the engine pump
- if that is the source of fuel pressure loss/fluctuation during
flight.
The only times I have problems with vaporization is during a hot start or
idling/taxiing very slowly on a really hot day - my red idiot light labeled lo
fuel pressure comes on and is backed up by the fuel pressure gauge dipping below
12 psi, a condition that has been resolved by turning on the boost pump.
BTW, the boost pump is on for takeoffs and landings as a backup.
Scott Krueger
AKA Grayhawk
Lancair N92EX IO320 SB 89/96
Aurora, IL (KARR)
A man
has got to know his limitations.