In a message dated 2/2/2007 3:49:54 P.M. Central Standard Time,
marv@lancaironline.net writes:
I
think it was Don at Aoirflow Performance who told me fuel boils at 130F
at
sea level. at 100F at 10,000 ft., and if pulled throuogh a filter to the
pump,
at 80F.
Terrence,
Are you sure those weren't degrees Centigrade?
The area behind my engine, the dead space betwixt the top cowl and the
air exiting the bottom of the engine cylinder head cooling fins, often reaches
70C (158F), especially during a slower flight regime (airport traffic pattern)
on a hot day (30C+) at 1500 MSL. The fuel does not demonstrate
"boiling" or vaporization at such temperatures. However, idling at slow
taxi on a 30C+ (86F+) for a long time (20+minutes), where the air temp behind
the engine reaches 90C+ (194F+), there is a vaporization problem that requires
the boost pump (also sitting the 90C temp) to help the engine pump (at God knows
what heat soaked temp) raise the fuel pressure high enough to force it back into
enough of a liquid state so that the engine pump could also push it thru the
fuel system as a liquid at the proper pressure.
140 kts+ climb or flight speed reduces the cowl temperatures
enough so that the fuel, under the proper pressure, reaches the injectors and
thence to the induction system for ultimate use by each and every cylinder's
advanced ignition system to be ignited so that my air pump actually
produces enough torque to be transferred to a rotor device finally
instigating sufficient rearward thrust that further relies on Newtonian concepts
to force the fuel laden wings passing thru non-violent air to provide sufficient
lift to overcome the instantaneous effects of gravity (another Newtonian
concept) so that my machine remains airborne successfully once again.
Oh well, all I can do is operate in the future by what I have observed in
the past.
Scott Krueger
AKA Grayhawk
Lancair N92EX IO320 SB 89/96
Aurora, IL (KARR)
A man
has got to know his limitations.