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Compression Test
My views: (Tenuous link, ALFA make aircraft components !!).
At altitude is there less cylinder pressure? YES
Will the gauge read lower? NO IDEA !
For those assuming the engine will keep 'pumping up' until it reaches a
theoretical maximum regardless of altitude, just remember that the cylinder
pressure is dumped overboard once every second revolution. The gauge
maintains the pressure as it has a check valve (non-return valve) in the
connection hose. As far as I can see....14.7 psi @ sea level @ 15degC
multiplied by 10 (10:1 compression) would give a theoretical 'perfect'
pressure of 147 psi. Thus the pressure should decrease proportionately at
altitude. Problem I guess, is will a $10.00 compresssion tester show the
difference ?
The analogy with turbosupercharged piston aircraft engines is a good one.
The higher you go the less dense the air, even though the ambient air
temperature also decreases (7 deg F per 1000ft IIRC). The forced induction
is needed to feed enough oxygen into the cylinder for X amount of fuel to be
burnt.
I don't believe that high compression is the thing which gives a bigger bang
it's the amount of fuel you can expose to the right amount of oxygen. The
smaller volume just makes flame propogation easier/better (hence Alfas
continued return to Twinspark rather than multi valve engines).
Apart from the obvious, Turbine engines are a bit different to pistons. 4
cycle piston engines have the four processes (suck, squeeze, bang, blow)
happening in the same place at different times. Jets have the four
processes happening at the same time in 4 different places.
Beatle
Oz
[demime 0.99c.7 removed an attachment of type image/gif]
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