The climb and and speed curves on all the 109's except the 109F show two clear points where the otherwise linear curves "bend" or so.
Well, some information I have sought up states that the DB605 engines had a variable speed compressor that adapted to the altitude. Thus the engines power output varied smoothly between the altitudes. So I gather that the climb and speed curves should also be more smooth than they currently are?
A good website that has this information can be found at
http://w1.1861.telia.com/~u186104874/db605.htm. A quote from that page:
"While the conventionel mechanical superchargers consisted of one or two compressors driven via a two-speed gear, Daimler-Benz utilised an ingenious barometricly controlled hydraulic clutch which adjusted the compressor speed and thus the charging of the engine according to the needs at a given altitude.
The conventional method results in a relative loss in efficiency below rated altitude, because the compressor uses energy to produce surplus charging. A graphic presentation of engine output relative to altitude would show a "saw-touth" line: the output in low gear rising with altitude until reaching the rated altitude, then output falls until the high gear kicks in, when the output again rises the rated altitude is reached.
In comparison the Daimler-Benz system is more flexible. A graphic presentation would show a smooth shallow curve. A source of efficiency loss with this system being progressive heating of the oil as pressure in the clutch builds with altitude."
Any comments? I don't know exactly if implementing this system would benefit or hinder the DB605 equipped planes. I would like to see this done anyway (if this whole issue is correct).
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SageFIN
"The wolves are gathering, the stars are shifting...
come, join us in the hunt!"
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