TwoTwoLeft
o- - - - - - -l
Should you one day fly a turboprop, you'll note torque (a measure of power which is basically the turboprop equivalent of manifold pressure) will do the same thing - rise with a reduction on RPM.
In the 600-hp Cessna Caravan for example, the torque limit for takeoff is 1658 ft/lbs at a prop RPM of 1900. That combo produces 600 shaft horsepower.
Once in climb/cruise, the prop RPM can be reduced as low as 1600 RPM, with the torque limit rising linearly as prop RPM decreases, until it hits a minimum RPM of 1600, where the torque limit is 1970 ft/lbs...which also gives you 600 shaft horsepower.
The common car formula works for turboprops as well (you just have to know the actual torque rating, not a percentage):
Horsepower = (torque x speed) / 5252
There's also a little extra power from the jet thrust of a turboprop, but that's another discussion.![]()
You're right as far as the coorilation in the power setting increase with an RPM reduction. But the reasons why this happens is very different between the two power plants.
They're both self propelling air pumps. But MP is more of a potential power indication with RPM being the limitor, while torque more of a final output of power being generated by a given RPM.
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