A
Anonymous
Guest
If I understand correctly, automotive engines require reduction units to reduce prop rpms at higher motor rpms since automotive engines reach peak output at 5000 rpms +. I'm assuming that an automotive motor turning 5000 rpms with a 2-1 reduction unit would be spinning the prop 2500 rpms. Is this correct?
Secondly, I'm a little confused because if a prop is turning 2500 rpms why does it matter how many rpms the motor is turning. Would the effect not be the same if the motor was turning 1000 or 4000 rpms. I'm guessing that it has something to do with the increase horsepower of the engine at higher rpms but if the prop is turning the same speed what's the difference?
Now for my real question. I've heard that aircraft engines generate their horsepower at lower rpms than automotive engines and because of this reduction units are not a necessity to maintain a slower prop speed. What's to be gained then by running a reduction gear on a small aircraft engine because I know folks are doing it with success.
Secondly, I'm a little confused because if a prop is turning 2500 rpms why does it matter how many rpms the motor is turning. Would the effect not be the same if the motor was turning 1000 or 4000 rpms. I'm guessing that it has something to do with the increase horsepower of the engine at higher rpms but if the prop is turning the same speed what's the difference?
Now for my real question. I've heard that aircraft engines generate their horsepower at lower rpms than automotive engines and because of this reduction units are not a necessity to maintain a slower prop speed. What's to be gained then by running a reduction gear on a small aircraft engine because I know folks are doing it with success.