Hi Mkloby,
>If the aircraft had a constant speed prop, the prop gov would seek to maintain an "ideal" prop rpm speed. If the engine is geared to the propeller at a fixed ratio, as you earlier stated, I don't understand how this is possible.
Hm, if you look at it that way, I could say you're right and that it is not possible to maintain an "ideal" propeller speed.
What the engine computer does is to command a specific speed and manifold pressure for the currently set power lever position. The propeller governor would try and maintain this speed, and if the pilot changed the power lever position, it would try to maintain a different speed as commanded by the engine computer.
However, for lack of an infinitely variable transmission between engine and propeller, the engine computer would have to command a very high propeller-and-engine rpm in order to allow the engine to deliver the desired high power. This speed would be less than ideal for the propeller as it would be hit by a serious loss of aerodynamic efficiency in high-speed flight, especially at altitude, and you'd burn a lot more fuel for just very little more speed, but as this was the only way to keep the engine happy, there was no way around this "abuse" of the propeller in a less-than-ideal operating range.
Regards,
Henning (HoHun)
>If the aircraft had a constant speed prop, the prop gov would seek to maintain an "ideal" prop rpm speed. If the engine is geared to the propeller at a fixed ratio, as you earlier stated, I don't understand how this is possible.
Hm, if you look at it that way, I could say you're right and that it is not possible to maintain an "ideal" propeller speed.
What the engine computer does is to command a specific speed and manifold pressure for the currently set power lever position. The propeller governor would try and maintain this speed, and if the pilot changed the power lever position, it would try to maintain a different speed as commanded by the engine computer.
However, for lack of an infinitely variable transmission between engine and propeller, the engine computer would have to command a very high propeller-and-engine rpm in order to allow the engine to deliver the desired high power. This speed would be less than ideal for the propeller as it would be hit by a serious loss of aerodynamic efficiency in high-speed flight, especially at altitude, and you'd burn a lot more fuel for just very little more speed, but as this was the only way to keep the engine happy, there was no way around this "abuse" of the propeller in a less-than-ideal operating range.
Regards,
Henning (HoHun)