Quote:
Originally Posted by nolimitfiend
Please describe when the pitch is changed on a constant speed propeller? Also, please discuss manifold pressure and how it is managed to determine power output/settings.
First I should point out that GA aircraft have either fixed pitch (e.g. training aircraft) or variable pitch, a.k.a. constant speed, props (found on higher performance airplanes).
Having a fixed pitch prop simplifies things for the pilot...one less control to worry about. The trade-off is performance. At lower speeds, such as in the climb, you want a prop with a smaller angle-of-attack, i.e. it takes a smaller bite of the airstream which is more efficient in the climb. At higher airspeeds, a bigger angle (also sometimes called a "coarse" pitch) gives best performance.
If you own a plane with a fixed pitch prop, you can decide to equip it with a climb prop or a cruise prop. Most owners will opt for the cruise prop because they want to get somewhere fast. But you might want the climb prop if your main use of the plane requires good performance at low speeds. Maybe you're a bush pilot and fly short hops in and out of small strips.
The constant speed prop, on the other hand, allows the pilot to set the prop for climb or cruise via a prop control on the center console. For takeoff, the control is set full forward, resulting in high speed or fine pitch (small bite). On the initial climb, we might set power to something like 25" manifold pressure (using the throttle) and 2500 rpm on the prop (by slightly pulling the prop control back).
Now we see the difference with the constant speed prop: it automatically varies the prop pitch to maintain the rpm we set. If we slow down, the pitch will decrease, otherwise the prop will bog down. As we speed up (for example, when we nose over into cruise flight), the prop pitch coarsens to maintain rpm.
Once established in cruise, we might pull the power and prop controls back to establish a cruise setting of 24" and 2400 rpm (or as recommended by the airplane's operating manual). The prop control is not continually adjusted during flight; we simply set it for the phase of flight we're in. Once we've set it during cruise, we probably won't touch it again until on the approach, at which time we'll again set it full forward in case of a go-around (when we want that good climb performance).
Note that a constant speed prop gives better overall performance, but there is a cost. It's a more complicated piece of equipment since the prop actually twists to achieve the variable pitch. This twisting movement is usually achieved using oil pressure in the prop hub assembly.
Piper Aircraft (prop control is the center, blue control):
Cessna Aircraft (prop control is the center, black knob):
You also asked about manifold pressure. That's the measure of power begin produced by the engine, measured in inches of mercury (just like atmospheric pressure). On simple GA planes (the ones with fixed pitch props), there is no manifold pressure gauge. RPM is sufficient for determining engine power on these planes. More power = higher RPM.
But on a plane with a constant speed prop, the prop will try to adjust its pitch to maintain RPM. In this case, RPM itself is not a reliable indication of the current power setting. These planes have a manifold pressure gauge. Moving the throttle forward will increase manifold pressure. The airplane operating manual will specify the safe settings. It might be full power for takeoff and then reduced to 25" during the climb, and back to 24" or 23" for cruise (with different settings for max range or max endurance or max speed).
One basic technique that I remember from my GA days is that when pulling back the prop control you should first reduce the manifold pressure. Pulling back the prop control first may cause a slight over-boost of the engine since the immediate coarsening of the prop pitch will cause an increase in the manifold pressure (due to the sudden increased drag on the prop).