F R E Q U E N T L Y A S K E D Q U E S T I O N S |
| If two-blade
propellers are the most efficient, then why dont all propellers have two blades? The short answer is because efficiency doesnt propel the airplane, thrust does. Efficiency is the ratio of the power coming out of the propeller to the power going into it. A two-blade propeller is capable of achieving a higher efficiency than a three-blade propeller and so on, but at the same time it uses less power and produces less thrust. If you were to operate a propeller at a lower power setting than that for which the efficiency is at its peak, you would have a lower thrust and also a lower efficiency. Likewise if you operate at a higher power setting, the thrust will be higher but the efficiency is lower there also. There is therefore an optimum power setting for each propeller where its efficiency will be highest. If conditions require more thrust than is available from this optimum power setting, then the power must be increased and prop efficiency begins to fall off from its peak value. There reaches a point where a propeller operating at a power higher than that which results in peak efficiency has the same efficiency as a prop with more blades operating at less-than-optimum power. Further increases in power favor the performance of the propeller with more blades. This is because the propeller with fewer blades is no longer operating at its peak efficiency. Do you have a prop for an (airboat,
hovercraft, or wind tunnel)? Do you make fixed pitch props? Could I get a 5 or 6 blade prop for
my 200 hp single? How much faster will my airplane go
with your prop? Will a three-blade prop make my
airplane quieter inside? Why is the scimitar blade better
than a conventional straight blade? What is the difference between an
oil-to-decrease-pitch and an oil-to-increase-pitch propeller? Are they interchangeable on
a given installation? For most general aviation propellers, an oil-to-increase pitch propeller is the simplest, lightest and most affordable form of controllable propeller. When the prop is rotating, centrifugal force acts not only to pull the blade firmly against the hub, but also to twist the blade toward low pitch. Therefore control force only needs to be supplied in one direction to increase pitch. The absence or reduction of this control force naturally results in a reduced pitch. The governor continually monitors the engine speed. When it senses that the RPM is higher than the setting selected by the pilot, it supplies oil to a hydraulic cylinder on the front of the propeller. The high-pressure oil pushes on a piston, which causes the blades to increase in pitch until the RPM returns to its preset value. When the governor senses an underspeed, it allows oil to drain from the cylinder, decreasing blade angle, until the RPM increases the desired amount. A spring inside the propeller ensures that the blades return to low pitch when the RPM is too low to generate sufficient centrifugal force. This type of propeller is used on most single engine airplanes. Conventional twin-engine airplanes need propellers having the ability to feather (where the blades are aligned parallel with the direction of flight) when there is a loss of power or a loss of oil pressure. The oil-to-increase pitch propeller would present a safety hazard to a conventional twin airplane because it defaults to a low pitch position in the absence of power or oil pressure. If power is lost on only one engine, its propeller will windmill creating negative thrust, which when combined with the positive thrust from the remaining engine, makes the airplane difficult or even impossible to control. A feathered propeller has very little drag, so there is less asymmetric thrust with one propeller feathered than with one propeller windmilling and the aircraft is more controllable. For a propeller to default to feather instead of low pitch requires that both the propeller and the governor be significantly different from that of the oil-to-increase pitch propeller. Each blade is generally fitted with a counterweight, which is sized and positioned such that centrifugal force on the counterweight assembly causes a twisting action toward high pitch. A large spring is also used to force the blades into the feathered position as RPM diminishes and the counterweight becomes ineffective. Control oil must now be supplied to decrease pitch, opposing the forces of the counterweights and the feathering spring. The governor for such a propeller operates in the opposite sense from that described previously, supplying oil only if it senses an underspeed. Acrobatic airplanes also benefit from using oil-to-decrease pitch propellers. These propellers are nearly identical to feathering propellers except that their high pitch angles are limited to values similar to those used in oil-to-increase pitch props. Due to the attitudes in which acrobatic airplanes operate oil pressure fluctuations sometimes occur. These fluctuations not only affect engine lubrication, but also change the speed of the propeller. If acrobatic aircraft were to use oil-to-increase pitch propellers, this could result in a momentary overspeed at the same time the engine is starved for lubricating oil. Using an oil-to-decrease pitch propeller results in an underspeed in this situation, which helps to protect both the propeller and the engine. Are custom or specialized
propellers and governors available from Hartzell at my request? Hartzell has a large selection of propellers, blades, spinners and governors and is often able to suggest a suitable propeller system without embarking on a costly development project. Can I use this (paint, filler,
glue, sealer, grease, etc.) instead of your specified (paint, filler, glue, sealer,
grease, etc.)? What can I do when my propeller is
outside of the airworthiness limits and I'm away from my home base? Where do I get Service Bulletin
Information and does it cost anything? The complete set of service documents is available in paper format as a bound set identified as Manual 126. All Hartzell Service Documents are also included on the Hartzell Technical Documents Library on CD ROM. To purchase either Manual 126 or the Hartzell Technical Documents Library on CD ROM, contact our New Parts Sales Dept. at newpartssales@hartzellprop.com. Continuing revision service for Manual 126 in paper format is available for $350 per year. Continuing revision service for the Hartzell Technical Documents Library on CD ROM is available for $175 per year. Contact our Technical Publications Dept. at manuals@hartzellprop.com. Ive found a good deal on a
propeller and it fits the engine in my homebuilt. Ive cut the diameter of the blades
to that recommended by the designer and had it balanced, so now there is no concern about
vibration. OK? If you have questions concerning the compatibility of an installation, Hartzell will gladly provide you with the information needed to make a safe choice. |