Electrically driven Hub

The blade pitch variation is achieved by electric servo-motor. The servo-motor is made under our own project and is produced for FP-propeller exclusively. The primary characteristics we done to our servo-motor are:

• Guaranted and tested functionality up to 3000 rpm of the propeller
• Epicyclic gearbox entirely made in metal
• Long durability (>2000 hr in the range -30°C +50°C)
• Absolute reliability of the functionality

The electric hub FP-propeller was designed in order to achieve the pitch variation speed of 3.5° /sec. This value was assumed because it is the maximum value of the pitch variation that can be controlled manually

Blade anchorage technology

The FP-propeller Srl Company manufactures a wide variety of propellers with in-flight variable pitch. The aim of FP-propeller Srl is to give to each airplane its best propeller, the one that meets the needs of the airplane pilot at the best. TBO of the hub is 2000 hours. We must consider that the variable pitch hub is a mechanical device to be made by high precision mechanics. In particular, the blade shank must rotate with high precision and rigid motion in its seat, on its axis. Ball and roll bearings are assuring this high quality motion. Concerning blades, two categories are used: — manufactured by FP — manufactured by leading world producers of propellers: Sensenich, Warp Drive, Whirl Wind; Catto Blade made by FP has the metal shank bound and immersed in the blade root.

Benefits

Blades made by other manufacturers have the root in composite material, unsuitable for precise anchorage in the variable pitch hub. The problem is solved by bonding the blade root in its metal shank, which becomes the anchor device of the blade to the hub . The metal shank is then fixed to the hub by roll bearings, free to rotate on the axis of the blade. The technology of anchorage of the blade to its metallic shank is of fundamental importance for the safe operation and for the lifetime of the entire propeller. Initially, the shank of the blade is aligned with the axis of the glass by a high precision mask and thus cemented permanently. The cementing of the shank is achieved by resin injection within the thin walls between blade root and metallic glass. The cementing technique, result of specific experimental study, has been tested in cooperation with the Department of Industrial Engineering at the University of Bologna. As final result, blade and metal shank become one body. In other words, blade and metal shank does not move in any direction with respect one to the other. With this technique, of blade anchorage, you get the following benefits. – The accuracy of the angular alignment, i.e. the difference of angle between the propeller blades, is less than 0.1 degrees, and is stable for the entire life of the propeller. – Consequently, there are no vibrations due to angular differences between the blades. – In addition, the blades are easy to mount in the hub, without need of laborious (and inaccurate) adjustments by the installer.

Competitor Comparison

For comparison, some competitors are anchoring the blade in the metal shank but without blocking it permanently. In front of the questionable “advantage” of being able to disassemble it, this solution “simplified” presents the following drawback: periodically, it is necessary to realign the propeller blades. Indeed, the simple mechanical interlocking is unable to inhibit the continuous, imperceptible rotation of the blade in its root, due to the inevitable vibrations of airplane operation. Usually, this process of blade realignment involves a “overhaul”, with the inevitable costs. Our business policy is to give to the Pilot a propeller with long-term reliability and durability, with low maintenance costs. Of course, regular check and maintenance is the safe way to fly in any case.