R22 Tail Rotor blades pitch angle variation
Hi,
I'm a french engineering student working on my final project dealing with the tail rotors of different aircrafts.
I would like to have the opinion of professionals (or people who knows the topic) about the mechanism of the pitch angle variation of the tail rotor blades on the Robinson R22 (from the pilot's spreader to the blade).
Does someone know the exact mechanism of this part of the aircraft ? Is is made with an addition of rods or anything else?
Thank you for your reply