It turns out that in Bell 206 the same circuit as in Bell 205 / UH-1, only there is no gyroscopic rod with a damper. Also one common horizontal hinge and tilting rotor. For some reason, it always seemed to me that on the B206 the usual common Yuryev-Sikorsky bushing, where the thrust turns the blades.
All the weight and stress of the entire aircraft is counting on the top of the mast and the little bit of metal attached to the main shaft. I would like to know what the mast is made of. That has to be on tough piece of metal. Especially with the extra long mast of the Robinson design.
we cannot thank these men enough for their dedication to work and the love of sharing knowledge so others can benefit. Respect.
It turns out that in Bell 206 the same circuit as in Bell 205 / UH-1, only there is no gyroscopic rod with a damper. Also one common horizontal hinge and tilting rotor. For some reason, it always seemed to me that on the B206 the usual common Yuryev-Sikorsky bushing, where the thrust turns the blades.
All the weight and stress of the entire aircraft is counting on the top of the mast and the little bit of metal attached to the main shaft. I would like to know what the mast is made of. That has to be on tough piece of metal. Especially with the extra long mast of the Robinson design.
So good
I admire your work and your videos!!! Great work!! Is there any chance of contacting with you for some questions that i have?
You can contact me anytime on FaceBook messenger if you need
Nice video suscribed.
جيد.جدا🍎
Kind of surprised that there isn't a damper or rubber stop to prevent hard mast bumping.
bagus kalau bisa lebih detail lagi agar bisa di pahami 👍👍👍👍
I was a 68 E MOS work on all rotor systems.
Good job buddy!
Hi,
the angle of phase lag on this rotor is 90° ?
hi ,1:41 how to assembly can you post deep videos
How is the rotor head bolted to the main sharft
Jesus Nut.
It’s pitch not feather