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.
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.
So good
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.
جيد.جدا🍎
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Kind of surprised that there isn't a damper or rubber stop to prevent hard mast bumping.
Nice video suscribed.
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° ?
How is the rotor head bolted to the main sharft
Jesus Nut.
hi ,1:41 how to assembly can you post deep videos
It’s pitch not feather