wrote in message
...

To avoid this problem, BJ tilted the entire rotor head rather than
changing the pitch cyclicly. In fact, the pitch on the blades only
changes when the collective is moved and not the cyclic. This results
in the grease being retained for a longer period of time. It still
needs frequent regreasing, but at least you don't need a new set of
bearings after each hour of flight.

OK - silly question. On the face of it, it seems to make a lot of sense to
do it this way

- simple connection - you could probably lose the swashplate somehow too
- fewer cyclical forces on components
- less chance of mast bumping

What are the downsides other than potentially odd handling?

I should imagine that the control forces would be enormous and pushing the
rotor head forwards would cause the fuselage to pitch backwards for a
start-off.

Regards
Andrew

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