PPRuNe Forums - View Single Post - Dynamics Concept - Modification to Intermeshing Rotors
Old 21st Feb 2005, 20:24
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Dave_Jackson
 
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A sales pitch ????.

slowrotor,

"I wonder about your preference for intermesh. Why not coaxial?"

The intermeshing has a number of advantages over the coaxial, particularly when considering future high-speed rotorcraft. A post in 1993 by the knowledgeable Paul Cantrell looked at the question from the opposite perspective: "I know the ABC is currently shelved, but I hope that it will started up again. I wonder whether intermeshing wouldn't work better - perhaps Sikorsky didn't want to have to deal with Kaman? I don't really know why they picked coaxial rather than intermeshing..."


"I would be concerned with gear mesh failure in a synchropter. "

This is an advantage. There are hundreds of potential failure points in a helicopter. The interconnecting final reduction is a short-coupled two gearset, which is intentionally over designed.

________________

quadrotor,

"... a blade collision ..., as the blade's tips would be almost in the same plane...'

This is one of a number of reasons for implementing Absolutely Rigid Rotors. The intermeshing feature is the only significant commonality between the well-known Kaman helicopters and the UniCopter project.

IMHO, Kellett was on the right track with his 3-blade rotors. He was seeking one million dollars to produce a rotor with greater rigidity. It appears that the death of Dave Driskill ended any chance of getting the funds and ended the company.


H-43 is a Kaman pilot, who has posted information about the Kaman helicopters on this forum. If interested, a search on [H-43] and [Rotorheads] should bring up his comments.


Dave

Last edited by Dave_Jackson; 21st Feb 2005 at 20:35.
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