----- Original Message -----
From: Paul <rotaryeng@earthlink.net>
Sent: Tuesday, April 25, 2000 6:55 PM
Subject: Cyclic loads - Noise
Bulent Aliev wrote:
I already had it in my plans to do the same modification if I could. It
is so
simple in theory, I can not believe it Burt did not do it. Moving the
prop hub
couple inches higher or lower will prevent the prop blades entering the
wing wake
along the full length of the blade at the same time.
In a two blade prop is even worse. Both blades unload and load
simultaneously.
Bulent
An interesting footnote. Most of the stress and noise mentioned
here is
related to *radial* wakes. If the wake is along a radial of the
prop shaft
then the affects are awful. Simply moving the wake a few inches
(the more
the better) off radial will make the wake *sweep* across the prop
blade
instead of impacting it all at once. The difference is remarkable.
At
Moller moving a strut once resulted in a 20 dB noise reduction.
This
means you too Perry, stay away from radial struts. Also, look at
the
Aerospatial (sp?) helicopters sometime with the buried tail rotor.
The
struts are in the form of an H. Most other buried rotors use
similar methods.
Jeff Spitzer
Wow. That IS interesting. So those Rutan designs have the thrust line
at wing level. Moving the engine up a few inches will make it
quieter. That will give more room under the engine for the rad too.
Paul Lamar
Richard Sohn wrote:
Pitch mechanism failure on a CSP has occured on tractor AC too. One of the
first CSP from Hoffmann had the pin come loose in the early sixties. The AC
was a KL 207, all wood four place low wing, crashed on approach. The test
pilot of the AC manufacturer was severly injured.
This aerea(pitch pin) should receive special attention when designing a new
prop.
Richard.
Ours is pressed into the steel hub and it is locked in place
by the other hub. Even if it comes loose it cannot come out of
its hole. The pitch change will still work. Perhaps the blade
will be a bit loose but it can be preflighted by feel.
Paul Lamar
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