Hi Jeff

The actual gyroscopic load total doesn't alter because the prop
mass/diameter/speed doesn't change with distance. However, changing its arm
(extension) would alter its distribution along the crank with the bearing
acting as a pivot and could well move it into the same journal as one where
harmonics are focussed as well. The total moments either side of the pivot
must equal zero.

John

The Martindale Family
29 Jane Circuit
Toormina NSW 2452
Australia

ph:  61 2 66 584767
email: johnja...@optusnet.com.au



----- Original Message ----- 
From: "Jeff Scott" <jscott.pi...@juno.com>
To: <kr...@mylist.net>
Sent: Wednesday, June 22, 2005 12:54 AM
Subject: Re: KR> Detonation as crank failure cause?


>
> Detonation can certainly cause some bearing damage, but it would have to
be quite severe and continuous to break a crank.  I've torn down an engine
subjected to severe and constant detonation (mistimed ignition timing due to
a slipped harmonic balancer in a boat).  It looked like someone had worked
over the tops of the pistons with a ball peen hammer.  The rod bearing
damage was minimal, any damage to the mains was undecernable, and the
crankshaft journals were all still within specs, although no longer
perfectly round.  Had it continued to run as it was, it would have pounded
out the rod bearings and damaged the crank by flattening or otherwise
trashing the rod journals first.
>
> Perhaps it's time to take into account the gyroscopic loads imposed by the
spinning prop.  The prop makes a great gyroscope out in front of the plane.
Any change in direction is resisted by the gyroscopic effect of the prop and
that load is transmitted as a bending moment to the prop hub.  In the
Corvair, there is only one small bearing in the front of the case taking
that load.  That bearing get's used like a fulcrum with second main
countering the gyroscopic load from the prop.  That works pretty well when
you transmit that load through a solid shaft like aircraft engines and even
the VW to some degree.  However, in a Corvair, you are transmitting that
load through the front two rod throws.  The 90 degree break across the throw
right next to the bearing journal indicates to me that the crank was being
flexed with that type of load just as if you had bent it back and forth
until it broke.  The further you move the prop out from that bearing, the
more it magnifies that load.  That doesn't mean that the Corvair is a bad or
dangerous engine.  Only that you have to be mindful of it's design
limitations and place the prop as close to the front bearing as possible to
keep the gyroscopic loads transmitted to the crankshaft to a minimum.  Also
perfectly tracked and balanced, as well as light weight props would be in
order.
>
> Ok, here's the disclaimer.  I am a mechanic, not an engineer, so take my
analysis with a grain of salt.  It is also not my intention to throw rocks
at anyone's plane or engine choice.  My interest here lies strictly in the
safety of my friends.
>
> -Jeff Scott
>
>
>
> -- "Mark Jones" <mjo...@muellersales.com> wrote:
> No one has mentioned anything about detonation of the engine as a factor
in crank failure. Detonation causes undue stresses on a crank by creating a
hammer like force generated from the piston through the rods to the crank.
This hammer-like shock wave being imposed on the crank causes severe
overloading. Detonation can destroy an engine very quickly. How many of the
crank failure engines actually were subjected to detonation. The only one
who has confessed to having detonation was Mark Langford and his was a brief
period on departure per his post of June 10th. Just something else to think
about.
>
> Mark Jones (N886MJ)
> Wales, WI
> Visit my web site: http://mywebpage.netscape.com/n886mj
> Email: flyk...@wi.rr.com
>
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>
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