we had interedsting problems on a robin 440 2 strtoke wi th harmonics at
certain rpm  causing the crank to fail, if we avoided these rpms in theory
it would last longer .and it was reciprocal as we added weight the rpm of
the harmonic changed and you could vary it pureely with weight in the
reduction drive
on direct drive engines i suppose this would mean the weight of the prop,
out of balemce props aerodynamically and weight wise - i guess would cause
more problems possibly shorter crank life.
i have ofen wondered about anti vibration dampers
i have even heard of some tuners adding crank weights with good effect for
smoother running
one thing i reckon there is probably quite a few factors ,
phil
----- Original Message -----
From: "Mark Langford" <n5...@hiwaay.net>
To: "KRnet" <kr...@mylist.net>
Sent: Wednesday, January 18, 2006 3:42 AM
Subject: Re: KR> Corvair info post


> Ron Eason wrote:
>
> >I have been reading some of these emails with interest from an engineer
> > stand point and find that flight testing is laborious way to test.
> > Why not simply test the cranks in a physical lab where gradual eccentric
> > dynamic loads can be placed on the shafts and record loaded failure?
>
> Do you have any idea how expensive this "simple test" would be?  And it
> still would not come close to  replicating the real-world environment of
an
> airplane in flight.
>
> > Some fan shafts geometries have critical harmonic RPM's that will cause
> > failure if the shaft rotates at that RPM for extended time periods. The
> > solution is to stay out of this RPM range i.e. above or below. I think
the
> > problem may be fatigue failure due to critical harmonic loading caused
by
> > the prop. This would require solids modeling the shaft and stress
> > analyzing.
>
> I'm a CAD kinda guy, and use solid modeling to solve a lot of my problems
> before they ever crop up.   We even solid modeled our house before we
built
> it....but solid modeling a crankshaft and replicating the dynamic forces
and
> their reactions on an entire engine/propeller system installed on an
> airplane are two different things.  In my view, engines are simply too
> complicated to model  all of the complex dynamics of all the reciprocating
> and rotating parts, at least with software mere mortals can afford (even
> Nastran/Patran).  We have Nastran/Patran at work, and if I thought there
was
> a prayer of getting useful info out of it, I'd have done it already.  Ford
> and GM may have something like that, but even those guys have to do real
> world testing on a new engine and test and fine tune it after
prototyping...
>
> Mark Langford, Harvest, AL
> see homebuilt airplane at http://www.N56ML.com
> email to N56ML "at" hiwaay.net
>
>
> _______________________________________
> Search the KRnet Archives at http://www.maddyhome.com/krsrch/index.jsp
> to UNsubscribe from KRnet, send a message to krnet-le...@mylist.net
> please see other KRnet info at http://www.krnet.org/info.html
>
>
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