If you can get your hands on "Converting Auto Engines for Experimental
Aircraft" Second Edition by Richard Finch I recommend it for good reading
and great insight. FWIW

On Tue, Oct 22, 2019 at 2:56 PM Daniel Branstrom via KRnet <
[email protected]> wrote:

> I am not an engineer, and my comment here is based on some reading and
> observations that I have made over the years in aviation. My opinion is
> worth the electrons that were used to produce this post.
>
> In every machine that has rotating parts, torsional harmonic vibration
> is present. I'll call it THV. If a vibration coincides with an operating
> range of the machine, the THV can destroy the machine. If the frequency
> is above or below the operating rotation, it becomes much less of a
> problem. In an automobile, THV is damped by the rubber tires, and the
> greater rotation mass of the flywheel, and, often, automatic
> transmissions. On an airplane, the power pulses go undampened to a
> propeller, which has its own harmonic vibration that can be fed back to
> the engine at certain frequencies and can destroy the engine. Wooden
> propellers tend to dampen this because of their composition.
>
> Aircraft engine manufacturers take torsional harmonic vibration into
> account when designing their engines. That's why some certified direct
> drive engines come with a warning not to operate them at certain rpms
> with certain propellers, or they have counterweights to smooth things
> out. Rotax engines, for example, have a coupling that dampens THV.
> Engines are certified in aircraft with designated propellers for that
> reason.
>
> Torsional harmonic vibration can snap crankshafts and destroy reduction
> drives. It is similar in concept to aerodynamic flutter in flight
> controls. The THV does not disappear where the power pulses are
> overlapping, so that all of the forces going  in same direction as they
> are in 6 or 8 cylinder engines, but at least all of the force going to
> the prop is in one direction. 4 or less cylinder engines have periods in
> their rotation when there is a backward force on the power output. The
> inertia in the engine, as well as flywheels or propellers keep the
> engine turning.
>
> There are very few companies that have been successful in experimental
> aviation with reduction drives. That doesn't mean that there aren't good
> ones out there, but the amount of engineering and manufacturing skill
> needed to build them can be immense and costly, and they have to have a
> big enough market to be profitable. It's also my opinion that as the
> power of the engine goes up, the forces on any reduction drive go up
> exponentially, and that's why it's easier to make a drive for an engine
> developing under 100 hp (which seems to be the dividing line) than one
> that has more power. It's for those reasons that I don't believe you
> will see a Rotax 200 hp engine.
>
> Years ago, there was a manufacturer of a redrive that was used on large
> engine conversions. It seemed to be a good one, with few problems, but
> when the drive was manufactured by someone new, the drives started
> breaking. I credit the problems to manufacturing technique.
>
> I have flown behind a Cessna 175, which has a geared engine. It was
> excellent both in climb ability and cruise speed, I found it close to
> the performance of a 182, and it had a fixed pitch propeller. The 175
> got a bad reputation, I believe, because pilots tried to operate it like
> an ungeard engine. The engine was designed to run at above the red line
> of ungeared engines, and operating it at low ungeared rpms is very hard
> on it. Also, it was not good practice to let the prop drive the engine.
>
> Consider the reputation of anyone making a reduction drive, and look for
> reports of people that have problems with it. Google engine problems or
> engine issues, and look at what other engines they have sold in the past.
>
> That's my 2 cents. Your mileage may vary.
>
> Dan Branstrom
>
>
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