"Jumo 222" and "DB 606/610" made in H16 form instead of being 24 cyl types - what gives?

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I realize you have to walk before you can run and the guys between the wars were really striving to get more speed/power/endurance/whatever out of both aircraft and engines but...

How did it come to pass that so many of them seem to have been dreamt up (and acted upon) after one too many at the pub?

"Hey... I know, if we mash three or four banks of cylinders together..."

On the bright side, at least whatever that thing is has a three bladed prop instead of two blades.
 
In retrospect it's easy to see which approaches are workable and which aren't.

Though arguably even at the time it would have made sense to spend more on improving the basic engines. But the revolutionary potential of jets weren't clear (or well, the potential was known, what wasn't clear was whether it would be possible to build something in practice that would tap into said potential), so it was understandable to have something next gen in the pipeline to prepare for the day when the V-12's and 18 cylinder radials run out of steam.
 
How did it come to pass that so many of them seem to have been dreamt up (and acted upon) after one too many at the pub?

"Hey... I know, if we mash three or four banks of cylinders together..."
It sometimes made sense at the time. 1920s when fuel didn't support much boost (if any) you had two choices for more power. More displacement or more rpm.
Adding a bank of existing cylinders offered about a 50% increase in power, assuming the crankshaft held up. Beefing up the crankcase and crankshaft seemed easy to do.

Going from a 2000 rpm engine to a 3000 rpm engine (same 50% potential power) may have been harder. ALL of the rotating. reciprocating parts (includes valves, valve springs, rocker arms, etc) increases the stress loads by 125% over existing loads. The existing engine is not quite of verge of breaking down but the just run it faster school could be in big trouble.
If you are trying to plane for a future engine (3-5 years down the road) you may come up with a different answer than trying to come up with an engine for next years race.

And in the 20s they were still trying to figure out sodium cooled valves, better valve seats, more reliable springs. better oil systems and so on. An extra bank of cylinders may have been the low risk option.
 
The truth is that H16 engine can always be perfectly balanced without using any counterweights. The key requirements is a full synchronization of shafts that acts as their own counterweights, offsetted by 180 degrees. It cancels both primary and secondary imbalances.
For example Napier Sabre has exactly the same amount of firing intervals as V12 engine.
So perfectly balanced balanced H16 would fire every 90 degrees. 45 degrees is not viable.
Having this in mind, one can use customized layout of crankshaft, that won't work for V8 or Flat-8 engines, that cancels all forces locally in groups of 8.


It is not true that the H16 engine will limit visibility, quite the opposite. The pilot always sits high enough to have a view over the engine, and the shorter engine body can improve the forward viewing angles. The H engine can move accessories to its lower part, guaranteeing a very small upper width. The only disadvantage is that in the case of a fighter, the higher position of the cabin will slightly increase the overall drag compared to the inverted V12. But the frontal area increases no more than the power, which may ultimately bring benefits. In the case of bombers, the benefits are immediate, but I still think it is better and much easier to make the H24 engine right away.
 
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Mercury to Pegasus is a 25mm change in stroke. For some reason (rounded off numbers?) this was only worth 47mm in listed diameter
There was around 3 inches of difference between diameters of Jupiter (138.4 cm) and Mercury (130.7 cm). Later their heads became bigger and Pegasus (Jupiter with superchae grew to 140 cm, and Mercury to around 131.5 So everything is quite consistent and minimized.
 

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