It would really help if we knew what type and size of motor the OP was considering.
Nik_2213 said:
Um, didn't some experimental piston-engined aircraft have dual engines set 'tandem' with concentric prop shafts and counter-rotating propellers ??
Can you find an example?
Counter-rotating propellers are driven by a single gearbox bolted to one end of the motor. The torque on the counter-rotating propellers cancel in the gearbox which removes the torque from the engine mounts on the airframe. Counter-rotating propellers are noisy and to avoid destructive oscillation, must limit the RPM. The shaft torque on big slow, many bladed propellers can be so great that hydraulic torque converters are needed to handle the power.
There are also systems that have two motors in the same nacelle, but with independent shafts. One drives a tractor propeller at the front, while the other drives a pusher prop behind. One advantage of independent counter-rotating engines and propellers is that some gyroscopic dynamics are reduced. Examples include the 12 engined Dornier Do X;
https://en.wikipedia.org/wiki/Dornier_Do_X and the Dornier Do 335 twin-engine push-pull fighter.
https://en.wikipedia.org/wiki/Dornier_Do_335
A V12 engine can be seen as two straight 6 engines or two V6 in-line engines sharing one shaft. A straight 6 can be seen as a pair of straight three cylinder motors in tandem.
Multiple parallel crankshafts get interesting. The Junkers Jumo 223 engine was a four crankshaft, 24-cylinder, opposed-piston, two-stroke diesel aircraft engine.
https://en.wikipedia.org/wiki/Junkers_Jumo_223
Collaboration between Junkers and Napier ended with WW2. Napier went on to developed the successful 18 cylinder Deltic, with three crankshafts,, an opposed piston, two-stroke diesel used for railway locomotive and marine propulsion.
https://en.wikipedia.org/wiki/Napier_Deltic