Some further comments on this topic:-
You recall that in a separate thread, I recommended "Valve Mechanisms for High-Speed Engines", Philip H Smith, 1967, GT Foulis, (Not to be sold in the USA). I would strongly recommend it again, for ideas that may spark solutions.
For instance, it shows the pre-war MG engine with a vertical bevel driven OHC drive with the generator integral to the shaft, ie, the rotating armature acts as a high inertia damper in the drive. Staying with your gear drive, you will I am sure have looked for a half-engine-speed accessory with a high inertia or other opposite torque canceling signature, such as a hydraulic pump that you could drive from the cam gear. Even if there were such an accessory, I doubt that your engine would require it anyway!
Another possibility is to arrange your pumping cams to have relatively long top dwell, and then have the return flank coincide with the pumping flank of a different cylinder. That will help to cancel out some of the instantaneous drive torque spike.
Then again, it may be instructive to contemplate the reduction gear drive used on the Napier Sabre aero engine. The H24 cylinder engine (two flat 12's, one above the other) joined the two crankshafts to the propeller output gear through helical compound gears with a balancing feature which cancelled out the torsionals from the two cranks. I assume that in this case, the propeller and it's output gear had high inertia and thus was a nodal point in the middle. If you will be using the flywheel/clutch mass as your nodal inertia on the crankshaft, then an arrangement as wonderfully elegant as the Napier solution, will be difficult to arrange.
PJGD