What about the DB605D which produced 1,850hp with B4 fuel and 2,000hp with C3 fuel? As far as I'm aware it was the only WWII aircraft engine designed to work well with both low and high octane fuel.
There were several versions; the D, DM (M = with MW50) then DC, DB.
The ASM had a compression ratio of 7.3:1 and I suspect so did the DM. The early DB601N had 8:1 but the DB601 had 6.9.
Both the DB (B4) and DC (C3) had a compression ratio of 8.3 the differences probably only related to camshaft and ignition timmings as well as boost limits. The engines could be easily converted to each other though there seems to have been a specialised version that was easier still to convert.
I suspect a variant of the DB(M) I've seen refered to as the DB/DC became the main production version with controls that allowed variable boost settings for C3 or B4.