Spindash64
Airman
- 82
- Oct 21, 2021
I'm aware this is likely a silly sounding question, but I still don't understand the relative advantages and disadvantages of different piston engine types that well, particularly not in relation to their potential uses in WWII aircraft. I know that there WERE some experiments with both: the Rolls Royce Crecy was a 2-stroke engine design that promised power similar to a late war R-2800 in the relative packaging of a Merlin, and the Germans had a turbocharged Diesel engine on the Ju-86P for trying to squeeze more range and altitude out of the design
Here's what I DO know:
-2 Stroke engines have a power stroke and a compression stroke: exhaust and intake happen during these, rather than sequentially. I could see some potential loss of efficiency from this, but I don't know for certain
-Diesel Cycle engines don't use a spark plug: instead, the "raw" air is compressed by itself, and fuel is sprayed directly into the cylinder, where it combusts. This means, as far as I know, no risk of engine knock, and possibly no risk of detonation
-2 strokes need to have Oil mixed into the fuel, and operate on a "lossy" system. In present day this raises emission concerns, but I don't see this being an issue for planners of the time. I've heard that 2 stroke engines often use a 32:1 mix, which would mean a 2 stroke plane at this ratio would be using around 3% of its effective fuel tank space for oil storage. That actually sounds like the same amount that planes carry in their dedicated oil tank, though…
So what am I missing here that makes the near unanimous of 4-stroke Otto so obvious to designers of the period? I KNOW that there must be some other serious tradeoffs that I just haven't noticed, or haven't fully appreciated yet, and I can't hope to even begin to understand engines if I can't understand something like this
Here's what I DO know:
-2 Stroke engines have a power stroke and a compression stroke: exhaust and intake happen during these, rather than sequentially. I could see some potential loss of efficiency from this, but I don't know for certain
-Diesel Cycle engines don't use a spark plug: instead, the "raw" air is compressed by itself, and fuel is sprayed directly into the cylinder, where it combusts. This means, as far as I know, no risk of engine knock, and possibly no risk of detonation
-2 strokes need to have Oil mixed into the fuel, and operate on a "lossy" system. In present day this raises emission concerns, but I don't see this being an issue for planners of the time. I've heard that 2 stroke engines often use a 32:1 mix, which would mean a 2 stroke plane at this ratio would be using around 3% of its effective fuel tank space for oil storage. That actually sounds like the same amount that planes carry in their dedicated oil tank, though…
So what am I missing here that makes the near unanimous of 4-stroke Otto so obvious to designers of the period? I KNOW that there must be some other serious tradeoffs that I just haven't noticed, or haven't fully appreciated yet, and I can't hope to even begin to understand engines if I can't understand something like this