Lockheed didn't want to produce the single-rotation unit and they also knew planes headed for Europe would need altitude performance. Both the single-rotation and the non-turbo would result in unhappy customers, and Lockheed wasn't looking for that outcome.
In the end, the government order prevailed.....
I file this under 'hangar talk', not under 'historical stuff'. No hard feelings.
You're being much too picky, Tomo...
Maybe I am too picky, but then I'm not the one inventing new clasifications for ww2 gear either.
The V-1710-93 had an auxiliary stage added. It was not an engine with internal 2-stages, and could easily be tuned to run without the auxiliary stage by the addition of standard parts. It had the external auxiliary stage. Yes, it functioned as a 2-stage engine, but the basic engine was still a single-stage supercharged V-12 that had the pressure carburetor fed by the aux stage.
You are mistaking that carburetor on the -93 was fed by auxiliary stage - the ram air 1st entered the carb, and after that it entered the aux stage. Nobody ever claimed that any V-1710 featured Merlin-like 2-stage compressor, the -93 is/was still a 2-stage supercharged engine.
The -93 did make it into the early P-63As, of which the USA got few. They only made 200 P-63A-8s, 730 P-63A-10s and 38 TP-63A-10s. 2,397 of 3,303 of all P-63 variants went to the Soviet Union, and the vast majority of the early -93's went to someone else and we never saw them except for the delivery flights through Alaska.
Allison made 2554 of the V-1710-93 engines, more than 40 percent of all 2-stage V-1710s.
All the rest of the V-1710s equipped with auxiliary stage superchargers were of the -100 series and that is why all the allison experts ignore the sub-100 series engines ... very few were actually flown and the survivors with the aux stages are rare...
I'm afraid that this is a combination of arrogance and misinformation, though the survivors are indeed rare.
So what I said earlier pretty much goes. Our regular service pilots really only saw the -100 series Allisons with the Aux-stage superchargers. A few test pilots saw earlier Aux-stage units, but they never made service and nobody who went through USAAF A&P school who got assigned to active-duty units had much to do with the sub -100 aux-stage engines except for a very few early P-63As that we got. The P-63s we DID get usually went to reserve units. We assigned 1825 P-63 serial numbers, but actually got about 900 of them, the vast majority of which had -100 series Allisons installed. I doubt we ever saw more than maybe 50 of the early P-63As with -93 engines, and they were never issued to combat units.
US service pilots rarely seen also the other Allison 2 stage engines, apart from token number of P-82 pilots. Of course, there was no '100 series' V-1710, but 'E series', or 'G series' for example.
I believe the Soviets were responsible for moving the cannon forward and almost doubling the ammunition capacity and they made several other changes to ensure the P-63 could recover from flat spins. It proved to be a good bird for them.
It was probably a good bird for them. Soviet demanded changes re. strength of airframe, that they judged as not strong enough, ref. AHT entry about the P-63. Soviets did not have any role in disposition of the cannon and ammo. The flat spins were specialty of P-39, not the P-63.