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tomo pauk How practical is it to apply very different supercharger designs to other engines than those they were originally intended for?
France ordered Allison V-1710 engines in 1939-40 to power American aircrafts (H-81/P-40 and P-38s without the turbocharger to use the same supercharger as the H-81s) as well as the Arsenal VG-32 fighter. However, the supercharging setup of early V-1710 was rather underwhelming, so how practical or fast would it have been to apply something like the Szydlowski superchargers, either directly adapted or just in principle? This would go a long way towards removing the only drawback of the V-1710 compared to French designs, as it was a generally better design than the Hispanos as far as the pure engine goes.
Looking at copying better French superchargers, it was probably the Germans than might've benefited the best?
Adopting the S/C from the G&R 14R 04/05 should've helped the BMW 801 series, while the S-P supercharger mated to the power sections of the 9 cyl radials could've also been explored. Both the BMW 132 and the Bramo 323 were with obsolete superchargers (straight vanes, 'squished' intakes - as it was in vogue for the majority of the radials of the day), and the 132 was even without the 2-speed S/C drive, thus it would've benefited due to the way intake of the air was controlled on the S-P supercharger.
The 'better' 132s, like the F, J, K, M and N, were with a ~245mm impeller, as well as with the fuel injection. The F, J and N were the 'high altitude' models (quite an exaggeration come 1939, but these are BMW's words), where the gearing was set for high speed rotation of the impeller. Max boost at 2300 rpm was 1.35 ata (the F model), or, at, 2400 rpm, 1.30 ata (J and N), but these are just the 1 min ratings for take off. The 5 min ratings were either 1.30 ata on 2250 rpm (F mod) for 810 PS at 3800m, or 1.25 ata on 2350 rpm (J, N) for 865 PS at 3400 m (and 820 PS at 3800 m).
The power vs. altitude rating for the J and N are very close to the HS 12Y-31 (240mm impeller, 10:1 drive ratio; 2400 rpm crankshaft speed, 860 CV at 3150m using 880 mm Hg boost = 34.65 in Hg = about 1.20 ata). The 12Y series of the engines benefited a good deal when a good S/C was installed with the -45; still a 240mm impeller but much better, also turning at 10:1 drive ratio, and was making better power at altitude, while the control system took care of the power at lower altitudes.
Quite a lot of words to say that the S-P supercharger on the German radials would've seen an increase of perhaps 15% power above 4 km vs. even the best versions, without cutting on the low altitude power.