GregP
Major
Hi Wuxak,
I didn't say the R-4360 had two crankshafts ... I said it was basically two crankshafts joined by a properly-designed main bearing mount that largely helped eliminate any coupling harmonics. It was a solid joining and became a single crankshaft, but the center exhibited almost no vibration at all except the same end harmonics as the 2-row unit. Altogether a neat design piece that never made the predicted power ... There weren't any 5,000 HP R-4360's as envisioned. They never made more than about 3,500 HP even in the developed versions, except for ONE engine that was tested at 4,500 HP. It never flew so, while I don't count it as a power output point, it DOES indicate potential that was never developed.
Today, the R-4360 is a powerhouse only becasue we stopped big-piston development for aircraft in 1945 ... and propellers are getting VERY scarce!
I didn't say the R-4360 had two crankshafts ... I said it was basically two crankshafts joined by a properly-designed main bearing mount that largely helped eliminate any coupling harmonics. It was a solid joining and became a single crankshaft, but the center exhibited almost no vibration at all except the same end harmonics as the 2-row unit. Altogether a neat design piece that never made the predicted power ... There weren't any 5,000 HP R-4360's as envisioned. They never made more than about 3,500 HP even in the developed versions, except for ONE engine that was tested at 4,500 HP. It never flew so, while I don't count it as a power output point, it DOES indicate potential that was never developed.
Today, the R-4360 is a powerhouse only becasue we stopped big-piston development for aircraft in 1945 ... and propellers are getting VERY scarce!