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Turbo/Supercharger Compressors and Turbines for Aircraft Propulsion in WWII: Theory, History and Practice—Guidance from the Past for Modern Engineers and Students
ISBN:
9780791884676
No. of Pages:
382
Publisher:
ASME
Publication date:
2021
eBook Chapter
7. Drive System
Page Count:
44
-
Published:2021
Citation
Kollmann, K, Douglas, CE, & Gülen, SC. "Drive System." Turbo/Supercharger Compressors and Turbines for Aircraft Propulsion in WWII: Theory, History and Practice—Guidance from the Past for Modern Engineers and Students. Ed. Kollmann, K, Douglas, CE, & Gülen, SC. ASME, 2021.
Download citation file:
In Figure 7-1, the power to drive the supercharger is plotted as a function of the rated altitude of the engine. For a rated height of 4 to 6 km, the supercharger consumes 10 to 15% of the total engine output. By the time the 22 km altitude is reached, the supercharger consumes (in theory) the same power as the engine driving it, therefore at 22 km rated altitude an engine will provide 1,000 HP to the propeller and require 1,000 HP to the supercharger drive shaft, therefore requiring a total crankshaft output of 2,000 HP.
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