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The B.M.W. 801 Aero‐Engine

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 August 1942

Abstract

THE B.M.W.801 is an air‐cooled, 14‐cylinder, 4‐strokc, 2‐row radial, fuel‐injection engine with reduction gear and engine‐driven cooling‐fan. Supercharging is by a single‐stage centrifugal blower with two automatic speed changes (Figs. 1 and 2).

Citation

(1942), "The B.M.W. 801 Aero‐Engine", Aircraft Engineering and Aerospace Technology, Vol. 14 No. 8, pp. 223-228. https://doi.org/10.1108/eb030930

Publisher

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MCB UP Ltd

Copyright © 1942, MCB UP Limited