U.S. Patent Specifications
Aircraft Engineering and Aerospace Technology
Article publication date: 1 December 1947
A power unit for aircraft and the like comprising, an internal combustion engine, a variable pitch propeller, a supercharger for said engine, a compressor, a series of combustion chambers surrounding said compressor and connected to be supplied by said compressor, each of said combustion chambers terminating rearwardly in a propulsion jet, means for clutching said propeller to be driven by said engine, and drive means connecting said engine to the drive shafts of said supercharger and said compressor.
(1947), "U.S. Patent Specifications", Aircraft Engineering and Aerospace Technology, Vol. 19 No. 12, pp. 403-404. https://doi.org/10.1108/eb031586
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