U.S. Patent Specifications

Abstract

In an aircraft propulsion mechanism, a rotatable shaft, a cross shaft mounted thereon, combustion chambers rotatably mounted on said cross shaft, an air‐cooling jacket for cach chamber, a funnel concentric with said rotatable shaft and open at its forward end, and radial tubes connecting said funnel to said jackets, each chamber having an air‐passage between said air‐cooling jacket and said chamber and open at both ends, and air from said outer air‐cooling jackets being discharged into said inner air‐passages near the entrance end thereof.

Citation

(1951), "U.S. Patent Specifications", Aircraft Engineering and Aerospace Technology, Vol. 23 No. 11, pp. 352-352. https://doi.org/10.1108/eb032105