U.S. Patent Specifications

Abstract

In an annular cowling system for aircraft power plants, the aircraft including a wall and an engine mounting structure extending forwardly thereof to the forward end of which an engine is adapted to be secured, braces on the wall and structure, longitudinal rails carried by said braces, circumferentially spaced relative to one another, and a plurality of individually structurally integral cowl segments disposed around said braces and detachably carried thereby, whereby the cowl segments are free of contact with and support by such a mounted engine.

Citation

(1940), "U.S. Patent Specifications", Aircraft Engineering and Aerospace Technology, Vol. 12 No. 7, pp. 222-222. https://doi.org/10.1108/eb030672