U.S. Patent Specifications

Abstract

In an aeroplane, two primary structural sections, the sections having confronting ends with a cavity therebetween, a turbo powerplant supported in the cavity, means hingedly connecting the sections at said ends whereby the sections may be hinged apart to expose the powerplant, and releasable means for holding the sections against such hinging.

Citation

(1953), "U.S. Patent Specifications", Aircraft Engineering and Aerospace Technology, Vol. 25 No. 7, pp. 217-218. https://doi.org/10.1108/eb032320