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
Publisher
:MCB UP Ltd
Copyright © 1953, MCB UP Limited