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U.S. Patent Specifications

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 October 1947

17

Abstract

A rib for aircraft comprising, in combination; a pair of contralateral members, each having upper and lower flanges, webs connecting said flanges, offset surfaces on said webs for securing one member to the other; and means bonding said offset surfaces to‐gether; the offset surfaces providing aligned upper and lower slots between said edges of said flanges, and elongated vertical passages between the webs and the slots.

Citation

(1947), "U.S. Patent Specifications", Aircraft Engineering and Aerospace Technology, Vol. 19 No. 10, pp. 337-338. https://doi.org/10.1108/eb031566

Publisher

:

MCB UP Ltd

Copyright © 1947, MCB UP Limited

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