U.S. Patent Specifications

Abstract

A pressure cabin for aircraft, comprising a structural frame, an airtight inner wall supported against said frame, said wall comprising a fabric woven from high tensile steel warps and textile weft threads, an outer envelope enclosing the whole, heat‐insulating material filling the space between said inner wall and said envelope, and an interior layer of puncture‐sealing material lining said inner wall.

Citation

(1945), "U.S. Patent Specifications", Aircraft Engineering and Aerospace Technology, Vol. 17 No. 8, pp. 247-248. https://doi.org/10.1108/eb031282