U.S. Patent Specifications

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Publication date: 1 May 1941


In a cylinder for an internal combustion engine having an exhaust port and passage, a heat insulating lining which forms a unitary part of the structure of the exhaust passage, said unitary part being integrally united with the material of the cylinder.


(1941), "U.S. Patent Specifications", Aircraft Engineering and Aerospace Technology, Vol. 13 No. 5, pp. 147-148. https://doi.org/10.1108/eb030778




Copyright © 1941, MCB UP Limited

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