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U.S. Patent Specifications

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 November 1936

Abstract

A method of preventing detrimental ice formation in the induction system of an internal‐combustion engine for aircraft which consists in causing a small proportion of an anti‐freezing substance to be dispersed in said induction system only when freezing conditions prevail.

Citation

(1936), "U.S. Patent Specifications", Aircraft Engineering and Aerospace Technology, Vol. 8 No. 11, pp. 322-322. https://doi.org/10.1108/eb030122

Publisher

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MCB UP Ltd

Copyright © 1936, MCB UP Limited