U.S. Patent Specifications

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