STRUCTUAL MODEL AND RESEARCH OF THE INNOVATIVE ANTI-ICING SYSTEM

In this article, analyzes the operational and technical characteristics of anti-icing systems used in modern civil aircraft, as a promising anti-icing system, a structural model of a system equipped with a microwave generator that can be installed on the wing of an aircraft, as well as on other aircraft surfaces that may be subject to icing, has been proposed. An application scheme for such a system for carbon-fiber and aluminum-based front edges has been developed, and the microwave generator to be used in the system will be used in the form of a block with low energy consumption and minimal traction on the icy parts of a particular type of aircraft.

Autorentext

Islam Isgandarov - PhD,Professor, Head of Department at National Aviation Academy, Baku.Sakhavat Amirbayli - Master, Chief Laboratory Assistant of Department at National Aviation Academy, Baku.