FIELD: aviation.
SUBSTANCE: invention relates to systems and methods of preventing formation of ice on aircraft parts. System for preventing icing, configured to prevent formation of ice with respect to one or more parts of aircraft, comprises combustion chamber (116), having air inlet (118) and gas outlet (128), air supply pipeline (112) connected to combustion chamber (118) air inlet (118) and configured to direct low pressure air into chamber (116), and one or more supply pipelines connected to combustion chamber (116) gas outlet hole (128), which are made with possibility of connection with one or more parts of aircraft. Combustion chamber (116) is configured to discharge heated gas to one or more feed pipelines through gas outlet (128) to prevent formation of ice or melting of ice with respect to one or more parts of aircraft. Low pressure air is air not compressed in engine inner circuit.
EFFECT: higher efficiency of aircraft engines.
27 cl, 8 dwg
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