The article presents reasons of an helicopter’s ising as well as an aircraft’s ising. The maion attention is addressed a conteraction of an ising. Autors divide the problem an two groups: an ising of an airframe – mostly lifting surfaces, an ising of engines. According to authors reasons, an extension (first of all) consequences of airframe’s ising considerably differ from seemingly similar events in an engine. The considerable attention is concentrated on a connteraction of consequences of an ising during the flight. The most complicated ising referes to helicopters, considering their particular aerodynamics characteristics. The autors dedicated is greather attention. Results reached during investigations of heating rotor blades in ITWL are presented.
An Icing Of Aircraft – Reasons, Consequences, Counteraction
2014
Article (Journal)
Electronic Resource
Unknown
an ising of lifting surfeces , resublimation of a steam , heat section of rotor blades , an antiising electric heating , oblodzenie statków powietrznych , resublimacja pary wodnej , elektryczne ogrzewanie przeciwoblodzeniowe , sekcje grzejne łopat nośnych , kolektor elektryczny , oblodzenie wlotów do silnika turbinowego , Industrial safety. Industrial accident prevention , T55-55.3
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