This document presents the results of an FAA investigation to determine the effects of using de-icing, as opposed to anti-icing, in aircraft turbine engine inlets. A literature search was conducted. Ice protection equipment technology was assessed. This report describes the icing/de-icing process, discusses de-ice system operation and performance and ice detector characteristics, and presents a method for determining the effects of the de-icing process on the turbine engine and its associated induction system. Keywords: Aircraft icing, De-icing systems, Ice detectors, Anti-icing. (MJM)
De-Icing of Aircraft Turbine Engine Inlets
1988
72 pages
Report
No indication
English
De-icing of aircraft turbine engine inlets
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