A system for removing and/or preventing ice build-up on an aircraft includes at least one heat exchanger mounted within an aperture in the tailpipe of a gas turbine engine. The heat exchanger includes an inner plate having a surface which faces inwardly into the tailpipe and which is in direct contact with the heated exhaust gas in the tailpipe, and an outer plate with a surface facing outwardly from the tailpipe and in direct contact with a cooler air stream passing around the turbine engine core. A series of heat exchange fins are formed on the inner p...
An exhaust gas heat exchanger for the turbine engine tailpipe of an aircraft, comprising: i) an inner plate having heat exchange fins extending away from an outer surface of the inner plate, said heat exchange fins forming channels to direct an exhaust gas stream from the turbine engine across the outer surface of the inner plate and enable heat transfer therewith, said inner plate being formed of a material which can withstand degradation by the exhaust gas from the turbine engine; ii) an outer plate having heat exchange fins extending away from an oute...
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