Heat recovery anti-icing system

Power plants – Combustion products used as motive fluid – With safety device

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F02C 7047

Patent

active

043286666

ABSTRACT:
A heat recovery anti-icing system is disclosed. The heat recovery system includes a blower which removes air from the air flow path of a combustion turbine power generating system and circulates the air through a heat exchanger located in the exhaust stack of the combustion turbine. The heated air circulating through the heat exchanger is returned to an inlet filter compartment in the air flow path so as to maintain the temperature of the air in the inlet filter compartment at an elevated level.

REFERENCES:
patent: 3422800 (1969-01-01), Haye
patent: 3703807 (1972-11-01), Rice
Tatge et al., Gas Turbine Inlet Air Treatment, General Electric Publication, GER-2490D, Oct. 1980.

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