Gas turbine fuel heating apparatus

Power plants – Combustion products used as motive fluid – Combustion products generator

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165140, F02C 708

Patent

active

057944482

ABSTRACT:
A fuel heating apparatus for a gas turbineis provided in which contact of high temperature air and fuel at the time of fuel leakage is prevented so that safety is ensured. The apparatus includes a turbine cooling air cooler of the air cooling type for cooling turbine cooling air and a fuel heater connected to the exhaust side of the turbine cooling air cooler for heating the fuel by the refrigerant air. The turbine cooling air cooler and the fuel heater 4, respectively, form a separate unit so that contact of high temperature air and fuel at the time of fuel leakage is prevented.

REFERENCES:
patent: 374094 (1887-11-01), Smith
patent: 3977196 (1976-08-01), Sedille
patent: 4137705 (1979-02-01), Andersen et al.
patent: 5317877 (1994-06-01), Stuart
patent: 5363641 (1994-11-01), Dixon et al.
patent: 5392595 (1995-02-01), Glickstein et al.
06146924 Japanese Patent Abstract; May 1994, 1 page.
631124833 Japanese Patent Abstract; May 1988, 1 page.

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