Gas turbine engine combustion apparatus

Details Gas turbine engine combustion apparatus Gas turbine engine combustion apparatus

1984-07-26

1985-12-31

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

Combustion products generator

60756, F23R 320

Patent

active

045612579

ABSTRACT:
A gas turbine engine combustion apparatus for vaporizing fuel comprises a flame tube having an upstream end wall in which are located a number of flow guides having associated fuel ducts. In operation, fuel and air flow through the U-shaped duct in each guide and the fuel flows onto the inside of the end wall which acts as a vaporizing surface. The exterior of the end wall is cooled by a flow of air from the engine compressor. The invention avoids the need of vaporizing tubes within the flame tube.

REFERENCES:
patent: 2552851 (1951-05-01), Gist
patent: 4138842 (1979-02-01), Zwick

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