System for detecting ignition failure in a gas turbine engine

Data processing: vehicles – navigation – and relative location – Vehicle control – guidance – operation – or indication – With indicator or control of power plant

Reexamination Certificate

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Details

C701S101000, C701S107000, C060S039094

Reexamination Certificate

active

07664590

ABSTRACT:
A method of operating a gas turbine engine is provided. The method includes introducing a fuel into a combustor, detecting a failure of ignition of the fuel, and preventing ignition until the introduced fuel is substantially removed from the gas turbine engine.

REFERENCES:
patent: 3774394 (1973-11-01), Criffield
patent: 3808796 (1974-05-01), Spears, Jr.
patent: 5103629 (1992-04-01), Mumford et al.
patent: 5996938 (1999-12-01), Simonetti

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