Apparatus and method for starting a large gas turbine having...

F - Mech Eng,Light,Heat,Weapons – 01 – D

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F01D 19/00 (2006.01)

Patent

CA 1083363

APPARATUS AND METHOD FOR STARTING A LARGE GAS TURBINE HAVING A CATALYTIC COMBUSTOR ABSTRACT OF THE DISCLOSURE Apparatus and method for starting a gas turbine engine is shown wherein the combustion chamber has a fixed geometry providing a high throughput velocity to prevent flashback during normal operation of the engine. Thus, there is provided a flame holding zone out of the main flow path through the chamber that exhausts into the chamber upstream of a catalytic reactor element to preheat the catalyst to a sufficiently high temperature for continuous auto-combustion therein prior to the rotor of the engine attaining running speed. After running speed the combustion in the flame holding zone is extinguished and the velocity of the fuel/ air mixture in the main flow path through the chamber is sufficient to maintain the combustion within the catalytic element for the continuous running of the engine without any flashback.

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