Fuel vaporizing tube

F - Mech Eng,Light,Heat,Weapons – 02 – C

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60/114, 60/171

F02C 3/24 (2006.01) F23R 3/32 (2006.01)

Patent

CA 1107518

Fuel Vaporizing Tube Abstract A combustor for gas turbines has fuel vapor- izing tubes and associated mechanisms. The vaporizing tubes are constructed to maintain uniform temperatures therein and the structure also maintains uniform tempera- tures in the head plate and splash plate of the com- bustor. The vaporizing tubes have a direction of vapor discharge disposed at an angle from the axis of the tube stem to direct the vapor stream to the side away from the stem base to minimize formation of localized hot spots and prevent head plate and/or splash plate damage. The interior of the vaporizer tubes are smoothly flow con- toured to eliminate eddies and flow losses and thereby prevent localized hot spots therewithin. The vapor tubes have non-uniform wall thickness serving to prevent areas of carbon build-up and localized hot spots. The splash plates are designed to act with respect to the dis- charge flow and reduce the total temperature spread in the head plate and splash plate. The splash plate configura- tion shields the head plate from the hot vapor discharge from the tubes.

317541

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