High reliability fuel oil nozzle for a gas turbine

F - Mech Eng,Light,Heat,Weapons – 23 – D

Patent

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60/171

F23D 11/38 (2006.01) F23D 11/00 (2006.01) F23D 11/24 (2006.01)

Patent

CA 1259197

- 7 - ABSTRACT OF THE DISCLOSURE A fuel nozzle for a gas turbine is arranged so that the air supply portion which surrounds the fuel supply portion is conveniently removable to permit cleaning but the two parts are resiliently related to permit differential expansion caused by the thermal differentials encountered during operation.

474237

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