Fuel nozzle guide heat shield for a gas turbine engine

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

Patent

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53/170

F23R 3/28 (2006.01)

Patent

CA 1170061

- 11 - Fuel Nozzle Guide Heatshield For A Gas Turbine Engine Abstract This invention relates to the construction of the heatshield of a fuel nozzle guide of a turbine power plant and provides the separation of the higher temperature operating structure from the cooler structure to assure that the expansion and contraction is permitted without undue restrain for increasing its durability.

373429

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