Fuel nozzle flange with reduced heat transfer

Details Fuel nozzle flange with reduced heat transfer Fuel nozzle flange with reduced heat transfer

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/28 (2006.01) F23D 11/38 (2006.01)

Patent

CA 2608287

A fuel nozzle for a gas turbine engine comprises a nozzle body defining a passage extending therethrough and a flange around the nozzle body extending radially and outwardly from the nozzle body. The flange defines a mounting face thereof and a plurality of mounting holes in the mounting face extending through the flange. The mounting face includes a contacting land protruding from the mounting face for abutting a mounting surface of a support structure of the engine when the fuel nozzle is mounted to the support structure.

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