Fuel conveying member for a gas turbine engine

Details Fuel conveying member for a gas turbine engine Fuel conveying member for a gas turbine engine

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/28 (2006.01) F02C 7/22 (2006.01)

Patent

CA 2594321

A gas turbine engine fuel conveying member in fluid flow communication with at least one fuel nozzle, the fuel conveying member having at least first and second member portions sealingly engaged to one another, and means for conveying fuel defined at a junction between the first and second member portions. The means for conveying fuel is defined by at least part of two different walls of each of the first and second member portions.

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