Fuel nozzle and manifold assembly connection

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

Patent

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Details

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

Patent

CA 2570773

A fuel supply assembly for a gas turbine engine including a manifold portion with a transfer conduit, a fuel nozzle with an entry conduit and disconnectable means for retaining the transfer and entry conduits in mating engagement with one another.

Un ensemble d'alimentation en carburant pour turbine à gaz comprend un collecteur avec un conduit de transfert, un injecteur avec un conduit d'entrée et un dispositif déconnectable pour retenir les conduits de transfert et d'entrée accouplés de manière homologue.

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