Apparatus for use in a fuel delivery system for a gas...

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

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F23R 3/30 (2006.01) F23R 3/28 (2006.01)

Patent

CA 2013594

TE-6137 APPARATUS FOR USE IN A FUEL DELIVERY SYSTEM FOR A GAS TURBINE ENGINE ABSTRACT OF THE DISCLOSURE A fuel manifold (70) for a gas turbine engine is formed from a plurality of spaced bodies (10) and intercon- necting conduits (72). The bodies (10) are adapted to provide fluid communication between the conduits (72) and a corresponding plurality of nozzle assemblies (62) which are removably secured to the bodies. The nozzle assemblies (62) can thereby be detached from a structure (58) to which the manifold (70) is secured, while all components (10, 72) of the manifold (70) remain secured to the structure (58) and to each other. A fail-safe sealing member (32) adapted for use with the fuel manifold/nozzle assembly combination (70, 62) is also disclosed.

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