Fuel manifold with reduced losses

Details Fuel manifold with reduced losses Fuel manifold with reduced losses

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/22 (2006.01)

Patent

CA 2580594

A fuel conveying member of a gas turbine engine fuel system conducting pressurized fluid flow is provided. The fuel conveying member comprises a body defining an L- shaped fuel flow passage therein, the L-shaped passage including an elbow. The elbow portion provides a substantially smooth fluid-dynamic transition between portions of the passage upstream and downstream thereof.

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