Fuel manifold with reduced losses

Power plants – Combustion products used as motive fluid – Combustion products generator

Reexamination Certificate

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Details

C060S740000, C060S734000

Reexamination Certificate

active

07854120

ABSTRACT:
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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