Patent ID: 9151228
Filing Date: 2015-10-06
Classification: F02C,F05D

Abstract:
1. A split fuel control module for a gas turbine engine, the split fuel control module comprising: a first frame unit, the first frame unit including a first base and a first inner side, the first inner side joined to and extending perpendicularly from the first base; a second frame unit, the second frame unit including a second base and a second inner side, the second inner side joined to and extending perpendicularly from the second base, the second inner side configured to align and couple with the first inner side; a segmented fuel path, the segmented fuel path including a fuel inlet configured to receive fuel from a fuel supply, an upstream fuel interface, a downstream fuel interface, and a fuel outlet configured to deliver fuel to the gas turbine engine, the upstream fuel interface fixed to the first frame unit, the downstream fuel interface fixed to the second frame unit and configured to mate with the upstream fuel interface when the first inner side is aligned and coupled to the second inner side; a distributed fuel controller, the distributed fuel controller including a primary fuel shut-off valve and a main fuel control valve, a first portion of the distributed fuel controller fixed to the first frame unit and a second portion of the distributed fuel controller fixed to the second frame unit.