Manifold for geared turbofan engine

摘要

A geared architecture for a gas turbine engine includes a lubricant manifold for directing lubricant flow to the geared architecture. The manifold including annular channel and a bowl member received within the annular channel for defining a passage for directing lubricant.

主权项

1. A gas turbine engine comprising:
a fan including a plurality of fan blades rotatable about an axis; a compressor section; a combustor in fluid communication with the compressor section; a turbine section in fluid communication with the combustor; a geared architecture driven by the turbine section for rotating the fan about the axis; and a manifold defining passages for directing lubricant flow to the geared architecture, the manifold including at least one annular channel and a bowl member received within the annular channel for defining at least one passage for directing lubricant.