THERMAL MANAGEMENT SYSTEM FOR A COMPONENT OF A GAS TURBINE ENGINE

A thermal management system (230) for a component of a gas turbine engine (20) is disclosed. In various embodiments, the thermal management system (230) includes a manifold (238) extending circumferentially about a longitudinal axis (A) and defining a plenum (240); a cooling fluid transfer tube (236) disposed within the plenum (240) and configured to transfer a component cooling fluid from a component cooling fluid source to the component; and a cooling fluid passageway (244) connected to the manifold (238) and configured to transfer a plenum cooling fluid from a plenum cooling fluid source to the plenum (240).