A COOLING SYSTEM COMPRISING AN EXHAUST DISTRIBUTION MANIFOLD

A cooling system (100) for a gas turbine engine (20) may comprise a heat exchanger (104) configured to receive a cooling airflow. The heat exchanger (104) may receive the cooling flow at a cooling flow input (126) of the heat exchanger (104) and output the cooling airflow at an exhaust output (128) of the heat exchanger (104). An exhaust distribution manifold (102) may be fluidly coupled to the exhaust output (128) of the heat exchanger (104). The exhaust distribution manifold (102) may define a plurality of openings (130).