COOLING AIR MANIFOLD FOR A GAS TURBINE ENGINE

摘要

COOLING AIR MANIFOLD FOR A GAS TURBINE ENGINE A manifold (20) includes a plurality of separate, identical flow channels (28) separated by flow dividers (46). The flow dividers (46) include a thickened boss section (54) for receiving a mounting bolt (50), and are skewed adjacent the manifold outlet for forming a plurality of tangentially directed nozzles (18).