A gas turbine engine strut (100) includes a strut body extending in a radial direction and defining an airfoil shape in cross-section perpendicular to the radial direction. The airfoil shape includes a leading edge and a trailing edge. An extraction inlet is defined through an exterior surface of the strut body, in fluid communication with an internal conduit of the strut body. An injection outlet is defined through the exterior surface of the strut body, in fluid communication with the internal conduit for fluid communication through the internal conduit from the extraction inlet to the injection outlet.
ENGINE STRUT FLOW CONTROL
MOTORSTREBEN-DURCHFLUSSREGELUNG
COMMANDE D'ÉCOULEMENT DE JAMBE DE MOTEUR
2024-07-03
Patent
Electronic Resource
English