A flow control system on an aircraft engine nacelle incorporates a plurality of flow control devices (16) each having a body (17). A second plurality of actuators (24) is coupled to the body (17) of an associated one of the flow control devices (16). The actuator (24) rotates the body (17) about a leading edge (18) of an inlet of a nacelle (14) from a retracted position to an extended position.
ROTATING DEVICES FOR MITIGATION OF ADVERSE FLOW CONDITIONS IN AN ULTRA-SHORT NACELLE INLET
DREHBARES VORRICHTUNGEN ZUR MINDERUNG UNERWÜNSCHTER STRÖMUNG BEDINGUNGEN IN EINEM ULTRA KURZEN GONDEL
DISPOSITIFS ROTATIFS POUR ATTENUER DES CONDITIONS DE FLUX INDESIRABLES DANS UNE NACELLE ULTRA-COURTE
2021-03-24
Patent
Elektronische Ressource
Englisch
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