A nacelle (24) is provided for an aircraft propulsion system (20). This nacelle (24) includes an outer barrel (58) and an active laminar flow control system (44). The active laminar flow control system (44) includes an array of perforations (112) in the outer barrel (58), a suction source (106A, 106B) and a drain mechanism (108A-110A, 108B-114B). The suction source (106A-106B) is fluidly coupled with the array of perforations (112). The drain mechanism (108B-110B) is fluidly coupled with and between the array of perforations (112) and the suction source (106A, 106B).
ACTIVE LAMINAR FLOW CONTROL SYSTEM WITH DRAINAGE
AKTIVES LAMINARSTRÖMUNGSSTEUERUNGSSYSTEM MIT DRAINAGE
SYSTÈME DE CONTRÔLE DE FLUX LAMINAIRE ACTIF AVEC DRAINAGE
2019-11-06
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |