An assembly (34) is provided for an aircraft propulsion system. A first seal wedge (122A) is configured with a first wedge-shaped cross-sectional geometry when viewed in a reference plane. A first aperture extends along a first axis within the first seal wedge (122A). A second seal wedge (122B) is configured with a second wedge-shaped cross-sectional geometry when viewed in the reference plane. A second aperture extends along a second axis within the second seal wedge. A first drain tube (80A) supports the first seal wedge (122A) and is fluidly coupled with the first aperture. A second drain tube (80B) supports the second seal wedge (122B) and is fluidly coupled with the second aperture. A manifold (82) is configured with an outlet (80C). The manifold (82) supports the first drain tube (80A) and the second drain tube (80B). The manifold (82) fluidly couples the first drain tube (80A) and the second drain tube (80B) in parallel with the outlet (80C).
DRAIN MAST SEAL ASSEMBLY WITH SEAL WEDGE(S)
ABFLUSSMASTDICHTUNGSANORDNUNG MIT DICHTUNGSKEIL(EN)
ENSEMBLE D'ÉTANCHÉITÉ DE MÂT DE DRAINAGE DOTÉ DE CALE(S) D'ÉTANCHÉITÉ
2023-09-27
Patent
Elektronische Ressource
Englisch