Sound absorbers and airframe components comprising such sound absorbers are disclosed. In one embodiment, an airframe component comprises an aerodynamic surface (48) and a sound absorber (38). The sound absorber (38) comprises a perforated panel (40) having a front side exposed to an ambient environment outside of the airframe component and an opposite back side. The panel (40) comprises perforations extending through a thickness of the panel for permitting passage of sound waves therethrough. The sound absorber (38) also comprises a boundary surface spaced apart from the perforated panel. The boundary surface and the back side of the perforated panel (40) at least partially define a cavity in the airframe component for attenuating some of the sound waves entering the cavity via the perforations in the perforated panel (40).
SOUND ABSORBERS FOR AIRFRAME COMPONENTS
SCHALLDÄMPFER FÜR FLUGWERKKOMPONENTEN
ABSORBANTS ACOUSTIQUES POUR PIÈCES DE CELLULE D'AÉRONEF
2019-09-25
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Online Contents | 1994