METHODS FOR REDUCING ACOUSTIC NOISE ON TOTAL AIR TEMPERATURE SENSORS USING ADDITIVE MANUFACTURING

In one embodiment, a cover (12) for an aircraft sensor includes a leading edge (28), the leading edge extending along a longitudinal axis. A first side panel (24) extending from the leading edge in a positive x direction transverse to the longitudinal axis and a second side panel (26) extending from...

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Bibliographische Detailangaben
Hauptverfasser: PITERA, Rudy, SABLE, Robert E
Format: Patent
Sprache:eng ; fre ; ger
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Zusammenfassung:In one embodiment, a cover (12) for an aircraft sensor includes a leading edge (28), the leading edge extending along a longitudinal axis. A first side panel (24) extending from the leading edge in a positive x direction transverse to the longitudinal axis and a second side panel (26) extending from the leading edge in the positive x direction. A first trailing edge (30) on the first side panel, the first trailing edge opposite the leading edge. A second trailing edge (32) on the second side panel, the second trailing edge opposite the leading edge. A first plurality of ridges (34) on an outer surface of the first side panel.