Patent · US Active

Reinforced acoustic treatment panel for an aircraft propulsion unit

US12077309B2 · kind B2 · utility

0Cited by
5References
12Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 10, 2022
Grant dateSep 3, 2024
Priority date
Expiry dateJun 10, 2042

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG10K11/168
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

An acoustic treatment panel intended to be disposed on at least one wall of an aircraft propulsion unit in contact with a fluidic flow, the panel including a first, acoustically reflective skin, a second, acoustically porous skin intended to be in contact with the fluidic flow, and a honeycomb structure extending between the first skin and the second skin and having a plurality of cavities. The panel includes at least one acoustically transparent reinforcing wall passing through a plurality of cavities of the honeycomb structure and extending from the second skin to the first skin, forming a non-orthogonal angle with the first and second skins.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.