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SOUND INSULATION DEVICE FOR AN AIRCRAFT

发明专利审中
7浏览
14权利要求 · 1 独立
§ Ⅰ

卷宗概要

发明人

Laurent CAZEAUX; Arnulfo CARAZO MENDEZ; Leana ROSSI; Suresh PALANI; Kevin BOUKHORS

IPC 分类

G10K 11/172B64D 33/2

CPC 分类

G10K11/172B64D33/2B64D2033/206

A sound insulation device comprising at least one cavity, called a quarter-wave cavity, a first abutment of two walls, respectively of a first strip and a second strip, in contact with each other, so that a passage is provided between the cavity and another cavity. The other cavity, called a Helmholtz cavity, is closed by an edge closure, a second joining of two walls, respectively of the first strip and the second strip, in contact with one another. Each of the walls of the first and second abutments include a portion arranged along the closing edge of the Helmholtz cavity, called the sacrificial portion and form the end of the covering.

原文(中文)

A sound insulation device comprising at least one cavity, called a quarter-wave cavity, a first abutment of two walls, respectively of a first strip and a second strip, in contact with each other, so that a passage is provided between the cavity and another cavity. The other cavity, called a Helmholtz cavity, is closed by an edge closure, a second joining of two walls, respectively of the first strip and the second strip, in contact with one another. Each of the walls of the first and second abutments include a portion arranged along the closing edge of the Helmholtz cavity, called the sacrificial portion and form the end of the covering.