초록 ▼

An acoustically treated structurally reinforced sound absorbing panel having particular application for use at the inlet cowl of a jet engine to reduce engine noise leaked into the environment. The sound absorbing panel includes a sound receiving chamber having a honeycomb shaped core manufactured f

An acoustically treated structurally reinforced sound absorbing panel having particular application for use at the inlet cowl of a jet engine to reduce engine noise leaked into the environment. The sound absorbing panel includes a sound receiving chamber having a honeycomb shaped core manufactured from corrugated metallic ribbons. The sound receiving chamber is sandwiched between a metallic backskin at one side thereof, and a metallic face sheet at the opposite side. The face sheet is perforated so that incoming sound waves which represent the engine noise enter the sound receiving chamber within which they are channeled towards and reflected between the metallic backskin and face sheet. An acoustic attenuation medium having a plurality of short metal fibers that are held together by a sintering process is diffusion bonded to the perforated face sheet so that the reflected sound waves which are channeled through the sound receiving chamber are transmitted through and attenuated by the acoustic attenuation medium.

대표청구항 ▼

1. In combination:a jet engine having an inlet cowl through which incoming air flow is received, said jet engine producing engine noise; and a non-adhesively bonded structurally reinforced sound absorbing panel surrounding at least some of the inlet cowl to reduce the engine noise produced by said j

1. In combination:a jet engine having an inlet cowl through which incoming air flow is received, said jet engine producing engine noise; and a non-adhesively bonded structurally reinforced sound absorbing panel surrounding at least some of the inlet cowl to reduce the engine noise produced by said jet engine and transmitted therefrom into the environment, said sound absorbing panel including: first and second metallic sound reflecting substrates spaced one above the other; a plurality of perforations formed through the first of said first and second metallic sound reflecting substrates to receive incoming sound waves that represent the engine noise produced by said jet engine; a sound receiving chamber comprising a metallic honeycomb shaped core located between said first and second metallic sound receiving substrates to channel the incoming sound waves between said first and second metallic sound reflecting substrates to produce a set of reflected sound waves, and a porous sound attenuating medium comprising metal fibers, said sound attenuating medium welded between said metallic honeycomb shaped core and the first of said first and second metallic sound reflecting substrates such that said non-adhesively bonded sound absorbing panel is adapted to withstand high-temperature and disbonding, and the set of reflected sound waves being channeled between said first and second metallic sound reflecting substrates via the honeycomb shaped core of said sound receiving chamber are transmitted through and attenuated by said sound attenuating medium.