Acoustic structure with increased bandwidth suppression
View Patent ↗The bandwidth or acoustical range of a nacelle or other type of acoustic structure is increased by acoustically coupling honeycomb cells together to form pairs of acoustic cells that have an effective acoustic or resonator length that is up to twice that of either acoustic cell taken alone.
1. An acoustic structure for reducing noise generated from a source, said acoustic structure comprising:
a honeycomb comprising a first edge located closest to said source and a second edge, said honeycomb comprising a first acoustic cell defined by a plurality of walls that extend between said first and second edges and a second acoustic cell defined by a plurality of walls that also extend between said first and second edges of said honeycomb wherein said first acoustic cell and said second acoustic cell share a common wall;
a first acoustic barrier for said first acoustic cell;
a second acoustic barrier for said second acoustic cell;
a surface in said common wall that defines an acoustic pathway between said first acoustic cell and said second acoustic cell, wherein said acoustic pathway is located between the first edge of said honeycomb and said first and second acoustic barriers; and
a third acoustic barrier for said second acoustic cell wherein said acoustic pathway is located between the second acoustic barrier and said third acoustic barrier to thereby provide a first noise attenuation zone comprising the portion of said first acoustic cell located between said first edge and said first acoustic barrier and the portion of said second acoustic cell located between said second acoustic barrier and said third acoustic barrier, wherein said acoustic pathway is the only opening into the portion of said first noise attenuation zone that comprises said portion of said second acoustic cell located between said second acoustic barrier and said third acoustic barrier.
2. An acoustic structure according to claim 1 wherein said third acoustic barrier is displaced away from the first edge of said honeycomb such that said third acoustic barrier and the portion of said second acoustic cell located between said third acoustic barrier and said first edge form a second noise attenuation zone.
3. An acoustic structure according to claim 1 wherein said first acoustic barrier and said second acoustic barrier are located at the second edge of said honeycomb.
4. An acoustic structure according to claim 1 wherein an acoustically porous sheet covers the first edge of said honeycomb.
5. An acoustic structure according to claim 1 wherein at least one acoustic septum is located within said first acoustic cell.
6. An acoustic structure according to claim 1 wherein at least one acoustic septum is located within said second acoustic cell.
7. An acoustic structure according to claim 1 wherein said acoustic structure is a nacelle for an engine.
8. An airplane comprising a nacelle according to claim 7 .
9. A method for reducing the noise generated from a source of noise, said method comprising the step of at least partially surrounding said source of noise with an acoustic structure according to claim 1 .
10. A method for reducing the noise generated from a source of noise according to claim 9 wherein said source of noise is an engine and said acoustic structure is a nacelle.
11. An acoustic structure according to claim 5 wherein at least one acoustic septum is located within said second acoustic cell.
12. A method for making an acoustic structure for reducing noise generated from a source, said method comprising the steps of:
providing a honeycomb comprising a first edge located closest to said source and a second edge, said honeycomb comprising a first acoustic cell defined by a plurality of walls that extend between said first and second edges and a second acoustic cell defined by a plurality of walls that also extend between said first and second edges of said honeycomb wherein said first acoustic cell and said second acoustic cell share a common wall;
providing a first acoustic barrier for said first acoustic cell;
providing a second acoustic barrier for said second acoustic cell;
forming a surface in said common wall that defines an acoustic pathway between said first acoustic cell and said second acoustic cell, wherein said acoustic pathway is located between the first edge of said honeycomb and said first and second acoustic barriers; and
providing a third acoustic barrier for said second acoustic cell wherein said acoustic pathway is located between the second acoustic barrier and said third acoustic barrier to thereby provide a first noise attenuation zone comprising the portion of said first acoustic cell located between said first edge and said first acoustic barrier and the portion of said second acoustic cell located between said second acoustic barrier and said third acoustic barrier, wherein said acoustic pathway is the only opening into the portion of said first noise attenuation zone that comprises said portion of said second acoustic cell located between said second acoustic barrier and said third acoustic barrier.
13. A method for making an acoustic structure according to claim 12 wherein said third acoustic barrier is displaced away from the first edge of said honeycomb such that said third acoustic barrier and the portion of said second acoustic cell located between said third acoustic barrier and said first edge form a second noise attenuation zone.
14. A method for making an acoustic structure according to claim 12 which includes the step of locating at least one acoustic septum within said first acoustic cell.
15. A method for making an acoustic structure according to claim 12 which includes the step of locating at least one acoustic septum within said second acoustic cell.
16. A method for making an acoustic structure according to claim 12 wherein said acoustic structure is a nacelle for an engine.
17. A method for making an acoustic structure according to claim 14 which includes the step of locating at least one acoustic septum within said second acoustic cell.