Low drag, variable-depth acoustic liner
Systems and devices of the various embodiments may provide a low-drag, variable-depth acoustic liner having shared inlet volumes. Various embodiments may include a low-drag, variable-depth acoustic liner providing aircraft noise reduction. Acoustic liners according to the various embodiments may be used in engine nacelles and/or on external surfaces of an aircraft to reduce acoustic radiation. Acoustic liners according to various embodiments may provide increased broadband acoustic performance with less drag than conventional liners. Various embodiments may provide an acoustic liner with a reduced open area of the facesheet, and therefore reduced drag of the liner, when compared with conventional acoustic liners.
1. An acoustic liner configured to be disposed on a surface, the acoustic liner for attenuating noise and comprising:
a facesheet comprising a plurality of openings, wherein the facesheet is an outermost portion of the acoustic liner when the acoustic liner is disposed on the surface; and
a core coupled to the facesheet, the core comprising at least two distinct acoustic chambers in communication with the plurality of openings, wherein each of the at least two distinct acoustic chambers are configured to define a resonating volume having a shared inlet volume proximate to the facesheet and an unshared chamber interior distal to the facesheet, the at least two distinct acoustic chambers having different resonant frequencies.
2. The acoustic liner of claim 1 , wherein the at least two distinct acoustic chambers are configured to have different resonant frequencies at least in part by having different chamber geometries.
3. The acoustic liner of claim 1 , wherein at least one of the at least two distinct acoustic chambers are multi-layered chambers.
4. The acoustic liner of claim 1 , wherein the at least two distinct acoustic chambers are configured to have different resonant frequencies at least in part by at least one of the chambers having poroacoustic media therein.
5. The acoustic liner of claim 1 , wherein:
the at least two distinct acoustic chambers share an inlet in communication with the plurality of openings;
the core comprises at least one shared inlet volume proximate to the facesheet at the inlet; and
the facesheet is configured such that the plurality of openings are arranged in groups only over the shared inlet volumes.
6. The acoustic liner of claim 1 , wherein the core comprises a honeycomb pattern of acoustic chambers.
7. The acoustic liner of claim 1 , wherein:
the core comprises a partition defining and separating a portion of the at least two distinct acoustic chambers;
the at least two distinct acoustic chambers each have an inlet in communication with the plurality of openings and the shared inlet volume comprises an opening in the partition between the at least two distinct acoustic chambers, the opening in the partition providing a fluid communication path between the at least two distinct acoustic chambers.
8. The acoustic liner of claim 1 , wherein a shape of the plurality of openings in the facesheet is selected from the group consisting of holes and slots.
9. An acoustic liner configured to be disposed on a surface, the acoustic liner for attenuating noise and comprising:
a facesheet comprising a plurality of openings, wherein the facesheet is an outermost portion of the acoustic liner exposed to a fluid flow when the acoustic liner is disposed on the surface; and
a core coupled to the facesheet, the core comprising at least two distinct acoustic chambers in communication with the plurality of openings, wherein each of the at least two distinct acoustic chambers are configured to define a resonating volume having a shared inlet volume proximate to the facesheet and an unshared chamber interior distal to the facesheet, the at least two distinct acoustic chambers having different resonant frequencies.
10. The acoustic liner of claim 9 , wherein the at least two distinct acoustic chambers are configured to have different resonant frequencies at least in part by having different chamber geometries.
11. The acoustic liner of claim 9 , wherein at least one of the at least two distinct acoustic chambers are multi-layered chambers.
12. The acoustic liner of claim 9 , wherein the at least two distinct acoustic chambers are configured to have different resonant frequencies at least in part by at least one of the chambers having poroacoustic media therein.
13. The acoustic liner of claim 9 , wherein:
the at least two distinct acoustic chambers share an inlet in communication with the plurality of openings;
the core comprises at least one shared inlet volume proximate to the facesheet at the inlet; and
the facesheet is configured such that the plurality of openings are arranged in groups only over the at least one shared inlet volume.
14. The acoustic liner of claim 9 , wherein the core comprises a honeycomb pattern of acoustic chambers.
15. The acoustic liner of claim 9 , wherein:
the core comprises a partition defining and separating a portion of the at least two distinct acoustic chambers;
the at least two distinct acoustic chambers each have an inlet in communication with the plurality of openings and the shared inlet volume comprises an opening in the partition between the at least two distinct acoustic chambers, the opening in the partition providing a fluid communication path between the at least two distinct acoustic chambers.
16. The acoustic liner of claim 9 , wherein a shape of the plurality of openings in the facesheet is selected from the group consisting of holes and slots.
17. A system having a source of noise associated with a flow, the system comprising:
a surface;
an acoustic liner disposed on the surface, the acoustic liner for attenuating noise associated with the flow, the acoustic liner comprising:
a facesheet comprising a plurality of openings, wherein the facesheet is an outermost portion of the acoustic liner when the acoustic liner is disposed on a surface; and
a core coupled to the facesheet, the core comprising at least two distinct acoustic chambers in communication with the plurality of openings, wherein each of the at least two distinct acoustic chambers are configured to define a resonating volume having a shared inlet volume proximate to the facesheet and an unshared chamber interior distal to the facesheet, the at least two distinct acoustic chambers having different resonant frequencies.
18. The system of claim 17 , wherein:
the system is an aircraft; and
the surface is a surface of an engine nacelle of the aircraft.
19. The system of claim 17 , wherein the system is a vehicle.
20. The system of claim 17 , wherein the system is a heating, ventilation, and air conditioning system.