Acoustic dampers
View Patent ↗An acoustic resonator for use in an engine is provided. The acoustic resonator includes a cavity having a volume, an aperture, and a passage connecting the aperture and the cavity. The aperture has a profiled surface for delaying separation of fluid entering the passage and for reducing losses caused by fluid separation.
1. A resonator comprising:
a cavity having a volume, an aperture, and a passage connecting the aperture and the cavity;
said aperture having means for delaying separation of fluid entering said passage and for reducing losses caused by fluid separation;
said aperture having a leading edge and said separation delaying means comprising said leading edge being formed by a non-planar surface; and
said aperture having a trailing edge and said trailing edge being formed by a first planar surface intersecting a second planar surface.
2. The resonator according to claim 1 , wherein said non-planar surface is formed by a rounded edge.
3. The resonator according to claim 2 , wherein said rounded edge begins at a point far enough back that flow will not separate from said surface.
4. An engine comprising a resonator incorporated into a portion thereof, said resonator comprising a cavity having a volume, an aperture, and a passage connecting the aperture and the cavity; said aperture having means for delaying separation of fluid entering said passage and for reducing losses caused by fluid separation; said aperture having a leading edge and said separation delaying means comprising said leading edge being formed by a non-planar surface; and said aperture having a trailing edge and said trailing edge being formed by a first planar surface intersecting a second planar surface.
5. The engine according to claim 4 , wherein said non-planar surface is formed by a rounded edge.
6. The engine according to claim 4 , wherein said portion comprises a fan inlet.
7. The engine according to claim 4 , wherein said portion comprises a nacelle inlet.
8. The engine according to claim 4 , wherein said portion comprises a portion of a rocket engine nozzle.