초록 ▼

An acoustic liner 20 includes a remote panel 26, a proximate panel 28 transversely spaced from the remote panel and a resonator chamber 34b residing between the panels. Perforations 38 penetrate the proximate panel in registration with the resonator chamber 34b. A neck 56 with an inlet 58 recessed f

An acoustic liner 20 includes a remote panel 26, a proximate panel 28 transversely spaced from the remote panel and a resonator chamber 34b residing between the panels. Perforations 38 penetrate the proximate panel in registration with the resonator chamber 34b. A neck 56 with an inlet 58 recessed from the proximate panel establishes communication between the chamber and a fluid stream G flowing past the proximate panel. A bypass coolant passage 66 guides coolant through the perforations without guiding it through the resonator chamber.

대표청구항 ▼

We claim: 1. A coolable acoustic liner for attenuating noise in a substantially longitudinally flowing fluid stream, comprising: a remote panel; a proximate panel transversely spaced from the remote panel; a resonator chamber residing between the remote and proximate panels, the resonator chamber h

We claim: 1. A coolable acoustic liner for attenuating noise in a substantially longitudinally flowing fluid stream, comprising: a remote panel; a proximate panel transversely spaced from the remote panel; a resonator chamber residing between the remote and proximate panels, the resonator chamber having a neck with an inlet, the inlet being recessed from the proximate panel; perforations penetrating through the proximate panel, the perforations including a plurality of longitudinally spaced perforations in registration with the resonator chamber; and a bypass cooling system for guiding coolant through the plurality of longitudinally spaced perforations without guiding coolant through the resonator chamber. 2. The liner of claim 1 wherein the bypass cooling system includes a bypass coolant passage defined in part by a passage wall and a cooperating partition. 3. A coolable acoustic liner for attenuating noise in a substantially longitudinally flowing fluid stream, comprising: a remote panel; a proximate panel transversely spaced from the remote panel; a resonator chamber residing between the remote and proximate panels, the resonator chamber having a neck with an inlet, the inlet being recessed from the proximate panel; perforations penetrating through the proximate panel in registration with the resonator chamber; and a bypass cooling system for guiding coolant through the perforations without guiding coolant through the resonator chamber, wherein the bypass cooling system includes a bypass coolant passage defined in part by a passage wall and a cooperating partition, a coolant intake comprising an opening in the remote panel for admitting coolant to the bypass cooling passage, and a coolant outlet for discharging coolant into a coolant plenum between the inlet and the proximate panel. 4. The liner of claim 1 wherein the remote panel is a relatively cold panel and the proximate panel is a relatively hot panel. 5. The liner of claim 1 wherein the liner circumscribes an axis, a longitudinal direction is axial, a transverse direction is radial, and a lateral direction mutually perpendicular to the longitudinal and transverse directions is circumferential. 6. The liner of claim 1 wherein the neck has longitudinal and lateral dimensions, and the lateral dimension exceeds the longitudinal dimension. 7. The liner of claim 1 comprising multiple resonator chambers all tuned to the same frequency. 8. The liner of claim 1 wherein the resonator chamber is a lower frequency resonator chamber and wherein the liner also includes at least one higher frequency resonator chamber. 9. The liner of claim 8 wherein the proximate panel includes regions of higher porosity in registration with lower frequency resonator chambers and regions of lower porosity in registration with higher frequency resonator chambers, and the liner also includes a bypass coolant passage for conveying bypass coolant to higher porosity regions without admitting the bypass coolant to the resonator chambers. 10. The liner of claim 8 comprising multiple lower frequency resonator chambers all tuned to a common lower frequency and multiple higher frequency resonator chambers all tuned to a common higher frequency. 11. A coolable acoustic liner for attenuating noise in a substantially longitudinally flowing fluid stream, comprising: a remote panel; a proximate panel transversely spaced from the remote panel; a resonator chamber residing between the remote and proximate panels, the resonator chamber having a neck with an inlet, the inlet being recessed from the proximate panel; perforations penetrating through the proximate panel in registration with the resonator chamber; and a bypass cooling system for guiding coolant through the perforations without guiding coolant through the resonator chamber, and wherein the remote panel includes coolant admission holes for admitting coolant into higher frequency resonator chambers. 12. A coolable acoustic liner for attenuating noise in a substantially longitudinally flowing fluid stream, comprising: a remote panel; a proximate panel transversely spaced from the remote panel; a resonator chamber residing between the remote and proximate panels, the resonator chamber having a neck with an inlet, the inlet being recessed from the proximate panel; perforations penetrating through the proximate panel in registration with the resonator chamber; and a bypass cooling system for guiding coolant through the perforations without guiding coolant through the resonator chamber, and wherein the remote panel includes auxiliary coolant admission holes for admitting auxiliary coolant into lower frequency resonator chambers. 13. The liner of claim 1 wherein the neck is laterally continuous. 14. The liner of claim 1 wherein the neck is isolated. 15. The liner of claim 14 wherein the neck is cylindrical. 16. The liner of claim 1 comprising a longitudinally forward band of resonator chambers and a longitudinally aft band of resonator chambers, each band including laterally distributed resonator chambers of at least two classes. 17. The liner of claim 16 wherein the resonator chambers are laterally distributed so that resonator chambers of a given class in the forward band of resonator chambers are laterally aligned with resonator chambers of the same class in the aft band of resonator chambers. 18. The liner of claim 16 wherein the resonator chambers are laterally distributed so that resonator chambers of a given class in the forward band are laterally nonaligned with resonator chambers of the same class in the aft band. 19. The liner of claim 18 wherein the resonator chambers are laterally distributed so that resonator chambers of a given class in the forward band of resonator chambers are laterally offset relative to resonator chambers of the same class in the aft band of resonator chambers. 20. The liner of claim 1 wherein the liner circumscribes an axis that extends in a longitudinal direction, and wherein the neck extends in a generally radial direction, and wherein multiple perforations of the plurality of longitudinally spaced perforations are associated with the inlet of the neck of the resonator chamber such that coolant passes through the multiple perforations of the resonator chamber to cool the proximate panel. 21. The liner of claim 1 wherein the bypass cooling system includes at least a radial coolant passage that extends at least in part along a wall of the resonator chamber that extends generally parallel to the neck.