Unit cell resonator networks for turbomachinery bypass flow structures

Patent metadata

Field	Value
Publication number	US-11830467-B2
Application number	US-202117503285-A
Country	US
Kind code	B2
Filing date	Oct 16, 2021
Priority date	Oct 16, 2021
Publication date	Nov 28, 2023
Grant date	Nov 28, 2023

Abstract

An acoustic attenuation structure for a gas turbine engine includes a periodic structure having a first unit cell, the first unit cell having a first central body and a first axial tube disposed on the first central body and a second axial tube disposed on the first central body, opposite the first axial tube, each of the first axial tube and the second axial tube being in fluid communication with one another through the first central body.

First claim

What is claimed is:

1. An exit guide vane for a propulsion system, comprising:
a suction-side facesheet;
a pressure-side facesheet; and
an acoustic attenuation structure disposed between the suction-side facesheet and the pressure-side facesheet, the acoustic attenuation structure including a periodic structure including a first unit cell, the first unit cell including a first central body, a first axial tube, a second axial tube, a first lateral tube, a second lateral tube, a third lateral tube, and a fourth lateral tube, the first axial tube disposed on the first central body and the second axial tube disposed on the first central body, opposite the first axial tube, each of the first axial tube and the second axial tube being in fluid communication with one another through the first central body,
wherein at least one of the first axial tube, the second axial tube, the first lateral tube, the second lateral tube, the third lateral tube, or the fourth lateral tube is at least partially sealed via a septum configured to restrict a flow of fluid therethrough.

2. The exit guide vane of claim 1 , wherein the first lateral tube is disposed on and in fluid communication with the first central body, and the second lateral tube is opposite the first lateral tube and disposed on and in fluid communication with the first central body.

3. The exit guide vane of claim 2 , wherein the third lateral tube is disposed on and in fluid communication with the first central body, and the fourth lateral tube is opposite the third lateral tube and disposed on and in fluid communication with the first central body.

4. The exit guide vane of claim 3 , wherein each of the first axial tube, the second axial tube, the first lateral tube, the second lateral tube, the third lateral tube and the fourth lateral tube are in fluid communication with each other via the first central body.

5. The exit guide vane of claim 2 , further comprising a second unit cell interconnected to the first unit cell, the second unit cell including a second central body and a pair of axial tubes and a pair of lateral tubes disposed on and in fluid communication with the second central body.

6. The exit guide vane of claim 5 , wherein the first lateral tube of the first unit cell is interconnected to one of the pair of lateral tubes of the second unit cell.

7. The exit guide vane of claim 6 , further comprising a third unit cell interconnected to the first unit cell and a fourth unit cell interconnected to the second unit cell and to the third unit cell, wherein each of the first unit cell, the second unit cell, the third unit cell and the fourth unit cell is comprised within a layer of unit cells.

8. A bifurcation structure for a propulsion system, comprising:
a first-side facesheet;
a second-side facesheet; and
an acoustic attenuation structure disposed between the first-side facesheet and the second-side facesheet, the acoustic attenuation structure including a periodic structure including a first unit cell, the first unit cell including a first central body, a first axial tube, a second axial tube, a first lateral tube, a second lateral tube, a third lateral tube, and a fourth lateral tube, the first axial tube disposed on the first central body and the second axial tube disposed on the first central body, opposite the first axial tube, each of the first axial tube and the second axial tube being in fluid communication with one another through the first central body,
wherein at least one of the first axial tube, the second axial tube, the first lateral tube, the second lateral tube, the third lateral tube or the fourth lateral tube is partially sealed via a septum configured to partially restrict a flow of fluid therethrough.

9. The bifurcation structure of claim 8 , wherein the first lateral tube is disposed on and in fluid communication with the first central body, and the second lateral tube is opposite the first lateral tube and disposed on and in fluid communication with the first central body.

10. The bifurcation structure of claim 9 , wherein the third lateral tube is disposed on and in fluid communication with the first central body, and the fourth lateral tube is opposite the third lateral tube and disposed on and in fluid communication with the first central body.

11. The bifurcation structure of claim 10 , wherein each of the first axial tube, the second axial tube, the first lateral tube, the second lateral tube, the third lateral tube and the fourth lateral tube are in fluid communication with each other via the first central body.

12. The bifurcation structure of claim 9 , further comprising a second unit cell interconnected to the first unit cell, the second unit cell including a second central body and a pair of axial tubes and a pair of lateral tubes disposed on and in fluid communication with the second central body.

13. The bifurcation structure of claim 12 , further comprising a third unit cell interconnected to the first unit cell and a fourth unit cell interconnected to the second unit cell and to the third unit cell, wherein each of the first unit cell, the second unit cell, the third unit cell and the fourth unit cell is comprised within a layer of unit cells.

14. A noise attenuation panel for a structure within a propulsion system, comprising:
a first periodic structure including a first unit cell, a second unit cell, a third unit cell and a fourth unit cell, wherein each of the first unit cell, the second unit cell, the third unit cell and the fourth unit cell includes a central body interconnected via a plurality of lateral tubes extending from the central body, the first periodic structure forming a first lateral layer of unit cells;
a facesheet and a back plate configured to enclose the first periodic structure;
a second periodic structure, the second periodic structure forming a second lateral layer of unit cells interconnected to the first lateral layer of unit cells, the second lateral layer of unit cells being interconnected to the first lateral layer of unit cells via a plurality of axial tubes, and
wherein the first lateral layer of unit cells and the second lateral layer of unit cells each comprise a plurality of volumes extending axially between adjacent pairs of unit cells that comprise the first lateral layer of unit cells and the second lateral layer of unit cells and wherein the plurality of volumes defines a space exterior to the first lateral layer of unit cells, the space being either partially restricted or completely restricted by a volume filler.

15. The noise attenuation panel of claim 14 , wherein the plurality of volumes includes a first volume including a first volume size and a second volume including a second volume size different from the first volume size.

Assignees

• Raytheon Tech Corp
• Rtx Coroporation

Inventors

• Reimann Craig Aaron
• Winkler Julian
• Homma Kenji
• Mendoza Jeffrey Michael
• Reba Ramons A

Classifications

• G10K11/16 Primary

  Methods or devices for protecting against, or for damping, noise or other acoustic waves in general (G10K11/36 takes precedence) · CPC title

• F02C7/24 Primary

  Heat or noise insulation (air intakes having provisions for noise suppression F02C7/045; turbine exhaust heads, chambers, or the like F01D25/30; silencing nozzles of jet-propulsion plants F02K1/00) · CPC title

• F05D2220/323

  for aircraft propulsion, e.g. jet engines · CPC title

• F05D2260/96

  Preventing, counteracting or reducing vibration or noise · CPC title

• F02C7/045

  having provisions for noise suppression · CPC title