Acoustic damper for gas turbine combustors with orthogonal slots

Patent metadata

Field	Value
Publication number	US-11536174-B2
Application number	US-201816632147-A
Country	US
Kind code	B2
Filing date	Jul 19, 2018
Priority date	Jul 20, 2017
Publication date	Dec 27, 2022
Grant date	Dec 27, 2022

Abstract

An acoustic damper includes a low porosity layer section and a housing. The low porosity layer section is formed in a liner of a gas turbine combustor and has an arrangement of elongated generally S-shaped slots formed therein. The housing has a plurality of feed apertures. The housing is coupled to the low porosity layer section thereby defining a cavity such that air outside the housing is configured to flow through the apertures and through the elongated generally S-shaped slots in the low porosity layer section, thereby transforming acoustic energy into thermal energy and aiding in providing an acoustic dampening effect for the gas turbine combustor during operation thereof.

First claim

What is claimed is:

1. An acoustic damper system for a gas turbine combustor, the system comprising:
a first low porosity layer section formed in a liner of the gas turbine combustor, the first low porosity layer section having a first arrangement of elongated generally S-shaped slots formed therein;
a first housing having a first plurality of feed apertures, the first housing being coupled to the first low porosity layer section thereby defining a first cavity, air outside the first housing being configured to flow through at least a portion of the first plurality of feed apertures in the first housing and through at least a portion of the first arrangement of elongated generally S-shaped slots in the first low porosity layer, thereby transforming a first range of frequencies of acoustic energy into thermal energy and aiding in providing an acoustic dampening effect on the first range of frequencies of acoustic energy for the gas turbine combustor during operation thereof;
a second low porosity layer section formed in the liner of the gas turbine combustor, the second low porosity layer section having a second arrangement of elongated generally S-shaped slots formed therein; and
a second housing having a second plurality of feed apertures, the second housing being coupled to the second low porosity layer section thereby defining a second cavity, air outside the second housing being configured to flow through at least a portion of the second plurality of feed apertures in the second housing and through at least a portion of the second arrangement of elongated generally S-shaped slots in the second low porosity layer, thereby transforming a second range of frequencies of acoustic energy into thermal energy and aiding in providing an acoustic dampening effect on the second range of frequencies of acoustic energy for the gas turbine combustor during operation thereof;
a first metering layer having a first arrangement of apertures therein, the first metering layer being positioned within the first housing such that the first metering layer divides the cavity into a first sub-cavity and a second sub-cavity, and wherein the first metering layer is generally parallel with and spaced a distance from the first low porosity layer section, the distance being between five millimeters and one hundred millimeters; and
a second metering layer having a second arrangement of apertures, the second metering layer being positioned within the first housing such that the first metering layer and the second metering layer divide the cavity into three sub-cavities, and wherein a porosity of the first arrangement of apertures is different from a porosity of the second arrangement of apertures.

2. The system of claim 1 , wherein the first low porosity layer section is positioned in a first circumferentially extending portion of the liner and the second low porosity layer section is positioned in a second circumferentially extending portion of the liner that is laterally offset from the first circumferentially extending portion of the liner, and wherein the first range of frequencies of acoustic energy and the second range of frequencies of acoustic energy (i) are different, (ii) partially overlap, (iii) do not overlap, or (iv) overlap by less than 10 percent.

3. An acoustic damper for a gas turbine combustor, the acoustic damper comprising:
a low porosity layer section formed in a liner of the gas turbine combustor, the low porosity layer section having an arrangement of elongated generally S-shaped slots formed therein, each of the elongated generally S-shaped slots of the arrangement having a major axis, the major axes of a first plurality of the elongated generally S-shaped of the arrangement slots being generally perpendicular to the major axes of a second plurality of the elongated generally S-shaped slots of the arrangement;
a housing having a plurality of feed apertures, the housing being coupled to the low porosity layer section thereby defining a cavity, air outside the housing being configured to flow through at least a portion of the plurality of feed apertures in the housing and through at least a portion of the elongated generally S-shaped slots in the low porosity layer section, thereby transforming acoustic energy into thermal energy and aiding in providing an acoustic dampening effect for the gas turbine combustor during operation thereof;
a first metering layer having a first arrangement of apertures therein, the first metering layer being positioned within the housing such that the first metering layer divides the cavity into a first sub-cavity and a second sub-cavity, and wherein the first metering layer is generally parallel with and spaced a distance from the low porosity layer section, the distance being between five millimeters and one hundred millimeters; and
a second metering layer having a second arrangement of apertures, the second metering layer being positioned within the housing such that the first metering layer and the second metering layer divide the cavity into three sub-cavities, and wherein a porosity of the first arrangement of apertures is different from a porosity of the second arrangement of apertures.

4. The acoustic damper of claim 3 , wherein a flame in a flame region of the gas turbine combustor produces a highest acoustic amplitude of the gas turbine combustor and wherein the acoustic damper is positioned directly adjacent to the flame region of the gas turbine combustor to provide the acoustic dampening effect.

5. The acoustic damper of claim 3 , wherein a portion of the liner directly surrounding the low porosity layer section does not include any (i) elongated generally S-shaped slots formed therein and (ii) feed apertures formed therein.

6. The acoustic damper of claim 3 , wherein a portion of the liner directly surrounding the low porosity layer section includes one or more cooling apertures therein.

7. The acoustic damper of claim 3 , wherein the low porosity layer section has a generally square shape with rounded corners and wherein portions of the liner directly adjacent to at least two sides of the low porosity layer section do not include any elongated generally S-shaped slots formed therein.

8. The acoustic damper of claim 3 , wherein each of the elongated generally S-shaped slots of the arrangement has a slot thickness that is between 0.1 millimeters and 0.3 millimeters.

9. The acoustic damper of claim 3 , wherein each of the elongated generally S-shaped slots includes:
an elongated generally straight slot portion having a first end and an opposing second end;
a first generally curved slot portion directly attached to the first end of the elongated generally straight slot portion; and
a second generally curved slot portion directly attached to the opposing second end of the elongated generally straight slot portion, wherein the elongated generally straight slot portion has a length between three millimeters and twenty millimeters, and wherein the first generally curved slot portion has a first arc length between two millimeters and ten millimeters and wherein the second generally curved slot portion has a second arc length between two millimeters and ten millimeters.

10. The acoustic damper of claim 9 , wherein the elongated generally straight slot portion of each respective elongated generally S-shaped slot corresponds to the major axis of the respective elongated generally S-shaped slot, and wherein the first generally curved slot portion of each respective elongated generally S-shaped slot extends from the respective elongated generally straight slot portion in a first direction and the second generally curved slot portion of each respective elongated generally S-shaped slot extends from

Assignees

• Harvard College
• Siemens Canada Ltd

Inventors

• Bertoldi Katia
• Javid Farhad
• Bourgeois Genevieve
• Jette François-Xavier
• Pham Minh Quan
• Shanian Ali
• Schaenzer Megan

Classifications

• F01D25/12

  Cooling · CPC title

• F01N2210/04

  Throttling-expansion and resonance · CPC title

• F23R2900/00014

  Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators · CPC title

• G10K11/172

  using resonance effects · CPC title

• F01N2490/15

  Plurality of resonance or dead chambers · CPC title