IP Library Granted Patent US 11,199,202
Granted Patent B2
US 11,199,202 · App. 16/631,250 · Granted Dec 14, 2021

Acoustic attenuator for a turbomachine and methodology for additively manufacturing said acoustic attenuator

Inventors: Byron L. Mohr (Olean, NY); Christopher Guerra (Olean, NY); Scott MacWilliams (Allegany, NY)
Assignee: DRESSER-RAND COMPANY
F04D29/66B33Y10/00B33Y80/00G06T17/00G10K11/162F05D2230/50F05D2260/96
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Quick Facts
Patent No.
US 11,199,202
App. No.
16/631,250
Granted
Dec 14, 2021
Kind
B2
Abstract

An acoustic attenuator for a turbomachine and methodology for additively manufacturing the acoustic attenuator are provided. The acoustic attenuator includes an annular body ( 202 ) having an outer surface ( 204 ) and an inner surface ( 206 ). The inner surface of the annular body may define a bore ( 208 ) extending along a longitudinal axis ( 209 ) of the acoustic attenuator between a first end and a second end of the acoustic attenuator. The annular body may be formed by a plurality of axially-successive cross-sectional layers (e.g., 632, 634, 636 ) unitized between the first end and the second end of the acoustic attenuator. The plurality of axially-successive cross-sectional layers may be transversely disposed relative to the longitudinal axis of the acoustic attenuator. At least some axially-successive cross-sectional layers of the plurality of axially-successive cross-sectional layers (e.g., 632, 634, 636 ) defining a pocket ( 214 ) disposed between the outer surface and the inner surface of the annular body. At least a segment of a periphery of the pocket comprises two sides ( 1452, 1454 ) arranged to join at a common end point to form an apex ( 1460 ) of the pocket.

Claims (36)

1. An acoustic attenuator for a turbomachine, the acoustic attenuator comprising:

an annular body having an outer surface and an inner surface, the inner surface of the annular body defining a bore extending along a longitudinal axis of the acoustic attenuator between a first end and a second end of the acoustic attenuator, the annular body formed by a plurality of axially-successive cross-sectional layers unitized between the first end and the second end of the acoustic attenuator, the plurality of axially-successive cross-sectional layers transversely disposed relative to the longitudinal axis of the acoustic attenuator; and

at least some axially-successive cross-sectional layers of the plurality of axially-successive cross-sectional layers defining a pocket disposed between the outer surface and the inner surface of the annular body,

wherein at least a segment of a periphery of the pocket comprises two sides arranged to join at a common end point to form an apex of the pocket, wherein the at least some axially-successive cross-sectional layers further define a radially-inward pocket relative to the pocket disposed between the outer surface and the inner surface of the annular body, and first and second sets of conduits,

wherein the radially inward pocket is substantially aligned with the pocket and wherein the aligned pockets and the corresponding conduits are disposed in a nested relationship.

2. The acoustic attenuator of claim 1 , wherein the common end point that forms the apex of the pocket is defined by an axially-leading cross-sectional layer of the at least some of the axially-successive cross-sectional layers that define the pocket.

3. The acoustic attenuator of claim 1 , wherein a respective side of the two sides arranged to join at the common end point defines a respective angle (θ) relative to a line

that bisects the pocket along the longitudinal axis of the acoustic attenuator, wherein the respective angle is selected so that the plurality of axially-successive cross-sectional layers is self-supporting.

4. The acoustic attenuator of claim 1 , wherein the respective angle (θ) comprises an angular value less than in a range from about 45 degrees to about 70 degrees.

5. The acoustic attenuator of claim 1 , wherein the two sides arranged to join at a common end point to form the apex of the pocket comprise straight sides.

6. The acoustic attenuator of claim 3 , wherein a cross-sectional shape of the pocket is selected from the group consisting of a polygonal cross-sectional shape, a conic cross-sectional shape, and a combination of two or more of said cross-sectional shapes.

7. The acoustic attenuator of claim 1 , wherein the at least some of the axially-successive cross-sectional layers that define the pocket further defining a set of conduits arranged to provide fluid communication between the pocket and the bore.

8. The acoustic attenuator of claim 1 , wherein at least a segment of a periphery of a respective conduit of the set of conduits comprises two sides arranged to join at a common end point to form an apex of the conduit.

9. The acoustic attenuator of claim 8 , wherein the common end point that forms the apex of the respective conduit is defined by an axially-leading cross-sectional layer of the at least some of the axially-successive cross-sectional layers that define the respective conduit.

10. The acoustic attenuator of claim 9 , wherein a cross-sectional shape of the respective conduit is selected from the group consisting of a polygonal cross-sectional shape, a conic cross-sectional shape, and a combination of two or more of said cross-sectional shapes.

11. The acoustic attenuator of claim 1 , wherein the outer surface of the annular body defines a boundary of a cover of the acoustic attenuator configured to enclose the pocket, wherein the cover and the annular body constitute a unitary structure.

12. The acoustic attenuator of claim 1 ,

wherein at least a segment of a periphery of the radially-inward pocket comprises two sides arranged to join at a common end point to form an apex of the radially-inward pocket.

13. The acoustic attenuator of claim 12 , wherein the common end point that forms the apex of the radially-inward pocket is defined by an axially-leading cross-sectional layer of the at least some of the axially-successive cross-sectional layers that define the radially-inward pocket.

14. The acoustic attenuator of claim 13 , wherein a respective side of the two sides arranged to join at a common end point to form the apex of the radially-inward pocket defines a respective angle (θ) relative to a line that bisects the radially-inward pocket along the longitudinal axis of the acoustic attenuator, wherein the respective angle is selected so that the plurality of axially-successive cross-sectional layers is self-supporting.

15. The acoustic attenuator of claim 14 , wherein the respective angle (θ) comprises an angular value less than in a range from about 45 degrees to about 70 degrees.

16. The acoustic attenuator of claim 14 , wherein the two sides arranged to join at a common end point to form the apex of the radially-inward pocket comprise straight sides.

17. The acoustic attenuator of claim 14 , wherein a cross-sectional shape of the radially-inward pocket is selected from the group consisting of a polygonal cross-sectional shape, a conic cross-sectional shape, and a combination of two or more of said cross-sectional shapes.

18. The acoustic attenuator of claim 12 , wherein the first set of conduits is arranged to provide fluid communication between the pocket and the radially-inward pocket, and the second set of conduits is arranged to provide fluid communication between the radially-inward pocket and the bore.

19. A method for manufacturing an acoustic attenuator for a turbomachine, the method comprising:

generating a computer-readable three-dimensional (3D) model of the acoustic attenuator, the model defining a digital representation comprising:

an annular body having an outer surface and an inner surface, the inner surface of the annular body defining a bore extending along a longitudinal axis of the acoustic attenuator between a first end and a second end of the acoustic attenuator, the annular body formed by a plurality of axially-successive cross-sectional layers disposed between the first end and the second end of the acoustic attenuator, the plurality of axially-successive cross-sectional layers transversely disposed relative to the longitudinal axis of the acoustic attenuator; and

at least some axially-successive cross-sectional layers of the plurality of axially-successive cross-sectional layers defining a pocket disposed between the outer surface and the inner surface of the annular body,

wherein at least a segment of a periphery of the pocket comprises two sides arranged to join at a common end point to form an apex of the pocket,

wherein a respective side of the two sides arranged to join at the common end point defines a respective angle (θ) relative to a line that bisects the pocket along the longitudinal axis of the acoustic attenuator, wherein the respective angle is selected so that the plurality of axially-successive cross-sectional layers is self-supporting,

wherein the at least some of the axially-successive cross-sectional layers that define the pocket further defining a set of conduits arranged to provide fluid communication between the pocket and the bore;

wherein the at least some axially-successive cross-sectional layers further defining a radially-inward pocket relative to the pocket disposed between the outer surface and the inner surface of the annular body, and first and second sets of conduits,

wherein the radially inward pocket is substantially aligned with the pocket, and wherein the aligned pockets and the corresponding conduits are disposed in a nested relationship; and

manufacturing the acoustic attenuator using an additive manufacturing technique in accordance with the generated three-dimensional model,

wherein the outer surface of the annular body defined by the model constitutes a boundary of a cover of the acoustic attenuator configured to enclose the pocket,

wherein the cover and the annular body constitute a unitary structure.

Assignments (2)
MERGER Recorded Mar 8, 2023
From: DRESSER-RAND COMPANY
To: SIEMENS ENERGY, INC.
Reel/Frame 062922/0542 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 15, 2020
From: MOHR, BYRON L.; GUERRA, CHRISTOPHER; MACWILLIAMS, SCOTT
To: DRESSER-RAND COMPANY
Reel/Frame 051521/0686 →
Continuity (2)
Provisional Application 62535266 · Jul 21, 2017
Related Publication 20200217332A1 · Jul 9, 2020