# US 11,028,732 B2 · High temperature panel damper for sheet metal structures

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- Number: US 11,028,732 B2
- Document ID: US11028732B2
- Status: Granted
- Kind: B2
- Application number: 16/561,782
- Filed: 2019-09-05
- Published: 2021-03-11
- Granted: 2021-06-08
- Earliest claimed: 2019-09-05
- Assignees: Rolls-Royce North American Technologies Inc.
- Applicants: Rolls-Royce North American Technologies Inc.
- Inventors: William McGivern; Michel S. Smallwood
- Web page: https://patentgrep.com/patent/US11028732B2

## CPC

- F01D 25/30: Exhaust heads, chambers, or the like
- F01D 25/04: Antivibration arrangements
- F05D 2260/31: Retaining bolts or nuts
- F05D 2260/96: Preventing, counteracting or reducing vibration or noise
- F01D: NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES (machines or engines for liquids F03; non-positive displacement pumps F04D)
- F05D: INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS

## Abstract

An exhaust assembly for use with a gas turbine engine includes an exhaust duct and a damper system coupled to the exhaust duct. The exhaust duct is configured for fluid communication with the gas turbine engine to receive hot exhaust gases produced by the gas turbine engine. The exhaust duct includes a plurality of panels that define an exhaust passageway. The damper system is coupled to one of the plurality of panels and is configured to dampen vibration of the exhaust duct during use of the gas turbine engine.

## Claims

### Claim 1

An exhaust assembly for use with a gas turbine engine, the exhaust assembly comprising
an exhaust duct configured for fluid communication with the gas turbine engine to receive hot exhaust gases produced by the gas turbine engine, the exhaust duct including a plurality of panels that define an exhaust passageway, a first panel included in the plurality of panels includes a flat inner surface that faces toward the exhaust passageway, a flat outer surface opposite the flat inner surface, and an outer edge that extends around the first panel, and the first panel being supported only along the outer edge, and
a damper system configured to dampen vibration of the exhaust duct during use of the gas turbine engine, the damper system including a fabric damper sheet, a rigid damper plate, and a damper bracket, the fabric damper sheet engaged with the flat outer surface of the first panel, the rigid damper plate arranged in face-to-face relation with the fabric damper sheet and spaced apart from the first panel to locate the fabric damper sheet between the damper plate and the first panel, the damper plate having a body and a perimeter edge arranged around the body, and the damper bracket has a frame that extends along the perimeter edge of the damper plate and defines a window that opens through the damper bracket to expose the body of the damper plate,
wherein the damper bracket is coupled with the first panel and engaged with the perimeter edge of the damper plate to change a resonance frequency of the exhaust duct and dampen the vibration of the exhaust duct during use of the gas turbine engine.

### Claim 2 (depends on 1)

The exhaust assembly of claim 1, wherein the damper plate is coupled to the damper bracket by friction only.

### Claim 3 (depends on 1)

The exhaust assembly of claim 1, wherein the fabric damper sheet comprises non-viscoelastic material.

### Claim 4 (depends on 1)

The exhaust assembly of claim 1, wherein the frame of the damper bracket includes an attachment segment with an inner surface coupled to the first panel and a clip segment with an inner surface engaged with the damper plate, and the clip segment is offset from the attachment segment and arranged generally parallel with the attachment segment.

### Claim 5 (depends on 4)

The exhaust assembly of claim 4, wherein clip segment is spaced apart from the damper plate to define a damper cavity between the clip segment and the first panel and a distance from the inner surface of the clip segment to the first panel is less than a cumulative thickness of the damper plate and the fabric damper sheet.

### Claim 6 (depends on 4)

The exhaust assembly of claim 4, wherein the frame further includes a link that extends outwardly away from the first panel at an angle relative to the first panel to interconnect the attachment segment and the clip segment.

### Claim 7 (depends on 1)

The exhaust assembly of claim 1, wherein the frame of the damper bracket includes an attachment segment with an inner surface coupled to the first panel, a clip segment with an inner surface engaged with the damper plate, and a link that extends outwardly away from the first panel at an angle relative to the first panel to interconnect the attachment segment to the clip segment, and the clip segment extends downwardly from the link at an angle toward the damper plate and is configured to apply a compressive force on the damper plate when the frame is fully installed on the first panel.

### Claim 8 (depends on 1)

The exhaust assembly of claim 1, wherein the damper bracket further includes a cross member that extends across the window of the frame to divide the window into a first aperture and a second aperture.

### Claim 9 (depends on 8)

The exhaust assembly of claim 8, wherein the damper bracket further includes a stiffening rib coupled with the cross member to reinforce the cross member and the frame.

### Claim 10

An exhaust assembly for use with a gas turbine engine, the exhaust assembly comprising
an exhaust duct including a plurality of panels that defines an exhaust passageway, a first panel included in the plurality of panels includes a flat inner surface that faces toward the exhaust passageway and a flat outer surface opposite the flat inner surface, and
a damper system that includes a damper, a damper plate, and a damper bracket, the damper coupled with the flat outer surface of the first panel, the damper plate arranged in face-to-face relation with the damper and spaced apart from the first panel to locate the damper between the damper plate and the first panel, the damper plate having a body and a perimeter edge arranged around the body, and the damper bracket is coupled with the first panel and engaged with the damper plate to change a resonance frequency of the exhaust duct and dampen the vibration of the exhaust duct during use of the gas turbine engine, wherein the damper bracket includes a frame that extends along a perimeter edge of the damper plate and defines a window that opens through the damper bracket to expose the body of the damper plate, and the frame is coupled with the first panel and engaged with the perimeter edge of the damper plate to change a resonance frequency of the exhaust duct.

### Claim 11 (depends on 10)

The exhaust assembly of claim 10, wherein the damper includes a fabric damper sheet made from non-viscoelastic material positioned between the damper plate and the first panel.

### Claim 12 (depends on 10)

The exhaust assembly of claim 10, wherein an air gap is defined between the damper plate and the first panel to provide the damper.

### Claim 13 (depends on 10)

The exhaust assembly of claim 10, wherein the damper bracket further includes a cross member that extends across the window of the frame to divide the window into a first aperture and a second aperture.

### Claim 14 (depends on 13)

The exhaust assembly of claim 13, wherein the damper bracket further comprises a stiffening rib coupled with the cross member to reinforce the cross member and the frame.

### Claim 15 (depends on 10)

The exhaust assembly of claim 10, wherein the damper bracket includes a plurality of washers coupled with an outer surface of the damper plate and a plurality of fasteners that extend through apertures formed in the damper plate and the first panel, the plurality of washers configured to clamp the damper plate and the damper between the plurality of washers and the first panel.

### Claim 16

A method comprising
providing an exhaust duct formed from a plurality of panels with inner surfaces defining an exhaust passageway and outer surfaces facing away from the exhaust passageway,
discharging exhaust gases through the exhaust passageway to cause at least one of the panels to vibrate and produce noise and to expose the at least one panel to temperatures greater than about 250 degrees Fahrenheit, and
changing a resonance frequency of the at least one panel by coupling a fabric damper sheet to the outer surface of the at least one panel to reduce vibrations and noise, wherein the step of changing the resonance frequency of the at least one panel includes applying a rigid damper plate over the fabric damper sheet to locate the fabric damper sheet between the damper plate and the at least one panel, and wherein the step of changing a resonance frequency of the at least one panel further includes clamping the damper plate and the fabric damper sheet to the at least one panel with a damper bracket that has a frame disposed around a perimeter of the damper plate and defines a window that opens to expose the damper plate.

### Claim 17 (depends on 16)

The method of claim 16, wherein the step of changing a resonance frequency of the at least one panel further includes clamping the damper plate and the fabric damper sheet to the at least one panel with a plurality of washers and corresponding fasteners, the plurality of washers disposed along an outer surface of the damper plate.
