Sound absorbing structure

Claim 2

A sound absorbing liner of the type mounted to the case of a gas turbine engine, wherein the improvement comprises: a liner having at least one sound absorbing panel having an upstream wall, a downstream wall, an inner wall and an outer wall each of which is adapted to contact means formed of viscoelastic material; means formed of viscoelastic material which extends from at least one of the said walls of the panel to the case for mounting the panel within the case and which is trapped by the wall of the panel and the case between the wall of the panel and the case for spacing the panel apart from the engine case to isolate the panel from mechanically induced vibrations in the engine case and to absorb acoustically induced vibrations in the liner.

Claim 3

A sound absorbing structure for a gas turbine engine of the type having a flowpath extending axially therethrough, which comprises: an engine case having a circumferentially extending groove which adapts the case to receive a liner; an acoustic liner having at least one sound absorbing panel facing the engine flowpath disposed in the groove in the case, the panel of the liner having an inner wall, an outer wall, an upstream wall and a downstream wall, each of which is adapted to contact means formed of viscoelastic material, and having means formed of viscoelastic material extending between at least one wall of the panel and the case for mounting the panel to the engine case and trapped by the wall of the panel and the case between the wall of the panel and the case for spacing said panel apart from the engine case; wherein the means formed of viscoelastic material isolates the sound absorbing panel of the liner from mechanically induced vibrations in the engine case and damps acoustically induced vibrations in the liner.

Claim 4

A sound absorbing structure for a gas turbine engine of the type having a flowpath extending axially therethrough, which comprises: an engine case having a circumferentially extending groove which adapts the case to receive a liner; an acoustic liner having at least one sound absorbing panel facing the engine flowpath disposed in the groove in the case, the panel of the liner having an inner wall, an outer wall, an upstream wall and a downstream wall, each of which is adapted to contact means formed of viscoelastic material, and having means formed of viscoelastic material extending between at least one wall of the panel and the case for mounting the panel to the engine case and trapped by the wall of the panel and the case between the wall of the panel and the case for spacing said panel apart from the engine case; wherein the means formed of viscoelastic material isolates the sound absorbing panel of the liner from mechanically induced vibrations in the engine case and damps acoustically induced vibrations in the liner.

Claim 5

A sound absorbing liner of the type mounted to the case of a gas turbine engine and disposed in a circumferentially extending groove in the case, wherein the improvement comprises: a liner having at least one sound absorbing panel having an upstream wall, a downstream wall, an inner wall, and an outer wall, each of which is adapted to contact means formed of viscoelastic material, the inner wall and the outer wall adapting the panel of the liner to extend radially inwardly of a portion of the case and to extend radially outwardly of a portion of the case; and, means formed of viscoelastic material which extends from at least one of said walls of the panel to the case for mounting the panel within the case, the means being trapped by the wall of the panel and the case between the wall of the panel and the case for spacing the panel apart from the engine case to isolate the panel from mechanically induced vibrations in the engine case and to absorb acoustically induced vibrations in the liner.

Claim 6

A sound absorbing liner of the type mounted to the case of a gas turbine engine and disposed in a circumferentially extending groove in the case, wherein the improvement comprises: a liner having at least one sound absorbing panel having an upstream wall, a downstream wall, an inner wall, and an outer wall, each of which is adapted to contact means formed of viscoelastic material, the inner wall and the outer wall adapting the panel of the liner to extend radially inwardly of a portion of the case and to extend radially outwardly of a portion of the case; and, means formed of viscoelastic material which extends from at least one of said walls of the panel to the case for mounting the panel within the case, the means being trapped by the wall of the panel and the case between the wall of the panel and the case for spacing the panel apart from the engine case to isolate the panel from mechanically induced vibrations in the engine case and to absorb acoustically induced vibrations in the liner.

Claim 7

A sound absorbing structure for a gas turbine engine of the type having a flowpath extending axially therethrough, which comprises: an engine case having a circumferentially extending groove which adapts the case to receive an acoustic liner; an acoustic liner disposed in the groove in the case such that a portion of the case is radially inwardly of the liner and a portion of the case is radially outwardly of the liner, the liner having at least one sound absorbing panel facing the engine flowpath which is disposed in said groove and which has an inner wall, and outer wall, an upstream wall and a downstream wall, each of which adapts the panel to contact means formed of viscoelastic material, and means formed of viscoelastic material which extends between a wall of the panel and the case for mounting the panel to the engine case and which is trapped by said wall of the panel and the case between the wall of the panel and the case for spacing said panel apart from the engine case; wherein the means of viscoelastic material isolates the sound absorbing panel of the liner from mechanically induced vibrations in the engine case and damps acoustically induced vibrations in the liner.

Claim 8

A sound absorbing structure for a gas turbine engine of the type having a flowpath extending axially therethrough, which comprises: an engine case having a circumferentially extending groove which adapts the case to receive an acoustic liner; an acoustic liner disposed in the groove in the case such that a portion of the case is radially inwardly of the liner and a portion of the case is radially outwardly of the liner, the liner having at least one sound absorbing panel facing the engine flowpath which is disposed in said groove and which has an inner wall, and outer wall, an upstream wall and a downstream wall, each of which adapts the panel to contact means formed of viscoelastic material, and means formed of viscoelastic material which extends between a wall of the panel and the case for mounting the panel to the engine case and which is trapped by said wall of the panel and the case between the wall of the panel and the case for spacing said panel apart from the engine case; wherein the means of viscoelastic material isolates the sound absorbing panel of the liner from mechanically induced vibrations in the engine case and damps acoustically induced vibrations in the liner.

Claim 9

The invention as claimed in claim 1 or claim 3 wherein the liner is formed of a plurality of panels which are spaced circumferentially about the engine.

Claim 10

The invention as claimed in claim 5 which further includes viscoelastic material disposed circumferentially between each pair of adjacent panels.

Claim 11

The invention as claimed in claim 2 or claim 4 wherein the panel of the liner extends circumferentially about the engine case, wherein said wall of the panel from which said means formed of viscoelastic material extends is a first wall, wherein one of the remaining walls is a second wall, wherein the second wall abuts the engine case, and wherein said means formed of viscoelastic material for providing viscous damping of induced vibrations is trapped between the engine case and the first wall for urging the second wall into contact with the engine case to provide frictional damping of induced vibrations.

Claim 12

The invention as claimed in claim 7 wherein said first wall is substantially perpendicular to said second wall.

Claim 13

The invention as claimed in claim 7 wherein said first wall and said second wall are spaced apart to form one or more first cavities therebetween for absorbing acoustic vibrations, and wherein said second wall bounds the working medium flowpath and has a plurality of passages therethrough placing said first cavities in gas communication with the flowpath; wherein one or more second cavities are formed between the first wall and the case for absorbing acoustic vibrations and wherein the first wall has a plurality of passages therethrough placing each of said first cavities in gas communication with one or more of said second cavities.

Claim 14

The invention as claimed in claim 2 or claim 4 wherein the panel of the liner extends circumferentially about the engine case wherein said wall of the panel from which said means formed of viscoelastic material extends is a first wall, wherein one of the remaining walls of the panel is a second wall spaced from the engine case, and a second means of viscoelastic material is trapped between said second wall and said case for mounting and for spacing apart the second wall of the panel of the liner from the engine case.

Claim 15

The invention as claimed in claim 10 wherein said first wall is substantially perpendicular to said second wall.

Claim 16

The invention as claimed in claim 10 wherein said first wall and said second wall are spaced apart to form one or more first cavities therebetween for absorbing acoustic vibrations, and wherein said second wall bounds the working medium flowpath and has a plurality of passages therethrough placing said first cavities in gas communication with the flowpath; wherein one or more second cavities are formed between the first wall and the case for absorbing acoustic vibrations and wherein the first wall has a plurality of passages therethrough placing each of said first cavities in gas communication with one or more of said second cavities.