Article and method for manufacturing an expanded combustor liner
A method of manufacturing a nested combustor liner includes manufacturing a nested combustor liner into a green state including a plurality of annular interior walls radially adjacent to one another and circumferentially surrounding an exhaust duct aperture and a plurality of annular exterior walls radially adjacent to one another and radially spaced apart from and circumferentially surrounding the plurality of annular interior walls and an ignitor wall attached to a first annular interior wall at a first interior end, extending radially toward and attached to a first annular exterior wall at a first exterior end. The method includes assembling the plurality of annular interior walls and the plurality of annular exterior walls, forming an assembled combustor liner. The method includes densifying the assembled combustor liner.
1 . A combustor liner, comprising:
a plurality of extended annular interior walls circumferentially surrounding an exhaust duct aperture, wherein each of the plurality of extended annular interior walls is radially adjacent to and axially extended from at least one other of the plurality of extended annular interior walls and a first annular interior wall includes a first interior flange extending radially away from the exhaust duct aperture and wherein a second annular interior wall has a second interior flange extending radially inward toward the first annular interior wall;
a plurality of extended annular exterior walls radially spaced apart from and circumferentially surrounding the plurality of annular interior walls, wherein each of the plurality of extended annular exterior walls is radially adjacent to and axially extended from at least one other of the plurality of extended annular exterior walls and a first annular exterior wall includes a first exterior flange extending radially away from the first annular interior wall and wherein a second annular exterior wall has a second exterior flange extending radially inward toward the first annular exterior wall;
an ignitor wall attached to a first interior wall end of the first annular interior wall and attached to a first exterior wall end of the first annular exterior wall;
a first compressible seal compressed between the first annular interior wall and the second annular interior wall and between the first interior flange and the second interior flange; and
a second compressible seal compressed between the first annular exterior wall and the second annular exterior wall and between the first exterior flange and the second exterior flange.
2 . The combustor liner of claim 1 , wherein the plurality of extended annular interior walls, the plurality of extended annular exterior walls, and the ignitor wall include nickel or a nickel-based alloy.
3 . An assembly for a turbine engine, comprising:
a plurality of interior walls of a combustor liner arranged axially along an exhaust duct aperture, each of the plurality of interior walls circumscribing the exhaust duct aperture, the plurality of interior walls including a first interior wall and a second interior wall, the second interior wall radially adjacent and projecting axially out from the first interior wall, the first interior wall comprising a first interior flange projecting radially outward away from the exhaust duct aperture, the second interior wall comprising a second interior flange projecting radially inwards towards the exhaust duct aperture, and the first interior flange axially engaged with the second interior flange;
a plurality of exterior walls of the combustor liner arranged axially along the exhaust duct aperture, each of the plurality of exterior walls circumscribing the plurality of interior walls, the plurality of exterior walls including a first exterior wall and a second exterior wall, the second exterior wall radially adjacent and projecting axially out from the first exterior wall, the first exterior wall comprising a first exterior flange projecting radially outward away from the exhaust duct aperture, the second exterior wall comprising a second exterior flange projecting radially inwards towards the exhaust duct aperture, and the first exterior flange axially engaged with the second exterior flange;
an endwall attached to and extending radially between one of the plurality of interior walls and one of the plurality of exterior walls; and
an interior seal element disposed axially between and contacting the first interior flange and the second interior flange.
4 . The assembly of claim 3 , wherein the endwall is attached to the first interior wall and the first exterior wall.
5 . The assembly of claim 3 , wherein the interior seal element is compressed axially between the first interior flange and the second interior flange.
6 . The assembly of claim 3 , wherein the interior seal element comprises a C-seal element.
7 . The assembly of claim 3 , wherein the endwall is an ignitor wall.
8 . The assembly of claim 3 , wherein the endwall circumscribes a centerline of the combustor liner.
9 . The assembly of claim 3 , wherein
the plurality of interior walls form a radial inner wall of the combustor liner;
the plurality of exterior walls form a radial outer wall of the combustor liner; and
a combustion chamber is disposed radially between the radial inner wall and the radial outer wall, and the combustion chamber extends axially along the radial inner wall and the radial outer wall to the endwall.
10 . The assembly of claim 3 , wherein the plurality of interior walls comprises nickel.
11 . The assembly of claim 3 , wherein the plurality of exterior walls comprises nickel.
12 . The assembly of claim 3 , wherein the endwall comprises nickel.
13 . An assembly for a turbine engine, comprising:
a plurality of interior walls of a combustor liner arranged axially along an exhaust duct aperture, each of the plurality of interior walls circumscribing the exhaust duct aperture, the plurality of interior walls including a first interior wall and a second interior wall, the second interior wall radially adjacent and projecting axially out from the first interior wall, the first interior wall comprising a first interior flange projecting radially outward away from the exhaust duct aperture, the second interior wall comprising a second interior flange projecting radially inwards towards the exhaust duct aperture, and the first interior flange axially engaged with the second interior flange;
a plurality of exterior walls of the combustor liner arranged axially along the exhaust duct aperture, each of the plurality of exterior walls circumscribing the plurality of interior walls, the plurality of exterior walls including a first exterior wall and a second exterior wall, the second exterior wall radially adjacent and projecting axially out from the first exterior wall, the first exterior wall comprising a first exterior flange projecting radially outward away from the exhaust duct aperture, the second exterior wall comprising a second exterior flange projecting radially inwards towards the exhaust duct aperture, and the first exterior flange axially engaged with the second exterior flange;
an endwall attached to and extending radially between one of the plurality of interior walls and one of the plurality of exterior walls; and
an exterior seal element disposed axially between and contacting the first exterior flange and the second exterior flange.
14 . The assembly of claim 13 , wherein the exterior seal element is compressed axially between the first exterior flange and the second exterior flange.
15 . The assembly of claim 13 , wherein the exterior seal element comprises a C-seal element.
16 . The assembly of claim 13 , wherein the endwall is an ignitor wall.
17 . The assembly of claim 13 , wherein the endwall circumscribes a centerline of the combustor liner.
18 . The assembly of claim 13 , wherein
the plurality of interior walls form a radial inner wall of the combustor liner;
the plurality of exterior walls form a radial outer wall of the combustor liner; and
a combustion chamber is disposed radially between the radial inner wall and the radial outer wall, and the combustion chamber extends axially along the radial inner wall and the radial outer wall to the endwall.
19 . The assembly of claim 13 , wherein at least one of:
the plurality of interior walls comprises nickel; or
the plurality of exterior walls comprises nickel.
20 . The assembly of claim 13 , wherein the endwall comprises nickel.