Combustor wall assembly for gas turbine engine

1. A combustor of a gas turbine engine, the combustor comprising:

an outer shell made of a metallic material;

a plurality of inner panels mounted to the outer shell, the plurality of inner panels spaced inwardly from the outer shell to define a double-wall configuration with the outer shell, the plurality of inner panels made of a ceramic material;

a damper disposed between the outer shell and a first inner panel of the plurality of inner panels; and

an insert disposed between the first inner panel and the outer shell, wherein:

the first inner panel and a second inner panel of the plurality of inner panels are positioned to define a gap therebetween;

part of the insert is disposed in the gap between the first inner panel and the second inner panel;

the part of the insert disposed in the gap includes first sealing faces oriented obliquely to a normal of an inner surface of the outer shell;

the first inner panel and the second inner panel each include a second sealing face oriented obliquely to the normal of the inner surface of the outer shell;

the first sealing faces of the insert are in respective sliding engagement with the second sealing faces of the first inner panel and of the second inner panel; and

the insert includes:

a first flange engaged with a first bracket rigidly attached to the first inner panel, the first flange being spaced apart from the outer shell; and

a second flange engaged with a second bracket rigidly attached to the second inner panel, the second flange being spaced apart from the outer shell;

wherein:

the first bracket defines a first channel separate from the outer shell, the first flange of the insert being received in the first channel; and

the second bracket defines a second channel separate from the outer shell, the second flange of the insert being received in the second channel.

2. The combustor as defined in claim 1 , wherein the damper is resilient.

3. The combustor as defined in claim 1 , wherein the damper is a spring.

4. The combustor as defined in claim 1 , wherein the damper is disposed between the outer shell and the insert.

5. The combustor as defined in claim 1 , wherein the damper is in direct engagement with the outer shell and the first inner panel.

6. The combustor as defined in claim 1 , wherein:

the damper is a first damper disposed between the insert and the outer shell; and

the combustor includes a second damper in direct engagement with the outer shell and the first inner panel.

7. The combustor as defined in claim 1 , wherein:

the damper is a first damper disposed between the insert and the outer shell; and

the combustor includes:

a second damper disposed between the outer shell and the first inner panel; and

a third damper disposed between the outer shell and the second inner panel.

8. The combustor as defined in claim 1 , wherein the part of the insert disposed in the gap between the first inner panel and the second inner panel tapers away from the outer shell.

9. The combustor as defined in claim 1 , wherein the part of the insert disposed in the gap between the first inner panel and the second inner panel tapers toward the outer shell.

10. The combustor as defined in claim 1 , wherein:

the insert is secured to the outer shell to limit movement of the insert relative to the outer shell; and

the damper is in direct engagement with the outer shell and the first inner panel.

11. The combustor as defined in claim 10 , wherein the insert is secured to the first inner panel and to the second inner panel via rigid connections.

12. The combustor as defined in claim 11 , wherein

the insert includes a third flange for securing the insert to the outer shell.

13. The combustor as defined in claim 12 , wherein the first flange is sealingly engaged with the first inner panel.

14. The combustor as defined in claim 1 , comprising a retainer secured to the outer shell for retaining the insert, wherein the damper is disposed between the insert and the outer shell.

15. The combustor as defined in claim 1 , wherein the plurality of inner panels and the insert are made from substantially a same type of material.

16. The combustor as defined in claim 1 , comprising a pin secured to the first inner panel and in sliding engagement with the outer shell.

17. A combustor of a gas turbine engine, the combustor comprising:

an outer shell;

a plurality of inner panels mounted to the outer shell, the plurality of inner panels spaced inwardly from the outer shell to define a double-wall configuration with the outer shell, the plurality of inner panels having a higher heat resistance than the outer shell;

a damper disposed between the outer shell and a first inner panel of the plurality of inner panels; and

an insert disposed between the first inner panel and the outer shell, wherein:

the first inner panel and a second inner panel of the plurality of inner panels are positioned to define a gap therebetween;

part of the insert is disposed in the gap between the first inner panel and the second inner panel;

the part of the insert disposed in the gap includes first sealing faces oriented obliquely to a normal of an inner surface of the outer shell;

the first inner panel and the second inner panel each include a second sealing face oriented obliquely to the normal of the inner surface of the outer shell; and

the first sealing faces of the insert are in respective sliding engagement with the second sealing faces of the first inner panel and of the second inner panel;

the insert includes:

a first flange engaged with a first bracket of the first inner panel, the first flange being spaced apart from the outer shell; and

a second flange engaged with a second bracket of the second inner panel, the second flange being spaced apart from the outer shell;

wherein:

the first bracket of the first inner panel defines a first channel separate from the outer shell, the first flange of the insert being received in the first channel; and

the second bracket of the second inner panel defines a second channel separate from the outer shell, the second flange of the insert being received in the second channel.

18. The combustor as defined in claim 17 , wherein the first sealing faces of the insert are oriented at an angle of between 30° and 60° from the normal of the inner surface of the outer shell.

19. The combustor as defined in claim 1 , comprising:

a first seal disposed between the first flange and the first bracket; and

a second seal disposed between the second flange and the second bracket.