Combustor thermal shield fabrication method
A method of fabricating a combustor thermal shield comprising a combustor panel, a cooling feature, and an attachment feature, the combustor thermal shield to be used in a gas turbine engine combustor, includes shaping a sheet of material used to form the combustor panel. The method also includes additively manufacturing the cooling feature onto the sheet of material forming the combustor panel. The method also includes attaching the attachment feature to the sheet of material forming the combustor panel. The method also includes curving the sheet of material forming the combustor panel to achieve a curve profile according to a design of the gas turbine engine combustor.
1. A method of fabricating a combustor thermal shield to be used in a gas turbine engine combustor, the method comprising:
shaping a sheet of material used to form a combustor panel of the combustor thermal shield;
additively manufacturing a cooling feature onto the sheet of material forming the combustor panel;
attaching an attachment feature to the sheet of material forming the combustor panel; and
after attaching the attachment feature to the sheet of material forming the combustor panel, curving the sheet of material forming the combustor panel to achieve a curve profile according to a design of the gas turbine engine combustor,
wherein attaching the attachment feature to the sheet of material forming the combustor panel comprises
creating a hole in the sheet of material forming the combustor panel;
inserting at least one of a screw or a bolt through the hole, the at least one of the screw or the bolt forming the attachment feature; and
joining the at least one of the screw or the bolt to the sheet of material forming the combustor panel by at least one of brazing, welding, or soldering.
2. The method of claim 1 , further comprising treating the sheet of material forming the combustor panel to be a substrate for the cooling feature.
3. The method of claim 1 , wherein the sheet of material comprises a metal alloy.
4. The method of claim 1 , wherein the joining comprises interference fitting.
5. The method of claim 1 , wherein a hot forming press curves the combustor panel.
6. The method of claim 1 , wherein a cold forming press curves the combustor panel.
7. The method of claim 1 , wherein the curving is performed after additively manufacturing the cooling feature and after attaching the attachment feature.
8. The method of claim 1 , wherein the curving is performed prior to additively manufacturing the cooling feature and prior to attaching the attachment feature.
9. The method of claim 1 , further comprising creating a cooling hole in the sheet of material forming the combustor panel.
10. A method of fabricating a combustor thermal shield to be used in a gas turbine engine combustor, the method comprising:
shaping a sheet of material used to form a combustor panel of the combustor thermal shield;
separately additively manufacturing a cooling feature;
joining the cooling feature onto the sheet of material forming the combustor panel;
attaching an attachment feature to the sheet of material forming the combustor panel; and
after attaching the attachment feature to the sheet of material forming the combustor panel, curving the sheet of material forming the combustor panel to achieve a curve profile according to a design of the gas turbine engine combustor,
wherein attaching the attachment feature to the sheet of material forming the combustor panel comprises
creating a hole in the sheet of material forming the combustor panel;
inserting at least one of a screw or a bolt through the hole, the at least one of the screw or the bolt forming the attachment feature; and
joining the at least one of the screw or the bolt to the sheet of material forming the combustor panel, by at least one of brazing, welding, soldering.
11. The method of claim 10 , wherein joining the cooling feature onto the sheet of material forming the combustor panel comprises at least one of brazing, welding, soldering, or interference fitting.
12. The method of claim 10 , wherein the sheet of material comprises a metal alloy.
13. The method of claim 10 , wherein joining the screw or bolt to the sheet of material comprises interference fitting.
14. The method of claim 10 , wherein curving the panel comprises using a hot forming press.
15. The method of claim 10 , wherein curving the panel comprises using a cold forming press.
16. The method of claim 10 , wherein the curving is performed after additively manufacturing the cooling feature and after attaching the attachment feature.
17. The method of claim 10 , wherein the curving is performed prior to joining the cooling feature and prior to attaching the attachment feature to the sheet of material forming the combustor panel.