| 摘要 |
According to one embodiment of the present disclosure, a method for working a combustor float wall panel is disclosed. The method may comprise providing a supplemental body of a combustor float wall panel, and attaching at least one cooling pin to the supplemental body. According to another embodiment, a method for working a combustor float wall panel of a gas turbine engine is disclosed. The method may comprise separating a combustor float wall panel from a combustor of a gas turbine engine, providing a supplemental body to the combustor float wall panel, attaching at least one cooling pin to the supplemental body; and returning the combustor float wall panel to the combustor of the gas turbine engine. |
