-
公开(公告)号:US20240157424A1
公开(公告)日:2024-05-16
申请号:US18345536
申请日:2023-06-30
Applicant: General Electric Company
Inventor: Joshua DEPOT , Jacob A. SALM , Jeremy E. GARD , Ellison LENZ
Abstract: The present application provides a deformation correction system for a hot gas path surface of a turbine shroud. The deformation correction system may include a first die having a curved surface and a second die such that the hot gas path surface of the turbine shroud is positioned between the first die and the second die.