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US 2016/0251982 A1Published application
Method and system for a ceramic matrix composite shroud hanger assembly
AssigneeGeneral Electric Company
InventorJason David Shapiro
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AssigneeGeneral Electric Company
InventorJason David Shapiro
Estimating the term…
A shroud and hanger assembly for a gas turbine engine and a method of transferring load from a ceramic matrix composite (CMC) shroud to a CMC shroud hanger assembly are provided. The shroud and hanger assembly includes a shroud hanger assembly formed of a first material having a first coefficient of thermal expansion, the shroud hanger assembly having a forward hanger portion and a separate aftward hanger portion and a shroud formed of a second material having a second coefficient of thermal expansion, the forward and aftward hanger portions configured to couple together to clamp across a forward radially extending wall of the shroud.
A shroud and shroud hanger assembly for a gas turbine engine, said assembly comprising:
A method of transferring load from a ceramic matrix composite (CMC) shroud to a CMC shroud hanger assembly, said method comprising:
A gas turbine engine comprising:
Dependencies are inferred from the claim text.