SHROUD HANGER ASSEMBLY

摘要

A shroud hanger assembly (30) or shroud assembly (30) is provided for a gas turbine engine wherein a hanger (32) includes a radially depending and axially extending arm. The arm (45) or retainer (60) engages a pocket (56) formed in a shroud (50) so as to retain the shroud (50) in a desired position relative to the hanger (32). An aft retaining structure is provided on the hanger (32) and provides a seat for a seal structure which biases the retainer (60) so that the arm (45) of the hanger (32) maintains engagement in the shroud pocket (56). A baffle (52) may be utilized at the hanger (32) to cool at least some portion of the shroud (50).