| 摘要 |
A bracket assembly for securing a transition segment to a combustion liner of a gas turbine engine includes at least one flange mounted to the transition segment. The at least one flange includes a channel that extends radially from the transition segment. The bracket assembly further includes a bracket fixedly mounted relative to the gas turbine engine. The bracket includes an elongated section having at least one end section that is received by the channel to establish an axial floating interface that secures the transition segment to the combustion liner.
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