| 摘要 |
A gas turbine engine (10) is provided. The gas turbine engine (10) includes an engine casing structure (69) and a part retained relative to the engine casing structure (69) by a channel-cooled hook (71, 73, 75; 171, 173, 175). The channel-cooled hook (71, 73, 75; 171, 173, 175) includes at least a portion of a hook cooling channel (176). A vane assembly (41; 410) for the gas turbine engine (10) is also provided. |
