| 摘要 |
<p>A rotor assembly (100) is disclosed. The rotor assembly (100) may include a first rotor disk (102) defining a first axially extending slot (114) and a second rotor disk (104) defining a second axially extending slot (116). Additionally, the rotor assembly (100) may include a pin (108) extending lengthwise between the first and second rotor disks (102, 104). The pin (108) may include a first end (110) terminating within the first axially extending slot (114) and a second end (112) terminating within the second axially extending slot (116). A corresponding gas turbine engine (10) is also disclosed.</p> |
