发明授权
US07284958B2 Separable blade platform 有权
可分离刀片平台

Separable blade platform
摘要:
A gas turbine engine blade platform including a par of platform retention members. The pair of platform retention members are configured to be located on opposite sides of a disk lug. The retention members interact with the disk lug to restrain radial movement of the platform during rotation of a disk.
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