Invention Grant
US09458726B2 Dovetail retention system for blade tracks 有权
叶片轨道的燕尾保留系统

Dovetail retention system for blade tracks
Abstract:
A turbine shroud for a gas turbine engine includes a metallic support ring and a ceramic blade track. The blade track is formed from a plurality of blade track segments including dovetail posts. The dovetail posts are inserted through apertures in the support ring and are coupled to the support ring by segment retainers coupled to the dovetail posts providing a retention system for the ceramic blade track.
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