Invention Grant
US09534500B2 Seal arrangement for segmented gas turbine engine components 有权
分段燃气涡轮发动机部件的密封装置

Seal arrangement for segmented gas turbine engine components
Abstract:
A seal arrangement for segmented turbine components comprises a sealing strip and a resilient cord element compressed against the strip to provide positive loading of the strip against the segment sealing faces. The sealing strip and the resilient cord element are engaged in confronting cavities defined in the end faces of adjacent segments. The resilient cord element is commonly held by both segments in a compressed state against the sealing strip.
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