Retractable seal system

The present application thus provides a retractable seal system (100) for use between a high pressure side (135) and a low pressure side (145) of a turbine engine (10). The retractable seal system (100) may include a seal (130) positioned in a slot (140) of a stationary component (110), a pressure b...

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Bibliographische Detailangaben
Hauptverfasser: Sha, Karimulla Shaika, Crum, Gregory, Kumar, Siddarth, Samudrala, Omprakash
Format: Patent
Sprache:eng ; fre ; ger
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Zusammenfassung:The present application thus provides a retractable seal system (100) for use between a high pressure side (135) and a low pressure side (145) of a turbine engine (10). The retractable seal system (100) may include a seal (130) positioned in a slot (140) of a stationary component (110), a pressure balance pocket (220) positioned about the seal (130), and a conduit (230) in communication with the pressure balance pocket (220) and the high pressure side (135).