Sealing and retention system
Abstract:
A seal system for a gas turbine engine is disclosed. The seal system includes a fairing. The seal system also includes a finger seal retention unit attached to the fairing, the finger seal retention unit comprising a channel defining an opening between the fairing and the finger seal retention unit. The seal system also includes a finger seal comprising a tab corresponding to the channel of the finger seal retention unit, the finger seal configured to be removably attached to the finger seal retention unit by inserting the tab into the channel.
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