SEALING CONFIGURATION TO REDUCE AIR LEAKAGE
    1.
    发明申请

    公开(公告)号:US20200025038A1

    公开(公告)日:2020-01-23

    申请号:US16037270

    申请日:2018-07-17

    Abstract: A seal assembly for a fluid transfer tube in a gas turbine engine is disclosed. In various embodiments, the seal assembly includes a boot seal configured to surround a length of the fluid transfer tube, the boot seal having a first end and a second end and a seal ring disposed at the first end, an attachment ring configured to mate with the seal ring and to secure the seal ring against a casing, an annular ring configured to mate with an interior surface of the boot seal at the second end and to surround a portion of the fluid transfer tube, and a clamp ring configured to surround the second end of the boot seal proximate the annular ring.

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