BLADE TRACK APPARATUS AND METHOD OF ASSEMBLING A BLADE TRACK APPARATUS

An apparatus comprises a gas turbine engine having a blade track segment circumferentially extending between a first arc end and a second arc end. The blade track segment has a radially inner side and a radially outer side. The radially outer side has a raised seal portion disposed near the first ar...

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Bibliographische Detailangaben
Hauptverfasser: GRIFFITHS, George, F, WESTPHAL, William, FREEMAN, Ted, Joseph, SMITH, Clayton, C
Format: Patent
Sprache:eng ; fre ; ger
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Beschreibung
Zusammenfassung:An apparatus comprises a gas turbine engine having a blade track segment circumferentially extending between a first arc end and a second arc end. The blade track segment has a radially inner side and a radially outer side. The radially outer side has a raised seal portion disposed near the first arc end of the blade track segment and structured to engage a sealing member to discourage passage of a working fluid between the inner side and the outer side. A corresponding method of assembly is also provided.