GAS TURBINE ENGINE BLADE OUTER AIR SEAL

A gas turbine engine sealing system includes a case (50) including forward and aft hooks (62, 64). The aft hook (64) is arranged radially outward of the forward hook (62). A blade outer air seal (65) has a J-hook (68) that receives the aft hook (64) and includes an end (72) received by the forward h...

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Bibliographische Detailangaben
Hauptverfasser: McCAFFREY, Michael G, EASTWOOD, Jonathan Jeffery, ENGLEHART, Joseph F, VENABLE, Christopher Carter
Format: Patent
Sprache:eng ; fre ; ger
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Zusammenfassung:A gas turbine engine sealing system includes a case (50) including forward and aft hooks (62, 64). The aft hook (64) is arranged radially outward of the forward hook (62). A blade outer air seal (65) has a J-hook (68) that receives the aft hook (64) and includes an end (72) received by the forward hook (62).