CLEARANCE CONTROL ASSEMBLY WITH SPECIFIC ASSEMBLY OF A CLEARANCE CONTROL RING

A clearance control assembly for a gas turbine engine includes a clearance control ring to position a blade outer air seal assembly radially relative to a blade tip. The clearance control ring is compression fit to the blade outer air seal assembly.

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Bibliographische Detailangaben
Hauptverfasser: RIOUX, Philip Robert, TATMAN, Neil L
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
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Beschreibung
Zusammenfassung:A clearance control assembly for a gas turbine engine includes a clearance control ring to position a blade outer air seal assembly radially relative to a blade tip. The clearance control ring is compression fit to the blade outer air seal assembly.