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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Format: | Patent |
Sprache: | eng ; fre ; ger |
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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. |
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