GAS TURBINE ENGINE ACTIVE CLEARANCE CONTROL SYSTEM
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United States of America Patent
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Jul 27, 2016
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Jul 27, 2016
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Abstract
A gas turbine engine includes a blade having a tip, a blade outer air seal operatively connected to a case assembly, and an active clearance control system disposed on the case assembly. The active control system includes an actuator assembly. The actuator assembly includes a motor assembly and a shaft. The shaft has a shaft body that extends between a first end that is operatively connected to the motor assembly and a second end that is operatively connected to the blade outer air seal.
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