Gas Turbine Engine And Method Of Assembling The Same

Abstract: GAS TURBINE ENGINE AND METHOD OF ASSEMBLING THE SAME ABSTRACT OF THE DISCLOSURE A gas turbine engine having a centerline axis is provided. The gas turbine engine includes a fan and a fan cowl assembly surrounding the fan to define a bypass duct configured to channel airflow for the fan. The fan cowl assembly includes a stationary cowl and a transcowl. The gas turbine engine further includes a plurality of actuators configured for displacing the transcowl relative to the stationary cowl. Each of the actuators is skewed relative to the centerline axis of the engine. FIG. 1

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