Abstract: An assembly for an aircraft propulsion system includes a propulsor and an imaging assembly. The propulsor includes a propulsor disk, a plurality of propulsor blades, and a nose cone. The plurality of propulsor blades are circumferentially distributed about the propulsor disk. Each propulsor blade of the plurality of propulsor blades extends radially between and to a root end and a tip end. The root end is disposed at the propulsor disk. The propulsor disk and the plurality of propulsor blades are configured to rotate about the rotational axis. The nose cone is disposed axially adjacent the propulsor disk. The imaging assembly includes an imaging device disposed on the nose cone. The imaging device includes a camera. The camera is configured to capture image data of each propulsor blade of the plurality of propulsor blades as the plurality of propulsor blades rotate about the rotational axis.

Abstract: A method of manufacturing a thin film magnetic transducer in which a layer of photoresist material is used to pattern the turns of a bi-level electrical coil. The thickness of the photoresist layer is increased to the maximum height of the bi-level coil. A multi-turn spiral type rectangular trench is formed to define the pattern of the coil structure. In the first coil plating step, a first coil section is plated in the trench to approximately the midpoint of its height. The layer of the resist material is then cured and a blocking mask is deposited over the portion of the first coil section that is not to be further increased in height. The area of the coil that is not blocked by the blocking mask is again plated using the initial pattern until each partial turn in the unblocked section reaches the top of the groove. The cured resist material and the blocking mask are then removed.