Line-of-sight coating fixture and apparatus
An embodiment of a line-of-sight coating fixture includes a support structure, a spindle, and a shadow structure. The support structure includes a plurality of compartments disposed below a platter, each compartment having an opening on a periphery of the support structure. Each compartment is adapted to receive and secure a base of a workpiece such that a body of each workpiece to be coated is disposed about a periphery of the support structure and extends above the platter. The spindle is disposed through a center of the platter or support structure for rotating the workpieces thereabout. The shadow structure is disposed about the spindle, inside of the periphery, the shadow structure sized and adapted to shield a portion of each workpiece from line-of-sight coating material.
1. A line-of-sight coating apparatus comprising:
a coating chamber defined by at least one wall;
a plurality of coating fixtures within the coating chamber, each of the plurality of coating fixtures comprising:
a support structure;
a platter;
a plurality of compartments disposed below the platter and partially defined by the platter, each of the plurality of compartments being separately enclosable by a respective hinged door disposed on a periphery of the support structure;
wherein each of the plurality of compartments adapted to receive and secure a root of a rotor blade such that the root is disposed below the platter and an airfoil of the rotor blade extends above the platter; and
wherein each of the plurality of compartments further comprises a respective removable insert adapted to conform to the root of the rotor blade, the insert being removable from a respective one of the plurality of compartments;
a spindle disposed through a center of the support structure for rotating a plurality of rotor blades thereabout; and
a shadow structure disposed about the spindle, above the platter and inside of the periphery, the shadow structure comprising a plurality of individual shadow bars disposed with rotational symmetry about the spindle; and
a line-of-sight coating source disposed along the at least one wall and directed toward the plurality of coating fixtures.
2. The apparatus of claim 1 , wherein plurality of coating fixtures are arranged linearly or longitudinally opposed to the coating source.
3. The apparatus of claim 1 , wherein the coating source includes an electron beam physical vapor deposition (EB-PVD) coating source.
4. The apparatus of claim 1 , wherein each platter is shaped to conform to a platform of each of the plurality of rotor blades, such that an upper surface of the platform is exposed to the line-of-sight coating source and a lower surface of the platform is shielded from the line-of-sight coating source.
5. The apparatus of claim 1 , wherein each of the plurality of shadow bars comprises abutting walls defining a recess for separately covering a trailing edge of each airfoil and shielding the trailing edge of each airfoil from coating material from the line-of-sight coating source.
6. The apparatus of claim 5 , wherein the recess defined by the abutting walls of each of the plurality of shadow bars also covers a portion of a pressure surface of the airfoil adjacent to the trailing edge.
7. The apparatus of claim 1 , wherein the removable insert includes a first insert piece and a second insert piece, each of the first and second insert pieces having an inner side wall with at least one lobe.
8. The apparatus of claim 1 , wherein a span of each airfoil is aligned with a rotational axis of the spindle.
9. The apparatus of claim 5 , wherein for each of the plurality of compartments, the root of the rotor blade is oriented such that the trailing edge is the radially innermost portion of the airfoil with respect to the spindle.
10. The apparatus of claim 1 , wherein all of the plurality of compartments are distributed with rotational symmetry about the spindle.