Multiple axis tumbler coating apparatus
The present invention relates to an apparatus for coating one or more workpieces such as components to be used in jet engines or industrial turbines. The apparatus comprises a device for simultaneously manipulating a workpiece about multiple axes while holding a center of the workpiece at a fixed position with respect to a source of coating material. The device for manipulating the workpiece preferably comprises a modular fixture while allows the workpiece to be simultaneously rotated about a first axis, rotated about a second axis at an angle to the first axis, and titled through a range of motion such as from +45 degrees to −45 degrees with respect to the first axis.
1. An apparatus for coating at least one engine component having a center and an airfoil portion with a leading edge, a trailing edge, and a longitudinal axis, said apparatus comprising:
a modular fixture having a first end plate and a stub shaft attached to a first surface of said first end plate;
said modular fixture being rotated about a first axis defined by said stub shaft;
means for supporting said at least one engine component at an angle with respect to said first axis, said supporting means being non-movably attached to a second surface of said end plate;
said supporting means including means for allowing said engine component to rotate about said longitudinal axis so that said leading edge rotates about said trailing edge while said center of said at least one engine component is maintained at a fixed horizontal and vertical location with respect to a source of coating material.
2. An apparatus according to claim 1 , wherein said supporting means comprises an arm attached to said second surface of said first end plate and said rotation allowing means comprising a bushing having a central bore incorporated into said arm and a spindle secured to said at least one engine component and passing through said central bore.
3. An apparatus according to claim 2 , further comprising means for holding said at least one engine component attached to said spindle.
4. An apparatus according to claim 1 , further comprising a second end plate secured to said first end plate by a plurality of axially extending support bars which extend parallel to said first axis.
5. An apparatus according to claim 4 , further comprising a central support element attached to said support bars.
6. An apparatus according to claim 4 , further comprising: said supporting means attached to said second surface of said first end plate supporting a first engine component; and additional means for supporting a second engine component attached to said second end plate.
7. An apparatus according to claim 6 , wherein said additional supporting means comprises an arm attached to said second end plate and rotation allowing means comprising a bushing having a central bore incorporated into said arm attached to said second end plate and a spindle secured to said second engine component and passing through said central bore in said bushing incorporated into said arm attached to said second end plate.