Apparatus and method for masking under platform areas of airfoil components
A fixture for masking a gas turbine engine blade, the blade having a root, a platform and an airfoil, the platform having inner and outer surfaces and peripheral faces extending between the surfaces, the fixture including a base with a receptacle for receiving the root of the blade; a removable sidewall mountable to the base to form a masking box with the receptacle that shields the root; a first removable Z plane detail mountable to the base, the first removable Z plane detail providing a first electrical contact point to the root; and a second removable Z plane detail mountable to the removable sidewall, the second removable Z plane detail providing a second electrical contact point to the root.
1. A fixture for masking a gas turbine engine blade, the blade having a root, a platform and an airfoil, the fixture comprising:
a base with a receptacle for receiving the root of the blade;
a removable sidewall mountable to the base to form a masking box with the receptacle that shields the root of the blade;
a first removable Z plane detail mountable to the base, the first removable Z plane detail shaped to interface with a root serration of the root to form a first electrical contact point with the gas turbine engine blade, wherein the first removable Z plane detail comprises a tab that extends through a slot in the base to form the first electrical contact point to the root;
a second removable Z plane detail mountable to the removable sidewall, the second removable Z plane detail providing a second electrical contact point to the root, wherein the second removable Z plane detail comprises a tab that extends through a slot in the removable sidewall to form the second electrical contact point to the root; and
a fastener configured to mount through the removable sidewall, the first removable Z plane detail, the second removable Z plane detail, and the base, wherein the fastener is configured to retain the first removable Z plane detail to the base, the second removable Z plane detail to the removable sidewall and the removable sidewall to the base to sandwich the root of the blade therein.
2. The fixture as recited in claim 1 , wherein the tab includes a rectilinear polygon shaped end surface.
3. The fixture as recited in claim 1 , wherein the removable sidewall includes a first and a second edge rail that at least partially surrounds a forward wall and an aft wall of the receptacle to orient the removable sidewall to form the masking box.
4. The fixture as recited in claim 1 , wherein at least one of the first removable Z plane detail and the second Z plane detail includes a hexagonal aperture for a head of the fastener.
5. The fixture as recited in claim 1 , wherein the base includes an indentation to receive the first removable Z plane detail.
6. The fixture as recited in claim 1 , wherein the removable sidewall includes an indentation to receive the second removable Z plane detail.
7. The fixture as recited in claim 1 , further comprising a shank that extends from said base, said shank defines a longitudinal axis, the longitudinal axis being parallel to an axis of the blade.
8. The fixture as recited in claim 1 , wherein the Z-plane is a reference surface upon which the root serration of the root is referenced with a turbine rotor disk.
9. The fixture as recited in claim 1 , wherein the first removable Z plane detail is mountable to the base opposite the receptacle that shields the root of the blade.
10. The fixture as recited in claim 1 , wherein the second removable Z plane detail is mountable to the removable sidewall opposite the receptacle that shields the root of the blade.