Fan blade for a gas turbine engine
An airfoil includes an airfoil body portion that has a pressure side and a suction side. A recessed area in the airfoil body portion is located on one of the pressure side or the suction side. At least one rib divides the recessed area into at least one geometric shape. A cover encloses the recessed area and includes at least one pedestal that engages a distal end of at least one rib. A weld extends through the cover and a portion of at least one rib. The weld spans a width of the distal end of at least one rib.
1. An airfoil comprising:
an airfoil body portion having a pressure side and a suction side;
a recessed area in the airfoil body portion located on one of the pressure side or the suction side;
at least one rib dividing the recessed area into at least one geometric shape;
a cover enclosing the recessed area and including at least one pedestal engaging a distal end of the at least one rib and the at least one pedestal includes a rib contact surface having a width greater than a width of the distal end of the at least one rib; and
a weld extending through the cover and a portion of the at least one rib, wherein the weld spans a width of the distal end of the at least one rib and the weld circumscribes the geometric shape and forms a continuous loop following the geometric shape.
2. The airfoil of claim 1 , wherein the at least one geometric shape is closed form.
3. The airfoil of claim 1 , wherein the at least one geometric shape includes at least one of an elliptical shape or a circular shape.
4. The airfoil of claim 1 , further comprising an indentation defining a perimeter of the recessed area and a perimeter weld extending through the cover into a portion of the body portion defining the indentation, wherein the perimeter weld circumscribes the recessed area.
5. The airfoil of claim 4 , wherein the perimeter weld includes an overlapping weld portion.
6. The airfoil of claim 4 , wherein the indentation includes a perimeter ledge for engaging an inner surface of the cover and a perimeter wall for engaging an edge of the cover.
7. The airfoil of claim 1 , wherein a ratio of a radius of a pedestal fillet to a width of the pedestal between the weld and the fillet is between 0.3 and 5.0.
8. The airfoil of claim 1 , wherein the distal end of the at least one rib includes a width greater than a width of a mid-portion of the at least one rib.
9. The airfoil of claim 1 , wherein the weld includes an overlapping weld portion.
10. An airfoil comprising:
an airfoil body portion having a pressure side and a suction side;
a recessed area in the airfoil body portion located on one of the pressure side or the suction side;
at least one rib dividing the recessed area into at least one geometric shape;
a cover enclosing the recessed area and including at least one pedestal engaging a distal end of the at least one rib; and
a weld extending through the cover and a portion of the at least one rib, wherein the weld spans a width of the distal end of the att least one rib, the weld circumscribes the geometric shape and forms a continuous loop following the geometric shape, and the weld includes an overlapping weld portion.
11. A method of forming an airfoil comprising the steps of:
forming a recessed area into an airfoil body portion, wherein the recessed area includes at least one rib dividing the recessed area into at least one geometric shape;
locating a cover over the recessed area, wherein the cover includes at least one pedestal engaging a distal end of the at least one rib and the at least one pedestal includes a rib contact surface having a width greater than a width of the distal end of the at least one rib; and
welding through the cover into a portion of the at least one rib to form a weld, wherein the weld spans a width of the distal end of the at least one rib and circumscribes the geometric shape and forms a continuous loop following the geometric shape.
12. The method of claim 11 , wherein welding through the cover into a portion of the at least one rib to form a weld includes an overlapping weld portion.
13. The method of claim 11 , further comprising forming an indentation in the airfoil body portion around a perimeter of the recessed area.
14. The method of claim 13 , further comprising welding a perimeter weld through the cover into a portion of the airfoil body portion defining the indentation, wherein the perimeter weld circumscribes the indentation.
15. The method of claim 14 , wherein the perimeter weld includes an overlapping weld portion.
16. The method of claim 13 , wherein the indentation includes a perimeter ledge for engaging an inner surface of the cover and a perimeter wall for engaging an edge of the cover.
17. The method of claim 11 , further comprising machining an exterior surface of the airfoil including a portion of the weld.