Airfoil including adhesively bonded shroud
An airfoil includes an airfoil body that extends between a leading edge and a trailing edge, a suction side and a pressure side, and a first end and a second end, a fitting located at one of the first end or the second end, the fitting including a body portion, a fillet portion, and a neck portion joining the body portion and the neck portion, the neck portion including a shelf, a fastener through the airfoil body, and a shroud having a complementary shape to the shelf such that the shroud nests in the shelf.
1. An airfoil comprising:
an airfoil body extending between a leading edge and a trailing edge, a suction side and a pressure side, and a first end and a second end;
a fitting located at one of the first end or the second end, the fitting including a body portion, a fillet portion, and a neck portion joining the body portion and the fillet portion, the neck portion including a shelf and there being a slot that extends through the fillet portion, the neck portion, and the body portion, the airfoil body extending in the slot;
a fastener through the body portion and the airfoil body; and
a shroud having a complementary shape to the shelf such that the shroud nests in the shelf.
2. The airfoil as recited in claim 1 , wherein the shroud comprises a polymeric material.
3. The airfoil as recited in claim 1 , wherein the fitting is metallic and the shroud is polymeric.
4. The airfoil as recited in claim 1 , further comprising a seal member at a perimeter edge of the shroud.
5. The airfoil as recited in claim 4 , wherein the perimeter edge includes a groove that is complementary in shape to the seal member.
6. The airfoil as recited in claim 5 , wherein the groove has a cross-sectional profile of a partial circle.
7. A turbine engine comprising a fan section including the airfoil as recited in claim 1 , a compressor section in communication with the fan section, a combustor in fluid communication with the compressor section, and a turbine section in fluid communication with the combustor.
8. The airfoil as recited in claim 1 , wherein the fillet portion extends from the neck portion and opposite from the fillet portion the body portion extend from the neck portion.
9. The airfoil as recited in claim 8 , wherein the airfoil body includes a though-hole from the suction side to the pressure side, and the fastener is disposed through the through-hole.