Airfoil with body and cover panel
An airfoil includes a metal body that has holes, a cover panel carried on the metal body, and push fasteners that extend through the cover panel and into the holes to lock the cover panel on the metal body. Each of the push fasteners includes flexible barbs that engage sides of the holes to resist retraction of the fasteners from the holes. The heads of the push fastener are embedded in recesses in the cover panel.
1. An airfoil comprising:
a metal body having holes;
a cover panel carried on the metal body; and
push fasteners extending through the cover panel and into the holes to lock the cover panel on the metal body, each of the push fasteners including flexible barbs that engage sides of the holes to resist retraction of the fasteners from the holes, and the push fasteners including heads that are embedded in recesses in the cover panel wherein sides of the recesses are obliquely sloped with respect to a length direction of the fasteners.
2. The airfoil as recited in claim 1 , wherein the heads are flush with, or below, an exterior surface of the cover panel.
3. The airfoil as recited in claim 1 , wherein the fasteners fall short of bottoming out in the holes.
4. The airfoil as recited in claim 1 , wherein each of the push fasteners includes a head that is embedded in the cover panel.
5. The airfoil as recited in claim 1 , wherein the cover panel includes stitching adjacent the head of the push fasteners.
6. The airfoil as recited in claim 1 , wherein the holes are straight.
7. The airfoil as recited in claim 1 , further comprising an adhesive layer between the cover panel and the metal body.
8. The airfoil as recited in claim 7 , wherein the adhesive layer is disposed on a perimeter edge of the metal body.
9. The airfoil as recited in claim 1 , wherein the metal body includes a rib, the rib having a base at the metal body and, distal from the metal body, a flange that is in facial contact with the cover panel.
10. A gas turbine engine comprising:
a fan;
a compressor section;
a combustor in fluid communication with the compressor section; and
a turbine section in fluid communication with the combustor, the fan having airfoils that each include
a metal body having holes,
a cover panel carried on the metal body, and
push fasteners extending through the cover panel and into the holes to lock the cover panel on the metal body, each of the push fasteners including flexible barbs that engage sides of the holes to resist retraction of the fasteners from the holes, and the push fasteners including heads that are embedded in recesses in the cover panel wherein sides of the recesses are obliquely sloped with respect to a length direction of the fasteners.