Self-stressing shape memory alloy-fiber reinforced polymer patch
A self-stressing shape memory alloy (SMA)/fiber reinforced polymer (FRP) composite patch is disclosed that can be used to repair cracked steel members or other civil infrastructures. Prestressed carbon FRP (CFRP) patches have emerged as a promising alternative to traditional methods of repair. However, prestressing these patches typically requires heavy and complex fixtures, which is impractical in many applications. This disclosure describes a new approach in which the prestressing force is applied by restraining the shape memory effect of nickel titanium niobium alloy (NiTiNb) SMA wires. The wires are subsequently embedded in an FRP overlay patch. This method overcomes the practical challenges associated with conventional prestressing.
1. A self-stressing composite patch for repair of damage to a structural element, comprising:
one or more wires comprising a prestrained shape memory alloy (SMA), wherein the wires have terminal ends; and
tabs comprising fiber reinforced polymer (FRP) located on the terminal ends of the wires, wherein the terminal ends of the wires are embedded in the tabs over a terminal embedment length, and wherein a central portion of the wires is not embedded in the tabs.
2. The self-stressing composite patch of claim 1 , further comprising a fiber reinforced polymer (FRP) overlay patch having a size designed to completely overlay the wires and the tabs after placement on the structural element.
3. The self-stressing composite patch of claim 2 , wherein the fiber reinforced polymer (FRP) of the overlay patch comprises carbon fibers embedded in an epoxy-based saturating resin.
4. The self-stressing composite patch of claim 2 , wherein the fiber reinforced polymer (FRP) of the overlay patch is carbon fiber reinforced polymer (CFRP), glass fiber reinforced polymer (GFRP), aramid fiber reinforced polymer (AFRP), steel fiber reinforced polymer (SFRP), or basalt fiber reinforced polymer (BFRP).
5. The self-stressing composite patch of claim 1 , wherein the shape memory alloy (SMA) is ternary nickel titanium niobium alloy (NiTiNb).
6. The self-stressing composite patch of claim 1 , wherein the fiber reinforced polymer (FRP) of the tabs comprises carbon fibers embedded in an epoxy-based saturating resin.
7. The self-stressing composite patch of claim 1 , wherein the fiber reinforced polymer (FRP) of the tabs is carbon fiber reinforced polymer (CFRP), glass fiber reinforced polymer (GFRP), aramid fiber reinforced polymer (AFRP), steel fiber reinforced polymer (SFRP), or basalt fiber reinforced polymer (BFRP).
8. The self-stressing composite patch of claim 1 , wherein the tabs have a length of about 180 mm.
9. The self-stressing composite patch of claim 1 , wherein the terminal embedment length is about 100 mm.
10. The self-stressing composite patch of claim 1 , wherein the wires have a length of about 300 mm.
11. The self-stressing composite patch of claim 1 , comprising about 10 to about 35 wires.
12. The self-stressing composite patch of claim 1 , further comprising an adhesive for affixing the tabs to the structural element.
13. The self-stressing composite patch of claim 12 , wherein the adhesive is an epoxy, vinyl ester, polyester, phenolic, or acrylic adhesive.