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 method for repair of a crack in a structural element using a self-stressing composite patch, comprising:
preparing a self-stressing patch comprising one or more prestrained shape memory alloy (SMA) wires, wherein the wires have terminal ends;
embedding the terminal ends of the wires into tabs comprising fiber reinforced polymer (FRP), 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;
affixing the tabs on opposite sides of the crack, whereby the central portion of the wires is substantially adjacent to the crack; and
heating the central portion of the wires to activate the prestrained shape memory alloy (SMA), whereby a prestressing force is applied to the tabs as they are affixed on opposite sides of the crack.
2. The method of claim 1 , further comprising the step of affixing a fiber reinforced polymer (FRP) overlay patch over the tabs and the wires, wherein the overlay patch is sized to completely overlay the tabs and the wires.
3. The method 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 method 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 method of claim 1 , wherein the shape memory alloy (SMA) is ternary nickel titanium alloy (NiTiNb).
6. The method of claim 1 , wherein the fiber reinforced polymer (FRP) of the tabs comprises carbon fibers embedded in an epoxy-based saturating resin.
7. The method 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), or basalt fiber reinforced polymer (BFRP).
8. The method of claim 1 , wherein the tabs have a length of about 180 mm.
9. The method of claim 1 , wherein the terminal embedment length is about 100 mm.
10. The method of claim 1 , wherein the wires have a length of about 300 mm.
11. The method of claim 1 , wherein the self-stressing patch comprises about 10 to about 35 wires.
12. The method of claim 1 , wherein the step of affixing the tabs comprises using an adhesive to affix the tabs to the structural element.
13. The method of claim 12 , wherein the adhesive is an epoxy, vinyl ester, polyester, phenolic, or acrylic adhesive.
14. The method of claim 1 , wherein the central portion of the wires is heated to a temperature of about 165° C.