Twin fin fairing

Abstract

A fairing for the reduction of vortex-induced vibration and the minimization of drag about a substantially cylindrical element immersed in a fluid medium. The fairing also eliminates the galloping phenomenon typically associated with a teardrop-shaped fairing. The fairing having a U-shaped cylindrical shell with opposing edges defining a longitudinal gap and parallel fins extending outwardly from the opposing edges of the shell, the parallel fins being positioned so as to reduce vortex-induced vibration, minimize drag and to eliminate the galloping phenomenon on the cylindrical element.

What is claimed is: 
     
       1. A fairing for the reduction of vortex-induced vibration, the minimization of drag and the elimination of the galloping phenomenon about a substantially cylindrical element immersed in a fluid medium, comprising:
 a one-piece fairing having a U-shaped cylindrical shell portion at comprising a leading edge of the faring with, opposing edges extending toward, and a trailing edge of the fairing, the opposing edges extending from the leading edge toward the trailing edge of the shell portion, the opposing edges further defining a longitudinal gap therebetween that extends from the leading edge to the trailing edge of the shell portion, wherein the longitudinal gap provides an opening that allows for placement of the substantially cylindrical element through the longitudinal gap and into the shell portion of the fairing; and 
 parallellongitudinal fins extending outwardly from the opposing edges of the shell portion in which the parallellongitudinal fins taper inward toward the trailing edge of the fairing, wherein the parallellongitudinal fins are positioned so as to reduce vortex-induced vibration and minimize drag on the cylindrical element. 
 
     
     
       2. The fairing of  claim 1 , further including a bearing pad connector configured to fit in the gap in the shell portion between the shell's shell portion's opposing edges and the parallel longitudinal fins. 
     
     
       3. The fairing of  claim 2 , wherein the bearing pad has a curved inside surface and side surfaces in parallel alignment with each of the fins. 
     
     
       4. The fairing of  claim 2 , wherein each fairing includes at least one bearing pad connector for securing the fairing to a cylindrical element, wherein each connector has a curved inside surface and side surfaces in alignment with each of the fins. 
     
     
       5. The fairing of  claim 4 , wherein each fairing includes a plurality of bearing pads connectors for securing the fairing to a cylindrical element. 
     
     
       6. The fairing of  claim 1 , further including at least a set of opposed connectors for securing the fairing to a cylindrical element, each connector being positioned on an inside surface of each parallel longitudinal fin. 
     
     
       7. The fairing of  claim 6 , wherein the fins include a plurality of opposed connectors. 
     
     
       8. The fairing of  claim 6 , wherein each connector includes an opening configured to receive a fastening means for securing the opposing connectors together. 
     
     
       9. The fairing of  claim 6 , further including a flange at a top and bottom edge of the fairing, the flange extending around the circumference of the shell and outwardly from the shell. 
     
     
       10. The fairing of  claim 9 , wherein the flange includes at least one V-shaped cutouts. 
     
     
       11. The fairing of  claim 1 , wherein each fin does not extend beyond the outer diameter of the shell. 
     
     
       12. The fairing of  claim 1 , wherein the fairing is constructed from a non-metallic, low corrosive material selected from a group consisting of polyethylene, polyurethane, vinyl ester resin, poly vinyl chloride and fiberglass. 
     
     
       13. The fairing of  claim 1 , wherein the shell portion has an outer diameter D and the longitudinal fins have a distance W located between opposing edges ends of the longitudinal fins at the trailing edge of the fairing. 
     
     
       14. The fairing of  claim 13 , wherein the a ratio of W to D is from W=D W<100% of D to W =75% of D. 
     
     
       15. A fairing system for the reduction of vortex-induced vibration, the minimization of drag and the elimination of the galloping phenomenon about a substantially cylindrical element immersed in a fluid medium, the fairing system comprising:
 a plurality of one-piece fairings having U-shaped cylindrical shell portions at, each shell portion comprising a leading edge of each shell portion, each shell portion having, opposing edges extending toward, and a trailing edge of the fairing, the opposing edges extending from the leading edge toward the trailing edge of the shell portion, the opposing edges further defining a longitudinal gap therebetween that extends from the leading edge to the trailing edge of the shell portion, wherein the longitudinal gap provides an opening that allows for placement of the substantially cylindrical element through the longitudinal gap and into the shell portion; 
 parallellongitudinal fins extending outwardly from the opposing edges of each of the plurality of shell portions in which the parallellongitudinal fins taper inward toward the trailing edge of the fairing, wherein the parallellongitudinal fins are positioned so as to reduce vortex-induced vibration and minimize drag on the cylindrical element; and 
 means for securing each of the plurality of fairings around the cylindrical element. 
 
     
     
       16. The fairing system of  claim 15 , wherein the means for securing the fairings around the cylindrical element includes a bearing pad connector configured to fit in the gap in each shell portion between the shell's shell portion's opposing edges and the parallel longitudinal fins. 
     
     
       17. The fairing system of  claim 16 , wherein the bearing pad has a curved inside surface and side surfaces in parallel alignment with each of the fins. 
     
     
       18. The fairing system of  claim 16 , wherein each fairing includes at least one bearing pad connector for securing the fairing to a cylindrical element, wherein each connector has a curved inside surface and side surfaces in alignment with each of the fins. 
     
     
       19. The fairing of  claim 15 , wherein the means for securing include at least a set of opposed connectors, each connector being positioned on an inside surface of each parallel longitudinal fin. 
     
     
       20. The fairing of  claim 19 , wherein the fins include a plurality of opposed connectors. 
     
     
       21. The fairing of  claim 19 , wherein each connector includes an opening configured to receive a fastening means for securing the opposing connectors together. 
     
     
       22. The fairing of  claim 15 , further including a flange at a top and bottom edge of the fairing, the flange extending around the circumference of the shell and outwardly from the shell. 
     
     
       23. The fairing of  claim 22 , wherein the flange includes at least one V-shaped cutout. 
     
     
       24. The fairing system of  claim 22 , wherein the flanges on each fairing are configured such that they allows each fairing to freely rotate on an adjoining fairing. 
     
     
       25. The fairing system of  claim 15 , wherein a circular collar is positioned between each of the plurality of fairings, the collar configured such that it allows each fairing to freely rotate on the collar. 
     
     
       26. The fairing system of  claim 25 , wherein the collar is in two sections held together by securing means for securing the collar around the cylindrical element. 
     
     
       27. The fairing system of  claim 25 , wherein the collar includes a plurality of compliant annulus spacers extending outwardly from an inside surface of the collar, the spacers being configured to induce frictional interaction between the collar and the cylindrical element. 
     
     
       28. The fairing system of  claim 15 , wherein each fin does not extend beyond the outer diameter of the shell. 
     
     
       29. The fairing system of  claim 15 , wherein the fairing is constructed from a non-metallic, low corrosive material selected from a group consisting of polyethylene, polyurethane, vinyl ester resin, poly vinyl chloride and fiberglass. 
     
     
       30. The fairing system of  claim 15 , wherein the shell portion has an outer diameter D and the parallel longitudinal fins have a distance W located between opposing edges ends of the fins at the trailing edge of the fairing. 
     
     
       31. The fairing of  claim 30 , wherein the a ratio of W to D is from W=D W<100% of D to W=75% of D. 
     
     
       32. The fairing of  claim 13 , wherein the ration ratio of W to D is from W=D W<100% of D to W=50% of D. 
     
     
       33. The fairing system of  claim 30 , wherein the ration ratio of W to D is from W=D W<100% of D to W=50% of D. 
     
     
       34. A fairing for the reduction of vortex-induced vibration, the minimization of drag and the elimination of the galloping phenomenon about a substantially cylindrical element immersed in a fluid medium, comprising:
 a one-piece fairing having a U-shaped cylindrical shell portion at comprising a leading edge of the faring with, opposing edges extending toward, and a trailing edge of the fairing, the opposing edges extending from the leading edge toward the trailing edge of the shell portion, the opposing edges further defining a longitudinal gap therebetween that extends from the leading edge to the trailing edge of the shell portion, wherein the longitudinal gap provides an opening that allows for placement of the substantially cylindrical element through the longitudinal gap and into the shell portion of the fairing; 
 parallellongitudinal fins extending outwardly from the opposing edges of the shell portion in which the parallellongitudinal fins taper inward toward the trailing edge of the fairing, wherein the parallellongitudinal fins are positioned so as to reduce vortex-induced vibration and minimize drag on the cylindrical element; 
 a flange at a top and bottom edge of the fairing, the flange extending around the circumference of the shell portion and outwardly from the shell portion; and 
 at least a set of opposed connectors for securing the fairing to the cylindrical element, each connector being positioned on an inside surface of each parallel longitudinal fin.