Radiation shield for a gaseous fuel circuit
A radiation shield assembly for blocking radiation at a gas turbine piping connection joint is provided. The radiation shield assembly includes a radiation shield configured to surround the gas turbine piping connection joint. The radiation shield includes at least two shield portions coupled to one another at a pair of flanged joints. Each shield portion of the at least two shield portions include an inner shell, an outer shell, and insulation disposed between the inner shell and the outer shell.
1. A radiation shield assembly for blocking radiation at a gas turbine piping connection joint, the radiation shield assembly comprising:
a radiation shield configured to surround the gas turbine piping connection joint, the radiation shield comprising at least two shield portions coupled to one another at a first flanged end and a second flanged end opposite the first flanged end, wherein each shield portion of the at least two shield portions comprises:
an inner shell comprising an inner arcuate portion extending between the first flanged end and the second flanged end, a first inner connection flange extending radially outward from the inner arcuate portion at the first flanged end, and a second inner connection flange extending radially outward from the inner arcuate portion at the second flanged end;
an outer shell including an outer arcuate portion, a first outer connection flange extending radially outwardly from the outer arcuate portion at the first flanged end, and a second outer connection flange extending radially outwardly from the outer arcuate portion at the second flanged end; and
insulation disposed between the inner shell and the outer shell, the insulation extending between a first terminal end adjacent the first flanged end and a second terminal end adjacent the second flanged end, wherein the first inner connection flange extends radially outward across the first terminal end and further extends radially outward of the outer arcuate portion parallel to the first outer connection flange such that the first inner connection flange and the first outer connection flange stack together in flush contact, and wherein the second inner connection flange extends radially outward across the second terminal end and further extends radially outward of the outer arcuate portion parallel to the second outer connection flange such that the second inner connection flange and the second outer connection flange stack together in flush contact.
2. The radiation shield assembly as in claim 1 , wherein the insulation is disposed wholly within the radiation shield between the inner shell and the outer shell; and wherein the radiation shield is sized to provide a clearance between the respective inner shells of the at least two shield portions and the gas turbine piping connection joint.
3. The radiation shield assembly as in claim 1 , further comprising a support assembly including a support plate and at least one support member coupled to the radiation shield; wherein the at least one support member extends between the support plate and one of the first flanged end and the second flanged end of the radiation shield.
4. The radiation shield assembly as in claim 1 , wherein the first inner connection flange and the second inner connection flange each comprise a pair of tabs disposed on opposite sides of the insulation and in contact with the insulation.
5. The radiation shield assembly as in claim 1 , wherein the outer arcuate portion extends between the first outer connection flange and the second outer connection flange.
6. The radiation shield assembly as in claim 5 , wherein the first outer connection flange is mechanically coupled to the first inner connection flange, and wherein the second outer connection flange is mechanically coupled to the second inner connection flange.
7. The radiation shield assembly as in claim 5 , wherein the radiation shield includes one or more support brackets coupled to the outer arcuate portion.
8. A gaseous fuel supply system for a gas turbine engine, the gaseous fuel supply system comprising:
a gaseous fuel supply;
an accessory system fluidly coupled to a plurality of combustion cans in a combustion section of the gas turbine engine;
an enclosure;
a gas fuel circuit disposed at least partially within the enclosure, the gas fuel circuit fluidly coupled to the gaseous fuel supply and fluidly coupled to the accessory system, wherein the gas fuel circuit includes a piping connection joint within the enclosure; and
a radiation shield surrounding the piping connection joint, the radiation shield comprising at least two shield portions coupled to one another at a first flanged end and a second flanged end opposite the first flanged end, wherein each shield portion of the at least two shield portions comprises:
an inner shell comprising an inner arcuate portion extending between the first flanged end and the second flanged end, a first inner connection flange extending radially outward from the inner arcuate portion at the first flanged end, and a second inner connection flange extending radially outward from the inner arcuate portion at the second flanged end;
an outer shell including an outer arcuate portion, a first outer connection flange extending radially outwardly from the outer arcuate portion at the first flanged end, and a second outer connection flange extending radially outwardly from the outer arcuate portion at the second flanged end; and
insulation disposed between the inner shell and the outer shell, the insulation extending between a first terminal end adjacent the first flanged end and a second terminal end adjacent the second flanged end, wherein the first inner connection flange extends radially outward across the first terminal end and further extends radially outward of the outer arcuate portion parallel to the first outer connection flange such that the first inner connection flange and the first outer connection flange stack together in flush contact, and wherein the second inner connection flange extends radially outward across the second terminal end and further extends radially outward of the outer arcuate portion parallel to the second outer connection flange such that the second inner connection flange and the second outer connection flange stack together in flush contact.
9. The gaseous fuel supply system as in claim 8 , wherein the gas fuel circuit further comprises a manifold, a branch line extending from the manifold to the piping connection joint, a pump line extending from the piping connection joint, and an outlet line extending from the pump line to the accessory system.
10. The gaseous fuel supply system as in claim 8 , wherein electrical devices, electrical wires, a ventilation system, and a gas detection system are disposed within the enclosure.
11. The gaseous fuel supply system as in claim 8 , wherein the insulation is disposed wholly within the radiation shield between the inner shell and the outer shell; and wherein the radiation shield is sized to provide a clearance between the respective inner shells of the at least two shield portions and the piping connection joint.
12. The gaseous fuel supply system as in claim 8 , further comprising a support assembly including a support plate and at least one support member coupled to the radiation shield; and wherein the at least one support member extends between the support plate and one of the first flanged end and the second flanged end of the radiation shield.
13. The gaseous fuel supply system as in claim 8 , wherein the first inner connection flange and the second inner connection flange each comprise a pair of tabs disposed on opposite sides of the insulation and in contact with the insulation.