High efficiency solar receiver
View Patent ↗A solar receiver includes a multi-sided central assembly with wing assemblies extending from corners thereof. The central assembly includes one-sided heat absorption panels, while the wing assemblies use two-sided heat absorption panels. Stiffener structures run across the exposed faces of the various heat absorption panels.
1. A solar receiver, comprising:
a central receiver assembly comprising an internal support structure and at least one external central tube panel, the internal support structure defining an interior volume, the at least one external central tube panel comprising a plurality of vertical tubes for conveying a heat transfer fluid, wherein the tubes are interconnected by at least one upper header and at least one lower header, and being arranged on an exterior face of the internal support structure with the at least one external central tube panel having an exposed first face and a non-exposed second face;
at least one wing assembly extending from the central receiver assembly, each wing assembly having a wing tube panel that comprises a plurality of vertical tubes for conveying a heat transfer fluid, wherein the tubes are interconnected by at least one upper header and at least one lower header, and each wing tube panel having a first exposed face and a second exposed face opposite the first face; and
at least one stiffener structure running from a first side edge to a second side edge across the first exposed face and the second exposed face of the wing tube panel at a first support elevation, the at least one stiffener structure formed from a first support assembly on the first face of the wing tube panel and a second support assembly on the second face of the wing tube panel, wherein each support assembly includes a support tube, a horizontal flange extending from the support tube and having a slot therein, and a scallop bar engaging the tube panel and having at least one lug, the scallop bar engaging the horizontal flange by a pin passing through the at least one lug and the slot of the horizontal flange.
2. The solar receiver of claim 1 , wherein the wing assembly further comprises a structural support frame, the structural support frame including:
a first vertical column;
an upper horizontal beam extending from an upper end of the first vertical column to an upper connection on the internal support structure; and
a lower horizontal beam extending from a lower end of the first vertical column to a lower connection on the internal support structure.
3. The solar receiver of claim 1 , wherein the support tube of each support assembly has a larger diameter than any tube in the wing tube panel.
4. The solar receiver of claim 1 , wherein the first support assembly of the first stiffener structure is fluidly connected to an inlet header of the wing tube panel or is fluidly connected to the at least one external central tube panel.
5. The solar receiver of claim 1 , further comprising a second stiffener structure running from the first side edge to the second side edge across the first face and the second face of the wing tube panel at a second support elevation.
6. The solar receiver of claim 5 , wherein the first support elevation and the second support elevation are not located at a middle section of the wing tube panel.
7. The solar receiver of claim 1 , wherein the first face and the second face of the wing tube panel are painted to increase heat absorption.
8. The solar receiver of claim 1 , wherein the at least one external central tube panel comprises wall tubes having helical internal ribs.
9. The solar receiver of claim 1 , wherein the internal support structure has a rectangular cross-section, the central receiver assembly has four external central tube panels, and a total of four wing assemblies extend from corners of the central receiver assembly.
10. A solar energy system, comprising:
a solar receiver according to claim 1 ; and
a field of heliostats configured to direct sunlight towards the first face of the central tube panel, the first face of the wing tube panel, and the second face of the wing tube panel.
11. The solar receiver of claim 1 , wherein the first support assembly of the first stiffener structure is fluidly connected to an inlet header of the wing tube panel or is fluidly connected to the at least one external central tube panel.
12. The solar receiver of claim 1 , wherein the first support assembly conveys a second heat transfer fluid that is different from the heat transfer fluid conveyed by the wing tube panel.
13. A solar receiver, comprising:
a central receiver assembly comprising an internal support structure and at least one external central tube panel, the internal support structure defining an interior volume, the at least one external central tube panel comprising a plurality of vertical tubes for conveying a heat transfer fluid, wherein the tubes are interconnected by at least one upper header and at least one lower header, and being arranged on an exterior face of the internal support structure with the at least one external central tube panel having an exposed first face and a non-exposed second face;
the central receiver assembly further comprising an upper heat shield located above the at least one external central tube panel, a lower heat shield located below the at least one external central tube panel, and a horizontal heat shield located above the at least one external central tube panel; and
at least one wing assembly extending from the central receiver assembly, each wing assembly having a wing tube panel that comprises a plurality of vertical tubes for conveying a heat transfer fluid, wherein the tubes are interconnected by at least one upper header and at least one lower header, and each wing tube panel having an first exposed face and an second exposed face opposite the first face and a heat shield having an upper face located above the wing tube panel, a lower face located below the wing tube panel, and a side face located distal from the central receiver assembly.
14. The solar receiver of claim 13 , wherein an open space is present between the side face of the wing assembly heat shield and a side edge of the wing tube panel.
15. The solar receiver of claim 13 , wherein the support tube of each support assembly has a larger diameter than any tube in the wing tube panel.
16. The solar receiver of claim 13 , wherein the first support assembly of the first stiffener structure is fluidly connected to an inlet header of the wing tube panel or is fluidly connected to the at least one external central tube panel.
17. The solar receiver of claim 13 , further comprising a second stiffener structure running from the first side edge to the second side edge across the first face and the second face of the wing tube panel at a second support elevation.
18. The solar receiver of claim 17 , wherein the first support assembly of the second stiffener structure is fluidly connected to an outlet header of the wing tube panel or is fluidly connected to the at least one external central tube panel.