Heat exchanger assembly formed of a lattice structure with a plurality of shell structure unit cells
An additively manufactured heat exchanger assembly formed of a lattice structure with a plurality of shell structure unit cells. The plurality of shell structure unit cells each include at least one junction and a plurality of connectors coupled to the junction. The junction and the plurality of connectors form an integral surface. The heat exchanger assembly further includes a fluid boundary wall defined within the lattice structure to define an active heat exchanger portion. The active heat exchanger portion includes at least one working fluid contained within the fluid boundary wall. Further, at least one of the plurality of shell structure unit cells extends through and beyond the fluid boundary wall. Further, the shell structure unit cells may be isotropic.
1. A heat exchanger assembly, comprising:
a lattice structure comprising a plurality of shell structure unit cells, each of the plurality of shell structure unit cells comprising at least one junction and a plurality of connectors coupled to the at least one junction, the at least one junction and the plurality of connectors forming an integral surface; and
a fluid boundary wall defined within the lattice structure to define an active heat exchanger portion of the heat exchanger assembly and an inactive heat exchanger portion of the heat exchanger assembly, the active heat exchanger portion comprising at least one working fluid contained within the fluid boundary wall, the inactive heat exchanger portion lacking working fluids including the at least one working fluid,
wherein at least one of the plurality of shell structure unit cells extends through and beyond the fluid boundary wall to define a first region that is part of the active heat exchanger portion and a second region that is part of the inactive heat exchanger portion.
2. The heat exchanger assembly of claim 1 , wherein the lattice structure is an additively manufactured lattice structure.
3. The heat exchanger assembly of claim 2 , wherein the additively manufactured lattice structure is formed via at least one of a DMLS (Direct Metal Laser Sintering) process, a DMLM (Direct Metal Laser Melting) process, a SLM (Selective Laser Melting) process, a Binder Jetting process, or a Hybrid Systems process.
4. The heat exchanger assembly of claim 1 , wherein the plurality of shell structure unit cells are configured as a plurality of isotropic shell structure unit cells.
5. The heat exchanger assembly of claim 1 , wherein the fluid boundary wall is a pressurized fluid boundary wall.
6. The heat exchanger assembly of claim 1 , wherein the plurality of connectors of each of the plurality of shell structure unit cells are configured as an ordered triplet of connectors, and wherein the ordered triplet of connectors are pair-wise perpendicular.
7. The heat exchanger assembly of claim 1 , wherein the lattice structure and the fluid boundary wall define a first fluid domain and a second fluid domain of the active heat exchanger portion of the heat exchanger assembly, the first fluid domain running adjacent to the second fluid domain within the lattice structure, the first fluid domain containing a first working fluid and the second fluid domain containing a second working fluid.
8. The heat exchanger assembly of claim 1 , wherein a gas turbine engine comprises the heat exchanger assembly.
9. A method of manufacturing a heat exchanger assembly for a rotary machine, the method comprising:
forming a lattice structure having a plurality of shell structure unit cells with at least one junction and a plurality of connectors coupled to the at least one junction, the at least one junction and the plurality of connectors forming an integral surface; and
forming a fluid boundary wall within the lattice structure to define an active heat exchanger portion of the heat exchanger assembly and an inactive heat exchanger portion of the heat exchanger assembly, wherein at least one of the plurality of shell structure unit cells extends through and beyond the fluid boundary wall; and
providing at least one working fluid within the fluid boundary wall.
10. The method of claim 9 , wherein forming the lattice structure comprises additively manufacturing the lattice structure, and wherein additively manufacturing the lattice structure comprises at least one of a DMLS (Direct Metal Laser Sintering) process, a DMLM (Direct Metal Laser Melting) process, a SLM (Selective Laser Melting) process, a Binder Jetting process, or a Hybrid Systems process.
11. The method of claim 9 , wherein the fluid boundary wall is a pressurized fluid boundary wall.
12. The method of claim 9 , further comprising heat treating the lattice structure and the fluid boundary wall defined within the lattice structure.
13. The method of claim 9 , further comprising removing portions of shell structure unit cells from outside the active heat exchanger portion.
14. The method of claim 13 , wherein portions of at least one of the plurality of shell structure unit cells extends through and beyond the fluid boundary wall after the removing the portions of shell structure unit cells from outside the active heat exchanger portion.
15. An additively manufactured lattice structure, comprising:
a plurality of shell structure unit cells, each of the plurality of shell structure unit cells comprising at least one junction and a plurality of connectors coupled to the at least one junction, the at least one junction and the plurality of connectors forming an integral surface; and
a boundary wall defined within the lattice structure;
wherein at least one of the plurality of shell structure unit cells extends through and beyond the boundary wall to define a first region configured to house a working fluid and a second region fluidly separated from the first region and configured to lack the working fluid.
16. The additively manufactured lattice structure of claim 15 , wherein the additively manufactured lattice structure is formed via at least one of a DMLS (Direct Metal Laser Sintering) process, a DMLM (Direct Metal Laser Melting) process, a SLM (Selective Laser Melting) process, a Binder Jetting process, or a Hybrid Systems process.
17. The additively manufactured lattice structure of claim 15 , wherein the plurality of shell structure unit cells are a plurality of isotropic shell structure unit cells.
18. The additively manufactured lattice structure of claim 15 , wherein the boundary wall is a pressurized boundary wall.
19. The additively manufactured lattice structure of claim 15 , wherein the plurality of connectors of each of the plurality of shell structure unit cells are configured as an ordered triplet of connectors, and wherein the ordered triplet of connectors are pair-wise perpendicular.
20. The additively manufactured lattice structure of claim 15 , wherein the additively manufactured lattice structure is part of a gas turbine engine.