Systems and methods utilizing gas temperature as a power source
US-12163485-B2 · Dec 10, 2024 · US
US10001079B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10001079-B2 |
| Application number | US-201514874941-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 5, 2015 |
| Priority date | Feb 10, 2003 |
| Publication date | Jun 19, 2018 |
| Grant date | Jun 19, 2018 |
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An improvement is provided to a pressurized close-cycle machine that has a cold-end pressure vessel and is of the type having a piston undergoing reciprocating linear motion within a cylinder containing a working fluid heated by conduction through a heater head by heat from an external thermal source. The improvement includes a heat exchanger for cooling the working fluid, where the heat exchanger is disposed within the cold-end pressure vessel. The heater head may be directly coupled to the cold-end pressure vessel by welding or other methods. A coolant tube is used to convey coolant through the heat exchanger.
Opening claim text (preview).
What is claimed is: 1. A heat exchanger for cooling a working fluid in an external combustion engine, the external combustion engine including a pressure vessel with a working space and a charge section, the heat exchanger comprising: a cooler body located inside the pressure vessel, the cooler body separating the working space from the charge section, the working space filled with a working fluid and the cooler body defining a cooler working space portion in the working space, and a continuous length of metal coolant tubing, the coolant tubing conveying a coolant through the heat exchanger and across a wall of the pressure vessel wherein a first section of the coolant tubing is located in the cooler working space, the cooler body directing a flow of the working fluid across the first section of the coolant tubing. 2. A heat exchanger according to claim 1 , further comprising a heat sink cast over the section of the metal coolant tubing. 3. A heat exchanger according to claim 2 , wherein the heat sink comprising a working fluid contact surface comprising a plurality of extended heat transfer surfaces. 4. A heat exchanger according to claim 1 , further comprising a flow constricting counter surface for confining the flow of the working fluid to a specified proximity of the section of coolant tubing. 5. A heat exchanger according to claim 1 , wherein a second section of the coolant tubing passes through the charge section. 6. A heat exchanger according to claim 5 , further comprising extended surfaces on the second section of the coolant tubing. 7. In a closed-cycle thermal engine, of the type contained within a pressure vessel with a working space and a charge section and having a piston undergoing reciprocating linear motion within a cylinder and a working fluid heated by conduction through a heater head, the working fluid being cooled by a heat exchanger, the heat exchanger comprising: a cooler body located in the pressure vessel and separating the working space from the charge section, the working space filled with the working fluid and the cooler body defining a cooler working space portion in the working space; and a continuous length of metal coolant tubing, the coolant tubing conveying a coolant through the heat exchanger and across a wall of the pressure vessel wherein a first section of the coolant tubing is located in the cooler working space, the cooler body directing a flow of the working fluid across the first section of the coolant tubing. 8. A closed-cycle thermal engine according to claim 7 , wherein the heater head is directly coupled to the pressure vessel. 9. A closed-cycle thermal engine according to claim 7 , wherein the heater head further comprising a flange for transferring a mechanical load from the heater head to the pressure vessel. 10. A closed-cycle thermal engine according to claim 7 , wherein the first section of the coolant tubing contained within the heat exchanger comprises a single continuous section of tubing. 11. A closed-cycle thermal engine according to claim 7 , wherein the coolant tubing comprises a single continuous piece of tubing. 12. A closed-cycle thermal engine according to claim 7 , wherein an outside diameter of the coolant tubing passes through the pressure vessel and is sealed to the pressure vessel. 13. A closed-cycle thermal engine according to claim 7 , wherein the first section of the coolant tubing comprising a plurality of extended heat transfer surfaces. 14. A closed-cycle thermal engine according to claim 7 , further comprising at least one spacing element to direct a flow of the working fluid to a specified proximity of the first section of coolant tubing. 15. A closed-cycle thermal engine according to claim 7 , wherein the heat exchanger further comprising an annular heat sink surrounding the first section of the coolant tubing wherein a flow of the working fluid in the cooler working space is directed along at least one surface of the annular heat sink. 16. A closed-cycle thermal engine according to claim 7 , wherein the first section of the coolant tubing is wrapped around an interior wall of the heat exchanger. 17. A closed-cycle thermal engine according to claim 7 , wherein the charge section comprising a charge fluid, the pressurized closed-cycle thermal engine further comprising a second section of the coolant tubing disposed within the pressure vessel in a manner adapted for cooling the charge fluid. 18. A closed-cycle thermal engine according to claim 17 , further comprising a fan for circulating the charge fluid. 19. A heat exchanger according to claim 17 , further comprising extended surfaces on the second section of the coolant tubing. 20. A heat exchanger according to claim 17 , wherein the second section of the coolant tubing is a single piece of tubing.
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