APPARATUS AND METHOD FOR CONVERTING THERMAL ENERGY
20230374917 · 2023-11-23
Assignee
Inventors
Cpc classification
F01K7/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01K7/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01K25/103
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F01K7/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01K7/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01K7/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
An apparatus for converting thermal energy into mechanical energy by a cycle, having a heat exchanger, a reservoir for an operating medium, a feed line, a turbine, and a return line having at least one recovery device is described. In order to also be able to utilize waste heat for the generation of electrical energy, the turbine is embodied as a disc rotor turbine. A method for converting thermal energy into mechanical energy in a cycle is also described, in which thermal energy is supplied to an operating medium in a reservoir, the operating medium evaporates and/or a pressure in the operating medium is increased, whereupon the operating medium releases energy in a turbine, after which the operating medium is returned to the reservoir.
Claims
1. An apparatus for converting thermal energy into mechanical energy by a cycle, having a heat exchanger, a reservoir for an operating medium, a feed line, a turbine, and a return line having at least one recovery device, wherein the turbine is embodied as a disc rotor turbine with full condensation of the operating medium, whereby a separate condenser can be eliminated.
2. The apparatus according to claim 1, wherein the turbine embodied as a disc rotor turbine comprises multiple discs rotatably arranged next to one another on an axle in a casing, wherein the surfaces of the discs are provided with microstructures.
3. The apparatus according to claim 1, wherein the turbine embodied as a disc rotor turbine comprises multiple discs rotatably arranged next to one another on an axle in a casing and, in the casing, comprises an inlet nozzle holder having a geometry that enables an injection of the operating medium between the discs.
4. The apparatus according to claim 1, wherein the turbine embodied as a disc rotor turbine comprises multiple discs rotatably arranged next to one another on an axle in a casing and, in the casing, comprises an inlet nozzle holder having a geometry that enables a generation of a rotating stream of the operating medium.
5. The apparatus according to claim 1, wherein a structure-borne noise measurement is integrated into the turbine for identifying laminar and turbulent flow.
6. The apparatus according to claim 1, wherein a valve is provided for regulating a flow rate.
7. The apparatus according to claim 1, wherein the reservoir for the operating medium can be connected to a heat source via a heat exchanger.
8. The apparatus according to claim 1, wherein CO.sub.2 is used as an operating medium.
9. The apparatus according to claim 1, wherein the apparatus is designed for a pressure of the operating medium at the turbine of more than 74 bar, preferably more than 100 bar, in particular to enable a supercritical state of the operating medium in the turbine.
10. The apparatus according to claim 1, wherein at least one valve is provided between the turbine and the reservoir, and the recovery device is embodied to generate a chronologically alternating force on the operating medium, in order to generate a pressure vibration in the operating medium.
11. The apparatus according to claim 1, characterized in that wherein the recovery device is embodied as a resonant tube.
12. The apparatus according to claim 1, wherein the recovery device comprises a spring-loaded, undamped mass, for example a piston or a membrane.
13. The apparatus according to claim 1, wherein the recovery device comprises a spring-loaded, damped mass, for example a piston or a membrane.
14. The apparatus according to claim 1, wherein the recovery device comprises field coils which generate a magnetic field.
15. The apparatus according to claim 14, wherein the field coils are arranged in an interior of a closed volume.
16. The apparatus according to claim 14, wherein the field coils are arranged outside of a closed volume.
17. The apparatus according to claim 1, wherein at least one valve is arranged between a turbine outlet and the reservoir, which valve enables a flow of the operating medium from the turbine outlet to the reservoir and prevents a flow in the opposite direction.
18. The apparatus according to claim 17, wherein the at least one valve is embodied as a valve without moving parts, in particular as a Tesla valve.
19. A method for converting thermal energy into mechanical energy in a cycle, in particular using an apparatus according to claim 1, wherein thermal energy is supplied to an operating medium in a reservoir, wherein the operating medium evaporates and/or a pressure in the operating medium is increased, whereupon the operating medium releases energy in a turbine after which the operating medium is returned to the reservoir, and wherein a full condensation of the operating medium occurs in the turbine, whereby a separate condenser can be eliminated.
20. The method according to claim 19, wherein CO.sub.2 is used as an operating medium.
21. The method according to claim 19, wherein the operating medium absorbs the thermal energy at a pressure of up to 73 bar and thereby evaporates.
22. The method according to claim 19, wherein the operating medium reaches a supercritical state, in particular at a pressure of more than 74 bar, preferably at a pressure of more than 100 bar, and a condensation from the supercritical state to a gaseous state and a liquid state takes place in the turbine.
23. The method according to claim 19, wherein pressure and temperature are measured in a return line and compared with a pressure and a temperature in a feed line, wherein a flow rate of the operating medium in the return line is regulated by a valve, arranged in the return line.
24. The method according to claim 19, wherein a return of the operating medium from the turbine to the reservoir takes place with a pressure increase in the operating medium by a recovery device with which a chronologically alternating force is applied to the operating medium.
25. The method according to claim 19, wherein the operating medium is set in oscillation, in particular in resonance, by the recovery device.
26. The method according to claim 25, wherein the oscillation of the operating medium is generated by a resonant tube.
27. The method according to claim 25, wherein the oscillation of the operating medium is generated by a spring-loaded mass.
28. The method according to claim 27, wherein mass is damped.
29. The method according to claim 25, wherein the operating medium comprises a magnetic fluid or is formed by a magnetic fluid and the oscillation is generated by an alternating magnetic field.
Description
[0052] Additional features, advantages, and effects of the invention follow from the exemplary embodiments described below. In the drawings which are thereby referenced:
[0053]
[0054]
[0055]
[0056]
[0057]
[0058]
[0059]
[0060] The apparatus 1 is essentially composed of a turbine 2, a reservoir 3 for the operating medium, a heat exchanger 4, a feed line 5 between the reservoir 3 and turbine 2 in order to convey an operating medium from the reservoir 3 to the turbine 2, a return line 6 after the turbine 2 in order to convey the operating medium from a turbine outlet back to the reservoir 3, a valve 7 for regulating a flow.
[0061] Furthermore, a pressure sensor 8 is provided with which the valve 7 can be controlled.
[0062] In order to convey the operating medium from the turbine outlet to the reservoir 3, wherein a higher pressure prevails in the reservoir 3 than at the turbine outlet, a recovery device 9 is provided in the return line 6.
[0063] CO.sub.2 is preferably used as an operating medium, since it has a low boiling point. The critical point is at 31° C. and 73.9 bar. For CO.sub.2, a phase transition between liquid and gaseous already occurs at a pressure of approximately 72 bar at a temperature of only 30° C., whereby a phase transition can be utilized for energy absorption and release even with a heat supplied at low temperatures. Thus, the operating medium in the reservoir can be present, for example, at a pressure of 72 bar, wherein waste heat is supplied thereto at a temperature of 40° C. by means of the heat exchange, wherein the operating medium evaporates, whereupon it is depressurized to a pressure of approximately 64 bar in the turbine, thereby cooling to an ambient temperature of 20° C., for example, and fully condensing, wherein work is outputted via the turbine.
[0064] Alternatively, it can also be provided that the operating medium is present in the reservoir (3) at a pressure of more than 74 bar, for example at approximately 100 bar, and reaches a supercritical state through a supply of heat, from which state it fully condenses to a gaseous state and, simultaneously or subsequently, to a liquid state in the turbine (2).
[0065] With corresponding pressure conditions in the apparatus (1), it can also be provided that an at least partial phase transition of the operating medium to a solid state takes place in the turbine at a temperature of 20° C., for example, so that dry ice particles form which are also unproblematic for the turbine (2) due to the use of a disc rotor turbine. As a result, heat accumulating at a low temperature of only 40° C., for example, can also be utilized to generate electricity.
[0066] Of course, other operating media such as refrigerants can also be used, for example 8744 or R134a.
[0067] The heat from a heat source 10 is supplied to the operating medium via a heat exchanger 4 arranged in the reservoir 3. Either primary energy or preferably waste heat, for example from an industrial process, with a temperature of approximately 40° C. can thereby be used. Heat sources with a lower temperature can also be used, however. It is thus especially beneficial that solar energy can also be utilized.
[0068] A disc rotor turbine is used as a turbine 2. This is also known as a boundary-layer turbine 2 or Tesla turbine 2. This disc rotor turbine comprises multiple discs rotatably arranged next to one another on an axle, which are arranged in a casing with side walls, an inlet opening, and an outlet opening. A stream of the operating medium, up to now usually water, is conducted parallel to the discs onto said discs through the inflow opening. Due to an adhesion force, the discs are then set in motion about the axle. The stream is decelerated by a friction. The stream is redirected onto a circular path by the side walls and thereby continues to drive the discs. Since only the bearings of the axle need to have low tolerances and no highly resilient materials are required, the production costs are also low and a long service life can be expected. Because a higher viscosity arises due to the condensation of the operating medium in the turbine 2, the discs are also driven more powerfully as a result. In typical turbines 2 with blades, a condensation would severely damage said blades. The energy extraction then subsequently takes place by a pressure reduction in the operating medium in the turbine 2.
[0069] To control the cycle, pressure and temperature are measured at the turbine outlet in the return line 6 and compared with the pressure and the temperature in the feed line 5. The cycle can thereupon be regulated via a valve 7 arranged in the return line 6 in order to regulate the flow rate, In this manner, a very good load regulation is possible with simultaneously low complexity.
[0070] The operating medium is then supplied to a recovery device 9 after the valve 7, which device is embodied as a pump in this case.
[0071] In the exemplary embodiments illustrated in
[0072]
[0073] In
[0074]
[0075] A further possibility for generating an oscillation is illustrated in
[0076] To control the flow direction of the operating medium, an additional one-way valve 17 is provided in this case between the valve 7, which is only used here to regulate the flow rate, and the recovery device 9. Alternatively, the flow direction in the apparatus 1 can, of course, also be ensured by a correspondingly embodied valve 7, so that no additional one-way valve 17 is required.
[0077] The one-way valve 17 can, similarly to the valve 7, of course also be provided after the recovery device 9, or between the recovery device 9 and the reservoir 3.
[0078] In the variant according to
[0079] A similar variant is illustrated in
[0080] With the apparatus 1 described above and the method according to the invention, previously unutilized waste heat can be converted into electrical energy under economically beneficial conditions. For example, industrial waste heat in the temperature range of approximately 40° C. to over 300° C., can thereby be used for conversion into electricity. Solar heat can also be utilized for additional electricity generation. Because the system is inherently closed, it can also be used beneficially and advantageously in remote regions without connection to other power supply lines.