(19)
(11) EP 1 936 129 A2

(12) EUROPEAN PATENT APPLICATION

(43) Date of publication:
25.06.2008 Bulletin 2008/26

(21) Application number: 07110803.9

(22) Date of filing: 23.07.1999
(51) International Patent Classification (IPC): 
F01K 25/06(2006.01)
(84) Designated Contracting States:
AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC MT NL PL PT RO SE SI SK TR
Designated Extension States:
AL BA HR MK RS

(62) Application number of the earlier application in accordance with Art. 76 EPC:
99305850.2 / 1070830

(71) Applicant: Exergy, Inc.
Hayward, California 94541 (US)

(72) Inventors:
  • KALINA, Alexander, I.
    Hillsborough,, CA 94010. (US)
  • PELLETIER, Richard, I.
    Livermore,, CA 94550 (US)
  • RHODES, Lawrence, B.
    Livermore,, CA 94550 (US)

(74) Representative: McCall, John Douglas 
W.P. THOMPSON & CO. Coopers Building Church Street
Liverpool L1 3AB
Liverpool L1 3AB (GB)

 
Remarks:
This application was filed on 21 - 06 - 2007 as a divisional application to the application mentioned under INID code 62.
 


(54) Method and apparatus of converting heat to useful energy


(57) A method and apparatus for implementing a thermodynamic cycle. A heated gaseous working stream including a low boiling point component and a higher boiling point component is separated (S), and the low boiling point component is expanded (T) to transform the energy of the stream into useable form and to provide an expanded relatively rich stream (31). This expanded rich stream (31) is then split into two streams, one (33) of which is expanded further to obtain further energy, resulting in a spent stream (34), the other (32) of which is extracted. The lean unexpanded stream (7) and the spent rich stream (34) are then combined in a regenerating subsystem with the extracted stream (32) to reproduce the working stream, which is then efficiently heated in a heater (HE-5) to provide the heated gaseous working stream that is separated.


Description

Background of the Invention



[0001] The invention relates to implementing a thermodynamic cycle to convert heat to useful form.

[0002] Thermal energy can be usefully converted into mechanical and then electrical form. Methods of converting the thermal energy of low temperature heat sources into electric power present an important area of energy generation. There is a need for increasing the efficiency of the conversion of such low temperature heat to electric power.

[0003] Thermal energy from a heat source can be transformed into mechanical and then electrical form using a working fluid that is expanded and regenerated in a closed system operating on a thermodynamic cycle. The working fluid can include components of different boiling temperatures, and the composition of the working fluid can be modified at different places within the system to improve the efficiency of operation. Systems that convert low temperature heat into electric power are described in Alexander I. Kalina's U.S. Pat. Nos. 4,346,561; 4,489,563; 4,982,568; and 5,029,444. In addition, systems with multicomponent working fluids are described in Alexander I. Kalina's U.S. Pat. Nos. 4, 548, 043; 4,586,340, 4,604,867; 4,732,005; 4,763,480, 4,899,545; 5,095,708; 5,440,882; 5,572,871 and 5,649,426, which are hereby incorporated by reference .

Summary of the Invention



[0004] The invention features, in general a method and system for implementing a thermodynamic cycle. A working stream including a low boiling point component and a higher boiling point component is heated with a source of external heat (e.g., a low temperature source) to provide a heated gaseous working stream. The heated gaseous working stream is separated at a first separator to provide a heated gaseous rich stream having relatively more of the low boiling point component and a lean stream having relatively less of the low boiling point component. The heated gaseous rich stream is expanded to transform the energy of the stream into useable form and to provide an expanded, spent rich stream. The lean stream and the expanded, spent rich stream are then combined to provide the working stream.

[0005] Particular embodiments of the invention may include one or more of the following features. The working stream is condensed by transferring heat to a low temperature source at a first heat exchanger and thereafter pumped to a higher pressure. The expanding takes place in a first expansion stage and a second expansion stage, and a stream of partially expanded fluid is extracted between the stages and combined with the lean stream. A separator between the expander stages separates a partially expanded fluid into vapor and liquid portions, and some or all of the vapor portion is fed to the second stage, and some of the vapor portion can be combined with the liquid portion and then combined with the lean stream. A second heat exchanger recuperatively transfers heat from the reconstituted multicomponent working stream (prior to condensing) to the condensed multicomponent working stream at a higher pressure. A third heat exchanger transfers heat from the lean stream to the working stream after the second heat exchanger. The working stream is split into two substreams, one of which is heated with the external heat, the other of which is heated at a fourth heat exchanger with heat from the lean stream; the two streams are then combined to provide the heated gaseous working stream that is separated at the separator.

[0006] Embodiments of the invention may include one or more of the following advantages. Embodiments of the invention can achieve efficiency of conversion of low temperature heat to electric power that exceeds the efficiency of standard Rankine cycles.

[0007] Other advantages and features of the invention will be apparent from the following detailed description of particular embodiments and from the claims.

Brief description of the drawing



[0008] The accompanying drawings and the description thereof, illustrate the invention by way of example. In the drawings:-

Fig. 1 is a diagram of a thermodynamic system for converting heat from a low temperature source to useful form.

Fig. 2 is a diagram of another embodiment of the Fig. 1 system which permits an extracted stream and a completely spent stream to have compositions which are different from the high pressure charged stream.

Fig. 3 is a diagram of a simplified embodiment in which there is no extracted stream.

Fig. 4 is a diagram of a further simplified embodiment.


Detailed Description of the Invention



[0009] Referring to Fig. 1, a system for implementing a thermodynamic cycle to obtain useful energy (e.g., mechanical and then electrical energy) from an external heat source is shown. In the described example, the external heat source is a stream of low temperature waste-heat water that flows in the path represented by points 25-26 through heat exchanger HE-5 and heats working stream 117-17 of the closed thermodynamic cycle. Table 1 presents the conditions at the numbered points indicated on Fig. 1. A typical output from the system is presented in Table 5.

[0010] The working stream of the Fig. 1 system is a multicomponent working stream that includes a low boiling component and a high boiling component. Such a preferred working stream may be an ammonia-water mixture, two or more hydrocarbons, two or more freons, mixtures of hydrocarbons and freons, or the like. In general, the working stream may be mixtures of any number of compounds with favorable thermodynamic characteristics and solubility. In a particularly preferred embodiment, a mixture of water and ammonia is used. In the system shown in Fig. 1, the working stream has the same composition from point 13 to point 19.

[0011] Beginning the discussion of the Fig. 1 system at the exit of turbine T, the stream at point 34 is referred to as the expanded, spent rich stream. This stream is considered "rich" in lower boiling point component. It is at a low pressure and will be mixed with a leaner, absorbing stream having parameters as at point 12 to produce the working stream of intermediate composition having parameters as at point 13. The stream at point 12 is considered "lean" in lower boiling point component.

[0012] At any given temperature, the working stream (of intermediate composition) at point 13 can be condensed at a lower pressure than the richer stream at point 34. This permits more power to be extracted from the turbine T, and increases the efficiency of the process.

[0013] The working stream at point 13 is partially condensed. This stream enters heat exchanger HE-2, where it is cooled and exits the heat exchanger HE-2 having parameters as at point 29. It is still partially, not completely, condensed. The stream now enters heat exchanger HE-1 where it is cooled by stream 23-24 of cooling water, and is thereby completely condensed, obtaining parameters as at point 14. The working stream having parameters as at point 14 is then pumped to a higher pressure obtaining parameters as at point 21. The working stream at point 21 then enters heat exchanger HE-2 where it is recuperatively heated by the working stream at points 13-29 (see above) to a point having parameters as at point 15. The working stream having parameters as at point 15 enters heat exchanger HE-3 where it is heated and obtains parameters as at point 16. In a typical design, point 16 may be precisely at the boiling point but it need not be. The working stream at point 16 is split into two substreams; first working substream 117 and second working substream 118. The first working substream having parameters as at point 117 is sent into heat exchanger HE-5, leaving with parameters as at point 17. It is heated by the external heat source, stream 25-26. The other substream, second working substream 118, enters heat exchanger HE-4 in which it is heated recuperatively, obtaining parameters as at point 18. The two working substreams, 17 and 18, which have exited heat exchangers HE-4 and HE-5, are combined to form a heated, gaseous working stream having parameters as at point 19. This stream is in a state of partial, or possibly complete, vaporization. In the preferred embodiment, point 19 is only partially vaporized. The working stream at point 19 has the same intermediate composition which was produced at point 13, completely condensed at point 14, pumped to a high pressure at point 21, and preheated to point 15 and to point 16. It enters the separator S. There, it is separated into a rich saturated vapor, termed the "heated gaseous rich stream" and having parameters as at point 30, and a lean saturated liquid, termed the "lean stream" and having parameters as at point 7. The lean stream (saturated liquid) at point 7 enters heat exchanger HE-4 where it is cooled while heating working stream 118-18 (see above). The lean stream at point 9 exits heat exchanger HE-4 having parameters as at point 8. It is throttled to a suitably chosen pressure, obtaining parameters as at point 9.

[0014] Returning now to point 30, the heated gaseous rich stream (saturated vapor) exits separator S. This stream enters turbine T where it is expanded to lower pressures, providing useful mechanical energy to turbine T used to generate electricity. A partially expanded stream having parameters as at point 32 is extracted from the turbine T at an intermediate pressure (approximately the pressure as at point 9) and this extracted stream 32 (also referred to as a "second portion" of a partially expanded rich stream, the "first portion" being expanded further) is mixed with the lean stream at point 9 to produce a combined stream having parameters as at point 10. The lean stream having parameters as at point 9 serves as an absorbing stream for the extracted stream 32. The resulting stream (lean stream and second portion) having parameters as at point 10 enters heat exchanger HE-3 where it is cooled, while heating working stream 15-16, to a point having parameters as at point 11. The stream having parameters as at point 11 is then throttled to the pressure of point 34, obtaining parameters as at point 12.

[0015] Returning to turbine T, not all of the turbine inflow was extracted at point 32 in a partially expanded state. The remainder, referred to as the first portion, is expanded to a suitably chosen low pressure and exits the turbine T at point 34. The cycle is closed.

[0016] In the embodiment shown in Fig. 1, the extraction at point 32 has the same composition as the streams at points 30 and 34. In the embodiment shown in Fig. 2, the turbine is shown as first turbine stage T-1 and second turbine stage T-2, with the partially expanded rich stream leaving the higher pressure stage T-1 of the turbine at point 31. Conditions at the numbered points shown on Fig. 2 are presented in Table 2. A typical output from the Fig. 2 system is presented in Table 6.

[0017] Referring to Fig. 2, the partially expanded rich stream from first turbine stage T-1 is divided into a first portion at 33 that is expanded further at lower pressure turbine stage T-2, and a second portion at 32 that is combined with the lean stream at 9. The partially expanded rich stream enters separator S-2. where it is separated into a vapor portion and a liquid portion. The composition of the second portion at 32 may be chosen in order to optimize its effectiveness when it is mixed with the stream at point 9. Separator S-2 permits stream 32 to be as lean as the saturated liquid at the pressure and temperature obtained in the separator S-2; in that case, stream 33 would be a saturated vapor at the conditions obtained in the separator S-2. By choice of the amount of mixing at stream 133, the amount of saturated liquid and the saturated vapor in stream 32 can be varied.

[0018] Referring to Fig. 3, this embodiment differs from the embodiment of Fig. 1, in that the heat exchanger HE-4 has been omitted, and there is no extraction of a partially expanded stream from the turbine stage. In the Fig. 3 embodiment, the hot stream exiting the separator S is admitted directly into heat exchanger HE-3. Conditions at the numbered points shown on Fig. 3 are presented in Table 3. A typical output from the system is presented in Table 7.

[0019] Referring to Fig. 4, this embodiment differs from the Fig. 3 embodiment in omitting heat exchanger HE-2. Conditions at the numbered points shown on Fig. 4 are presented in Table 4. A typical output from the system is presented in Table 8. While omitting heat exchanger HE-2 reduces the efficiency of the process, it may be economically advisable in circumstances where the increased power given up will not pay for the cost of the heat exchanger.

[0020] In general, standard equipment may be utilized in carrying out the method of this invention. Thus, equipment such as heat exchangers, tanks, pumps, turbines, valves and fittings of the type used in a typical Rankine cycles, may be employed in carrying out the method of this invention.

[0021] In the described embodiments of the invention, the working fluid is expanded to drive a turbine of conventional type. However, the expansion of the working fluid from a charged high pressure level to a spent low pressure level to release energy may be effected by any suitable conventional means known to those skilled in the art. The energy so released may be stored or utilized in accordance with any of a number of conventional methods known to those skilled in the art.

[0022] The separators of the described embodiments can be conventionally used gravity separators, such as conventional flash tanks. Any conventional apparatus used to form two or more streams having different compositions from a single stream may be used to form the lean stream and the enriched stream from the fluid working stream.

[0023] The condenser may be any type of known heat rejection device. For example, the condenser may take the form of a heat exchanger, such as a water cooled system, or another type of condensing device.

[0024] Various types of heat sources may be used to drive the cycle of this invention.
Table 1
# P psiA X T °F H BTU/lb G/G30 Flow lb/hr Phase
7 325.22 .5156 202.81 82.29 .5978 276,778 SatLiquid
8 305.22 .5156 169.52 44.55 .5978 276,778 Liq28°
9 214.26 .5156 169.50 44.55 .5978 276,778 Wet.9997
10 214.26 .5533 169.52 90.30 .6513 301,549 Wet.9191
11 194.26 .5533 99.83 -29.79 .6513 301.549 Liq 53°
12 85.43 .5533 99.36 -29.79 .6513 301,549 Wet.9987
13 85.43 .7000 99.83 174.41 1 463,016 Wet. 6651
14 84.43 .7000 72.40 -38.12 1 463,016 SatLiquid
15 350.22 .7000 94.83 -13.08 1 463,016 Liq 73°
16 335.22 .7000 164.52 65.13 1 463,016 SatLiquid
117 335.22 .7000 164.52 65.13 .8955 463,016 SatLiquid
17 325.22 .7000 203.40 302.92 .8955 414,621 Wet .5946
118 335.22 .7000 164.52 65.13 1045 463,016 SatLiquid
18 325.22 .7000 197.81 281.00 .1045 48,395 Wet .6254
19 325.22 .7000 202.81 300.63 1 463,016 Wet .5978
21 355.22 .7000 73.16 -36.76 1 463,016 Liq 96°
29 84.93 .7000 95.02 150.73 1 463,016 Wet .6984
30 325.22 .9740 202.81 625.10 .4022 186,238 SatVapor
32 214.26 .9740 170.19 601.53 .0535 24,771 Wet.0194
34 85.43 .9740 104.60 555.75 .3487 161,467 Wet.0467
23 Water 64.40 32.40 9.8669 4,568,519  
24 Water 83.54 51.54 9.8669 4,568.519  
25 Water 208.40 176.40 5.4766 2,535,750  
26 Water 169.52 137.52 5.4766 2,535,750  
Table 2
# PpsiA X T °F H BTU/lb G/G30 Flow lb/hr Phase
7 325.22 .5156 202.81 82.29 .5978 276,778 SatLiquid
8 305.22 .5156 169.52 44.55 .5978 276,778 Liq 28°
9 214.19 .5156 169.48 44.55 .5978 276,778 Wet.9997
10 214.19 .5523 169.52 89.23 .6570 304,216 Wet.921
11 194.19 .5523 99.74 -29.96 .6570 304,216 Liq 53°
12 85.43 .5523 99.53 -29.96 .6570 304,216 Wet.9992
13 85.43 .7000 99.74 173.96 1 463,016 Wet.6658
14 84.43 .7000 72.40 -38.12 1 463,016 SatLiquid
15 350.22 .7000 94.74 -13.18 1 463,016 Liq73°
16 335.22 .7000 164.52 65.13 1 463,016 SatLiquid
117 335.22 .7000 164.52 65.13 8955 463,016 SatLiquid
17 325.22 .7000 203.40 302.92 .8955 414,621 Wet .5946
118 335.22 .7000 164.52 65.13 .1045 463,016 SatLiquid
18 325.22 .7000 197.81 281.00 .1045 48,395 Wet .6254
19 325.22 .7000 202.81 300.63 1 463,016 Wet.5978
21 355.22 .7000 73.16 -36.76 1 463,016 Liq 96°
29 84.93 .7000 94.96 150.38 1 463,016 Wet.6989
30 325.22 .9740 202.81 625.10 .4022 186,238 SatVapor
31 214.59 .9740 170.63 602.12 .4022 186,238 Wet.0189
32 214.69 .9224 170.63 539.93 .0593 27,437 Wet.1285
33 214.69 .9829 170.63 612.87 .3430 158,800 SatVapor
34 85.43 .9829 102.18 564.60 .3430 158,800 Wet.0294
35 214.69 .5119 170.63 45.44 .0076 3,527 SatLiquid
23 Water 64.40 32.40 9.8666 4,568,371  
24 Water 83.50 51.50 9.8666 4,568,371  
25 Water 208.40 176.40 5.4766 2,535,750  
26 Water 169.52 137.52 5.4766 2,535,750  
Table 3
# P psiA X T °F H BTU/lb G/G30 Flow lb/hr Phase
10 291.89 .4826 203.40 80.72 .6506 294,484 SatLiquid
11 271.89 .4826 109.02 -23.56 .6506 294,484 Liq 89°
12 75.35 .4826 109.07 -23.56 .6506 294,484 Wet .9994
13 75.35 .6527 109.02 180.50 1 452,648 Wet .6669
14 74.35 .6527 72.40 -47.40 1 452,648 SatLiquid
15 316.89 .6527 103.99 -12.43 1 452,648 Liq 64°
16 301.89 .6527 164.52 55.41 1 452,648 SatLiquid
17 291.89 .6527 203.40 273.22 1 452.648 Wet.6506
21 321.89 .6527 73.04 -46.18 1 452,648 Liq97°
29 74.85 .6527 100.84 146.74 1 452,648 Wet.7104,
30 291.89 .9693 203.40 631.64 .3494 158,164 SatVapor
34 75.35 .9693 108.59 560.44 .3494 158,164 Wet.0474
23 Water 64.40 32.40 8.1318 3,680,852  
24 Water 88.27 56.27 8.1318 3,680,852  
25 Water 208.40 176.40 5.6020 2,535,750  
26 Water 169.52 137.52 5.6020 2,535,750  
Table 4
# P psiA X T °F H BTU/lb G/G30 Flow lb/hr Phase
10 214.30 .4059 203.40 80.05 .7420 395,533 SatLiquid
11 194.30 .4059 77.86 -55.30 .7420 395,533 Liq 118°
12 52.48 .4059 78.17 -55.30 .7420 395,533 Liq 32°
29 52.48 .5480 104.46 106.44 1 533,080 Wet .7825
14 51.98 .5480 72.40 -60.06 1 533,080 SatLiquid
21 244.30 .5480 72.83 -59.16 1 533,080 Liq 98°
16 224.30 .5480 164.52 41.26 1 533,080 SatLiquid
17 214.30 .5480 203.40 226.20 1 533,080 Wet .742
30 214.30 .9567 203.40 646.49 .2580 137,546 SatVapor
34 52.48 .9567 114.19 571.55 .2580 137,546 Wet .0473
23 Water 64.40 32.40 5.7346 3,057,018  
24 Water 93.43 61.43 5.7346 3,057,018  
25 Water 208.40 176.40 4.7568 2,535,750  
26 Water 169.52 137.52 4.7568 2.535.750  
Table 5
Performance Summary KCS34 Case 1
Heat in 28893.87 kW 237.78 BTU/lb
Heat rejected 25638.63 kW 210.99 BTU/lb
Σ Turbine enthalpy drops 3420.86 kW 28.15 BTU/lb
Turbine Work 3184.82 kW 26.21 BTU/lb
Feed pump ΔH 1.36, power 175.97 kW 1.45 BTU/lb
Feed + Coolant pump power 364.36 kW 3.00 BTU/lb
Net Work 2820.46 kW 23.21 BTU/lb
Gross Output 3184.82 kWe  
Cycle Output 3008.85 kWe  
Net Output 2820.46 kWe  
Net thermal efficiency 9.76 %  
Second law limit 17.56 %  
Second law efficiency 55.58 %  
Specific Brine Consumption 899.05 lb/kW hr  
Specific Power Output 1.11 Watt hr/lb  
Table 6
Performance Summary KCS34 Case 2
Turbine mass flow 58.34 kg/s 463016 lb/hr
Pt 30 Volume flow 4044.45 l/s 514182 ft^3/hr
Heat in 28893.87 kW 212.93 BTU/lb
Heat rejected 25578.48 kW 188.50 BTU/lb
Σ Turbine enthalpy drops 3500.33 kW 25.80 BTU/lb
Turbine Work 3258.81 kW 24.02 BTU/lb
Feed pump ΔH 1.36. power 196.51 kW 1.45 BTU/lb
Feed + Coolant pump power 408.52 kW 3.01 BTU/lb
Net Work 2850.29 kW 21.00 BTU/lb
Gross Output 3258.81 kWe  
Cycle Output 3062.30 kWe  
Net Output 2850.29 kWe  
Net thermal efficiency 9.86 %  
Second law limit 17.74 %  
Second law efficiency 55.60 %  
Specific Brine Consumption 889.65 lb/kW hr  
Specific Power Output 1.12 Watt hr/lb  
Table 7
Performance Summary KCS34 Case 3
Turbine mass flow 57.03 kg/s 452648 lb/hr
Pt 30 Volume flow 4474.71 1/s 568882 ft3/hr
Heat in 28893.87 kW 217.81 BTU/lb
Heat rejected 25754.18 kW 194.14 BTU/lb
Σ Turbine enthalpy drops 3300.55 kW 24.88 BTU/lb
Turbine Work 3072.82 kW 23.16 BTU/lb
Feed pump ΔH 1.21, power 170.92 kW 1.29 BTU/lb
Feed + Coolant pump power 341.75 kW 2.58 BTU/lb
Net Work 2731.07 kW 20.59 BTU/lb
Gross Output 3072.82 kWe  
Cycle Output 2901.89 kWe  
Net Output 2731.07 kWe  
Net thermal efficiency 9.45 %  
Second law limit 17.39 %  
Second law efficiency 54.34 %  
Specific Brine Consumption 928.48 lb/kW hr  
Specific Power Output 1.08 Watt hr/lb  
Heat to Steam Boiler 15851.00 kW 577.22 BTU/lb
Heat Rejected 10736.96 kW 390.99 BTU/lb
Table 8
Performance Summary KCS34 Case 4
Turbine mass flow 67.17 kg/s 533080 lb/hr
Pt 30 Volume flow 7407.64 l/s 941754 ft^3/hr
Heat in 28893.87 kW 184.94 BTU/lb
Heat rejected 26012.25 kW 166.50 BTU/lb
Σ Turbine enthalpy drops 3020.89 kW 19.34 BTU/lb
Turbine Work 2812.45 kW 18.00 BTU/lb
Feed pump ΔH 89. power 147.99 kW 0.95 BTU/lb
Feed + Coolant pump power 289.86 kW 1.86 BTU/lb
Net Work 2522.59 kW 16.15 BTU/lb
Gross Output 2812.45 kWe  
Cycle Output 2664.46 kWe  
Net Output 2522.59 kWe  
Net thermal efficiency 8.73 %  
Second law limit 17.02 %  
Second law efficiency 51.29 %  
Specific Brine Consumption 1005.22 lb/kW hr  
Specific Power Output 0.99 Watt hr/lb  



Claims

1. A method for implementing a thermodynamic cycle comprising:

heating a working stream including a low boiling point component and a higher boiling point component with a source of external heat to provide a heated gaseous working stream,

separating said heated gaseous working stream at a first separator to provide a heated gaseous rich stream having relatively more of said low boiling point component and a lean stream having relatively less of said low boiling point component,

expanding said heated gaseous rich stream to transform the energy of the stream into useable form and to provide an expanded, spent rich stream, and

combining said lean stream and said expanded, spent rich stream to re-provide said working stream.


 
2. A method as claimed in claim 1, wherein, after said combining and before said heating with said external source of heat, said working stream is condensed by transferring heat to a low temperature source at a first heat exchanger, and said working stream is thereafter pumped to a higher pressure.
 
3. A method as claimed in claim 2, further comprising transferring, at a second heat exchanger, heat from said working stream, prior to said working stream being condensed, to said working stream after said working stream has been pumped to said higher pressure and prior to said heating with said external source of heat.
 
4. A method as claimed in claim 2 or 3, further comprising transferring, at a third heat exchanger, heat from said lean stream to said working stream after said working stream has been pumped to said higher pressure and prior to said heating with said external source of heat.
 
5. A method as claimed in claim 3, further comprising transferring, at a third heat exchanger, heat from said lean stream to said working stream after said working stream has received heat at said second heat exchanger and prior to said heating with said external source of heat.
 
6. A method as claimed in any one of claims 2 to 5, further comprising splitting said working stream, after said pumping and prior to said heating with said external source of heat, into a first working substream and a second working substream, and wherein said heating with said external source of heat involves heating said first working substream with said external source of heat to provide a heated first working substream and thereafter combining said heated first working substream with said second working substream to provide said heated gaseous working stream.
 
7. A method as claimed in claim 6, further comprising transferring, at a fourth heat exchanger, heat from said lean stream to said second working substream.
 
8. A method as claimed in any one of the preceding claims, wherein said heating with said external source of heat occurs at a fifth heat exchanger.
 
9. A method as claimed in any one of the preceding claims, wherein said expanding takes place in a first expansion step and a second expansion step,
said heated gaseous rich stream being partially expanded to provide a partially expanded rich stream in said first expansion step,
further comprising dividing said partially expanded rich stream into a first portion and a second portion,
wherein said first portion is expanded to provide said expanded, spent rich stream in said second expansion step, and
further comprising combining said second portion with said lean stream before said combining of said lean stream and said expanded, spent rich stream.
 
10. A method as claimed in claim 9, wherein said dividing includes separating said partially expanded rich stream into a vapor portion and a liquid portion, said first portion including at least some of said vapor portion, and said second portion including said liquid portion.
 
11. A method as claimed in claim 10, further comprising combining some of said vapor portion with said liquid portion to provide said second portion.
 
12. A method as claimed in any one of claims 9 to 11, further comprising transferring, at a heat exchanger, heat from said lean stream with said second portion to said working stream before said working stream has been heated with said external source of heat.
 
13. Apparatus for implementing a thermodynamic cycle comprising
a heater that heats a working stream including a low boiling point component and a higher boiling point component with a source of external heat to provide a heated gaseous working stream,
a first separator connected to receive said heated gaseous working stream and to output a heated gaseous rich stream having relatively more of said low boiling point component and a lean stream having relatively less of said low boiling point component,
an expander that is connected to receive said heated gaseous rich stream, and transform the energy of the stream into useable form and to output an expanded, spent rich stream, and
a first stream mixer that is connected to combine said lean stream and said expanded, spent rich stream and output said working stream, the output of said stream mixer being connected to the input to said heater.
 
14. An apparatus as claimed in claim 13, further comprising a first heat exchanger and a pump that are connected between said first stream mixer and said heater, said first heat exchanger condensing said working stream by transferring heat to a low temperature source, and said pump thereafter pumping said working stream to a higher pressure.
 
15. An apparatus as claimed in claim 14, further comprising a second heat exchanger connected to transfer heat from said working stream, prior to said working stream being condensed, to said working stream after said working stream has been pumped to said higher pressure at said pump and prior to said heating with said external source of heat at said heater.
 
16. An apparatus as claimed in claim 14 or 15, further comprising a third heat exchanger connected to transfer heat from said lean stream to said working stream after said working stream has been pumped to said higher pressure at said pump and prior to said heating with said external source of heat at said heater.
 
17. An apparatus as claimed in claim 14 or 15, further comprising a third heat exchanger connected to transfer heat from said lean stream to said working stream after said working stream has received heat at said second heat exchanger and prior to said heating with said external source of heat at said heater.
 
18. An apparatus as claimed in any one of claims 14 to 17, further comprising
a stream splitter connected to split said working stream, after said pumping at said pump and prior to said heating with said external source of heat at said heater, into a first working substream and a second working substream, said heater heating said first working substream to provide a heated first working substream, and
a third stream mixer connected to combine said heated first working substream with said second working substream to provide said heated gaseous working stream.
 
19. An apparatus as claimed in claim 18, further comprising a fourth heat exchanger connected to transfer heat from said lean stream to said second working substream.
 
20. An apparatus as claimed in any one of claims 13 to 19, wherein said heater is a fifth heat exchanger.
 
21. An apparatus as claimed in any one of claims 13 to 20, wherein said expander includes a first expansion stage and a second expansion stage,
said first expansion stage being connected to receive said heated gaseous rich stream and to output a partially expanded rich stream,
further comprising a stream divider that is connected to receive said partially expanded rich stream and divide it into a first portion and a second portion,
wherein said second stage is connected to receive said first portion and expands said first portion to provide said expanded, spent rich stream, and
further comprising a second stream mixer that is connected to combine said second portion with said lean stream before said lean stream is combined with said expanded, spent rich stream at said first stream mixer.
 
22. An apparatus as claimed in claim 21, wherein said stream divider includes a second separator that is connected to receive said partially expanded rich stream and to separate it into a vapor portion and a liquid portion, said first portion including at least some of said vapor portion, and said second portion including said liquid portion.
 
23. An apparatus as claimed in claim 22, wherein said stream divider includes a fourth stream mixer connected to combine some of said vapor portion from said second separator with said liquid portion from said second separator to provide said second portion.
 
24. An apparatus as claimed in any one of claims 21 to 23, further comprising a heat exchanger connected to transfer heat from said lean stream with said second portion to said working stream before said working stream has been heated with said external source of heat at said heater.
 




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Cited references

REFERENCES CITED IN THE DESCRIPTION



This list of references cited by the applicant is for the reader's convenience only. It does not form part of the European patent document. Even though great care has been taken in compiling the references, errors or omissions cannot be excluded and the EPO disclaims all liability in this regard.

Patent documents cited in the description