CN202630196U - Spatial composite energy source collecting plate application system - Google Patents
Spatial composite energy source collecting plate application system Download PDFInfo
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- CN202630196U CN202630196U CN 201220078376 CN201220078376U CN202630196U CN 202630196 U CN202630196 U CN 202630196U CN 201220078376 CN201220078376 CN 201220078376 CN 201220078376 U CN201220078376 U CN 201220078376U CN 202630196 U CN202630196 U CN 202630196U
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- pipeline
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- working medium
- collecting plate
- catalyst carrier
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Abstract
The utility model provides a spatial composite energy source collecting plate application system. The spatial composite energy source collecting plate application system comprises a spatial composite energy source collecting plate, a first compressor, a first condenser, a second evaporator condenser, a heat-carrying agent circulating pump, and tail end heating equipment, wherein the first compressor is connected with the output end of the spatial composite energy source collecting plate through a first pipeline; the first condenser is connected with the output end of the first compressor through a second pipeline; the second evaporator condenser is connected with the first output end of the first condenser through a fourth pipeline; the first output end of the second evaporator condenser is connected with the spatial composite energy source collecting plate through a fifth pipeline; the heat-carrying agent circulating pump is connected with the second output end of the first condenser through a sixth pipeline; the tail end heating equipment is connected with the heat-carrying agent circulating pump; and the spatial composite energy source collecting plate, the first pipeline, the first compressor, the second pipeline, the first condenser, the fourth pipeline, the second evaporator condenser and the fifth pipeline form a first circulating loop. By the application system provided by the utility model, heat energy can be provided, and energy resources can be saved.
Description
Technical field
The utility model relates to space compound energy energy collecting plate applied technical field, is meant a kind of space compound energy energy collecting plate application system especially.
Background technology
The working medium majority of conventional heat pump use at present produces atmospheric ozone layer and destroys, and traditional working medium also has other unknown side effects.
Current conventional heat pump working medium hot property in low temperature environment is poor, is difficult to the heating of low temperature environment, and the maximum characteristics of the space compound energy are that operating rate is fast, and traditional working medium is difficult to reach the high heat exchange efficiency that matches.
The upper limit that tradition working medium produces hot water generally was merely for 50 several years, and is relatively low.
CO
2Have high critical pressure and low critical-temperature as heat pump fluid, operating pressure is high, and traditional operation of heat pump mode can not meet the demands.
The utility model content
The technical problem that the utility model will solve provides a kind of space compound energy energy collecting plate application system, can in low temperature environment, a large amount of space compound energy conversion be become operational heat energy, energy savings.
For solving the problems of the technologies described above, the new embodiment of this practicality provides a kind of space compound energy energy collecting plate application system, comprising:
Space compound energy energy collecting plate 2;
First compressor 1 is connected through first pipeline 21 with said space compound energy energy collecting plate 2 outputs;
First condenser 11 is connected through second pipeline 22 with the output of said first compressor 1;
Second condenser/evaporator 4 is connected through the 4th pipeline 24 with first output of said first condenser 11, and first output of said second condenser/evaporator 4 also is connected through the 5th pipeline 25 with said space compound energy energy collecting plate 2;
Catalyst carrier circulating pump 10 is connected through the 6th pipeline 26 with second output of said first condenser 11;
Terminal heating equipment 9 is connected with said catalyst carrier circulating pump 10;
Wherein, said space compound energy energy collecting plate 2, said first pipeline 21, said first compressor 1, said second pipeline 22, said first condenser 11, said the 4th pipeline 24, said second condenser/evaporator 4 and said the 5th pipeline 25 form first closed circuit.
Wherein, said first pipeline 21 is to carry low temperature CO
2The pipeline of working medium, said low temperature CO
2Working medium has absorbed the heat energy that said space compound energy energy collecting plate 2 absorbs;
Said second pipeline 22 is to carry high temperature CO
2The pipeline of working medium, said high temperature CO
2Working medium is the said low temperature CO that carries in 1 pair of said first pipeline of said first compressor
2The high temperature CO that obtains after the working medium compression
2Working medium;
Said the 4th pipeline 24 is to carry 11 pairs of said high temperature CO of said first condenser
2The high temperature CO that working medium obtains after carrying out lowering the temperature for the first time
2The pipeline of working medium;
Said the 5th pipeline 25 is to carry 4 pairs of high temperature CO that obtain after the cooling the said first time of said second condenser/evaporator
2The liquid CO that working medium obtains after lowering the temperature for the second time
2The pipeline of working medium;
Said the 6th pipeline 26 is the pipelines that carry the high temperature catalyst carrier, and said high temperature catalyst carrier is that said first condenser 11 utilizes the high temperature CO in said second pipeline 22
2The high temperature catalyst carrier that working medium obtains after to said catalyst carrier heat exchange, said high temperature catalyst carrier is transferred to said terminal heating equipment 9 through said catalyst carrier circulating pump 10.
Wherein, said first compressor 1 has first water jacket 61; Said first water jacket 61 is connected with said first condenser 11 through the 3rd pipeline; Said terminal heating equipment 9 is connected with said first water jacket 61 through the 7th pipeline 27;
Wherein, first water jacket 61 of said first compressor 1, said the 3rd pipeline 23, said first condenser 11, said the 6th pipeline 26, said catalyst carrier circulating pump 10, said terminal heating equipment 9 and said the 7th pipeline 27 form second closed circuit.
Wherein, said the 3rd pipeline 23 is the pipelines that carry catalyst carrier; Said the 7th pipeline 27 is to carry the pipeline of being exported and inputed to the catalyst carrier of said first water jacket 61 by said terminal heating heating equipment 9.
Wherein, said the 5th pipeline 25 between first output of said second condenser/evaporator 4 and the said space compound energy energy collecting plate 2 is provided with first throttle valve 3.
Wherein, above-mentioned space compound energy energy collecting plate application system also comprises:
Second compressor 5 is connected through the 8th pipeline 28 with second output of said second condenser/evaporator 4;
The 3rd condenser 8 is connected through the 9th pipeline 29 with first output of said second compressor 5;
First output of said the 3rd condenser 8 is connected through the 11 pipeline 31 with said second condenser/evaporator 4, and second output of said the 3rd condenser 8 is connected through the 12 pipeline 32 with said catalyst carrier circulating pump 10;
Wherein, said second condenser/evaporator 4, said the 8th pipeline 28, said second compressor 5, said the 9th pipeline 29, said the 3rd condenser 8 and said the 11 pipeline 31 form the 3rd closed circuit.
Wherein, said the 8th pipeline 28 is the pipelines that carry high-temperature low-pressure working medium;
Said the 9th pipeline 29 is the pipelines that carry HTHP working medium, and wherein said HTHP working medium is the HTHP working medium that obtains after 5 pairs of said high temperature refrigerants of said second compressor compress;
Said the 11 pipeline 31 is the pipelines that carry liquid refrigerant, and said liquid refrigerant is the liquid refrigerant that obtains after 4 pairs of said HTHP working medium of said second condenser/evaporator are lowered the temperature;
Said the 12 pipeline 32 is the pipelines that carry the high temperature catalyst carrier that obtains behind the energy that absorbs said HTHP working medium.
Wherein, said the 11 pipeline 31 between first output of said the 3rd condenser 8 and said second condenser/evaporator 4 is provided with second choke valve 7.
Wherein, said second compressor 5 has second water jacket 62, and said terminal heating equipment 9 is connected with said second water jacket 62 through the 13 pipeline 33, and said the 3rd condenser 8 is connected with said second water jacket 62 through the tenth pipeline 30; Wherein, said the tenth pipeline 30 is the pipelines that carry said catalyst carrier;
Wherein, second water jacket 62 of said second compressor 5, said the tenth pipeline 30, said the 3rd condenser 8, said the 12 pipeline 32, said catalyst carrier circulating pump 10, said terminal heating equipment 9 and said the 13 pipeline 33 form the 4th closed circuit.
Wherein, said the 13 pipeline 33 is to carry the pipeline of being exported and inputed to the catalyst carrier of said second water jacket 62 by said terminal heating equipment 9.
The beneficial effect of the technique scheme of the utility model is following:
In the such scheme, realize obtaining the high temperature catalyst carrier in the low temperature environment, and do not waste energy, make abundant space compound energy conversion become operational heat energy.
Description of drawings
Fig. 1 is the space compound energy energy collecting plate application system structure chart of the utility model.
The specific embodiment
For technical problem, technical scheme and advantage that the utility model will be solved is clearer, will combine accompanying drawing and specific embodiment to be described in detail below.
As shown in Figure 1, the embodiment of the utility model provides a kind of space compound energy energy collecting plate application system, comprising: space compound energy energy collecting plate 2; First compressor 1 is connected through first pipeline 21 with the output of said space compound energy energy collecting plate 2; First condenser 11 is connected through second pipeline 22 with the output of said first compressor 1; Second condenser/evaporator 4 is connected through the 4th pipeline 24 with first output of said first condenser 11, and first output of said second condenser/evaporator 4 also is connected through the 5th pipeline 25 with said space compound energy energy collecting plate 2; Catalyst carrier circulating pump 10 is connected through the 6th pipeline 26 with second output of said first condenser 11; Terminal heating equipment 9 is connected with said catalyst carrier circulating pump 10; Wherein, said space compound energy energy collecting plate 2, said first pipeline 21, said first compressor 1, said second pipeline 22, said first condenser 11, said the 4th pipeline 24, said second condenser/evaporator 4 and said the 5th pipeline 25 form first closed circuit.
Wherein, said first pipeline 21 is to carry low temperature CO
2The pipeline of working medium, said low temperature CO
2Working medium has absorbed the heat energy that said space compound energy energy collecting plate 2 absorbs; Said second pipeline 22 is to carry high temperature CO
2The pipeline of working medium, said high temperature CO
2Working medium is the said low temperature CO that carries in 1 pair of said first pipeline of said first compressor
2The high temperature CO that obtains after the working medium compression
2Working medium; Said the 4th pipeline 24 is to carry 11 pairs of said high temperature CO of said first condenser
2The high temperature CO that working medium obtains after carrying out lowering the temperature for the first time
2The pipeline of working medium; Said the 5th pipeline 25 is to carry 4 pairs of high temperature CO that obtain after the cooling the said first time of said second condenser/evaporator
2The liquid CO that working medium obtains after lowering the temperature for the second time
2The pipeline of working medium; Said the 3rd pipeline 23 is the pipelines that carry catalyst carrier; Said the 6th pipeline 26 is the pipelines that carry the high temperature catalyst carrier, and said high temperature catalyst carrier is that said first condenser 11 utilizes the high temperature CO in said second pipeline 22
2The high temperature catalyst carrier that working medium obtains after to said catalyst carrier heat exchange, said high temperature catalyst carrier is transferred to said terminal heating equipment 9 through said catalyst carrier circulating pump 10.
Wherein, said first compressor 1 has first water jacket 61; Said first water jacket 61 is connected with said first condenser 11 through the 3rd pipeline 23; Said terminal heating equipment 9 is connected with said first water jacket 61 through the 7th pipeline 27; Wherein, first water jacket 61 of said first compressor 1, said the 3rd pipeline 23, said first condenser 11, said the 6th pipeline 26, said catalyst carrier circulating pump 10, said terminal heating equipment 9 and said the 7th pipeline 27 form second closed circuit.
Wherein, said the 3rd pipeline 23 is the pipelines that carry catalyst carrier; Said the 7th pipeline 27 is to carry the pipeline of being exported and inputed to the catalyst carrier of said first water jacket 61 by said terminal heating equipment 9.
Wherein, said the 5th pipeline 25 between first output of said second condenser/evaporator 4 and the said space compound energy energy collecting plate 2 is provided with first throttle valve 3, the CO of 3 pairs second condenser/evaporators of this first throttle valve, 4 outputs
2Working medium is carried out step-down, this CO
2After getting back to space compound energy energy collecting plate 2, reuptake the heat that this space compound energy energy collecting plate 2 absorbs, get back to first pipeline 21 once more, and get into first compressor 1.
Preferably, said system can also comprise: second compressor 5 is connected through the 8th pipeline 28 with second output of said second condenser/evaporator 4; The 3rd condenser 8 is connected through the 9th pipeline 29 with first output of said second compressor 5; First output of said the 3rd condenser 8 is connected through the 11 pipeline 31 with said second condenser/evaporator 4, and second output of said the 3rd condenser 8 is connected through the 12 pipeline 32 with said catalyst carrier circulating pump 10; Wherein, said second condenser/evaporator 4, said the 8th pipeline 28, said second compressor 5, said the 9th pipeline 29, said the 3rd condenser 8 and said the 11 pipeline 31 form the 3rd closed circuit.
Wherein, said the 8th pipeline 28 is the pipelines that carry high-temperature low-pressure working medium; Said the 9th pipeline 29 is the pipelines that carry HTHP working medium, and wherein said HTHP working medium is the HTHP working medium that obtains after 5 pairs of said high temperature refrigerants of said second compressor compress; Said the 11 pipeline 31 is the pipelines that carry liquid refrigerant, and said liquid refrigerant is the liquid refrigerant that obtains after 4 pairs of said HTHP working medium of said second condenser/evaporator are lowered the temperature; Said the 12 pipeline 32 is the pipelines that carry the high temperature catalyst carrier that obtains behind the energy that absorbs said HTHP working medium.
Wherein, said the 11 pipeline 31 between first output of said the 3rd condenser 8 and said second condenser/evaporator 4 is provided with second choke valve 7.
Wherein, Said second compressor 5 has second water jacket 62; Said terminal heating equipment 9 is connected with said second water jacket 62 through the 13 pipeline 33, and said the 3rd condenser 8 is connected with said second water jacket 62 through the tenth pipeline 30, and said the tenth pipeline 30 is the pipelines that carry said catalyst carrier; Wherein, second water jacket 62 of said second compressor 5, said the tenth pipeline 30, said the 3rd condenser 8, said the 12 pipeline 32, said catalyst carrier circulating pump 10, said terminal heating equipment 9 and said the 13 pipeline 33 form the 4th closed circuit.
Wherein, said the 13 pipeline 33 is to carry the pipeline of being exported and inputed to the catalyst carrier of said second water jacket 62 by said terminal heating equipment 9.
In the such scheme, first compressor 1 will contain the CO of great amount of heat energy from the space compound energy
2Be compressed into high temperature CO
2Gas is sent into first condenser 11, gives the catalyst carrier of flowing through same first condenser 11 and being sent here by catalyst carrier circulating pump 10 with a part of thermal energy conduction, through cooling for the first time, and the first cooling back CO
2Gas gets into second condenser/evaporator 4 again, has been absorbed great amount of heat energy and has become liquid CO by high temperature level working medium
2, liquid CO
2After 3 step-downs of first throttle valve, inject space compound energy collecting plate 2, the compound energy in the fast Absorption space compound energy energy collecting plate 2 has absorbed the CO of compound energy
2Become gas again, return first compressor 1.
Second compressor 5 will suck and be compressed into the HTHP Working medium gas by the high temperature refrigerant gas that has absorbed great amount of heat energy in second condenser/evaporator 4; Send into the 3rd condenser 8; Thermal energy conduction is given the catalyst carrier of flowing through the 3rd condenser 8 and sending here equally by catalyst carrier circulating pump 10; Self is through cooling liquefy working medium, and liquid refrigerant is injected second condenser/evaporator 4 through 7 step-downs of second choke valve, absorbs the high temperature CO of second condenser/evaporator 4 of flowing through equally
2The heat energy of gas makes CO
2The rapid decrease temperature and pressure of gas, liquefy CO
2, absorbed the high temperature level working medium of heat energy, become high-temperature gas working medium heavily again and get into second compressor 5.Catalyst carrier in second water jacket 62 of second compressor 5 is stablized second compressor, 5 temperature, and gets into the 3rd condenser 8 and become the high temperature catalyst carrier; Equally, the catalyst carrier in first water jacket 61 of first compressor 1 is stablized the temperature of first compressor 1 and is got into first condenser 11, absorbs CO
2The heat energy that high temperature level working medium produces becomes the high temperature catalyst carrier, delivers to terminal heating equipment 9 like high-temperature water, has accomplished the space compound energy and has become operational heat energy process.
Native system can produce a large amount of heat energy, can be widely used in various building heatings and hot water supply.Be used for transmitting between heat pump (compressor) system and the space compound energy energy collecting plate 2 CO of energy
2Being natural refrigerant, is zero to depletion of the ozone layer potential, and greenhouse effects potential is 1000-2000/one of conventional heat pump working medium, and natural environment is not had destruction.CO
2Heat exchange efficiency be the several times of traditional working medium, heating capacity be traditional working medium 6-10 doubly, with space compound energy energy collecting plate 2 high speed absorptivities good coupling, CO are arranged
2Working medium can become the above hot water of 90 degree with the space compound energy conversion, can satisfy the human multiple heat request of using.CO
2Working medium has high critical pressure and low critical-temperature, and operating pressure is higher than traditional operation of heat pump mode.Adopt the overlapping method of operation, CO
2Compressor has reduced CO as the low temperature machine
2Operating pressure, make traditional heat pump also can use CO
2Working medium realizes obtaining the high temperature catalyst carrier in the low temperature environment, and does not waste energy, and makes abundant space compound energy conversion become operational heat energy.
The above is the preferred implementation of the utility model; Should be understood that; For those skilled in the art; Under the prerequisite that does not break away from the said principle of the utility model, can also make some improvement and retouching, these improvement and retouching also should be regarded as the protection domain of the utility model.
Claims (10)
1. a space compound energy energy collecting plate application system is characterized in that, comprising:
Space compound energy energy collecting plate (2);
First compressor (1) is connected through first pipeline (21) with the output of said space compound energy energy collecting plate (2);
First condenser (11) is connected through second pipeline (22) with the output of said first compressor (1);
Second condenser/evaporator (4); Be connected through the 4th pipeline (24) with first output of said first condenser (11), first output of said second condenser/evaporator (4) also is connected through the 5th pipeline (25) with said space compound energy energy collecting plate (2);
Catalyst carrier circulating pump (10) is connected through the 6th pipeline (26) with second output of said first condenser (11);
Terminal heating equipment (9) is connected with said catalyst carrier circulating pump (10);
Wherein, said space compound energy energy collecting plate (2), said first pipeline (21), said first compressor (1), said second pipeline (22), said first condenser (11), said the 4th pipeline (24), said second condenser/evaporator (4) and said the 5th pipeline (25) form first closed circuit.
2. space compound energy energy collecting plate application system according to claim 1 is characterized in that,
Said first pipeline (21) is to carry low temperature CO
2The pipeline of working medium, said low temperature CO
2Working medium has absorbed the heat energy that said space compound energy energy collecting plate (2) absorbs;
Said second pipeline (22) is to carry high temperature CO
2The pipeline of working medium, said high temperature CO
2Working medium is the said low temperature CO of said first compressor (1) to carrying in said first pipeline
2The high temperature CO that obtains after the working medium compression
2Working medium;
Said the 4th pipeline (24) is to carry said first condenser (11) to said high temperature CO
2The high temperature CO that working medium obtains after carrying out lowering the temperature for the first time
2The pipeline of working medium;
Said the 5th pipeline (25) is to carry the high temperature CO that said second condenser/evaporator (4) obtained after the cooling the said first time
2The liquid CO that working medium obtains after lowering the temperature for the second time
2The pipeline of working medium;
Said the 6th pipeline (26) is the pipeline that carries the high temperature catalyst carrier, and said high temperature catalyst carrier is that said first condenser (11) utilizes the high temperature CO in said second pipeline (22)
2The high temperature catalyst carrier that working medium obtains after to said catalyst carrier heat exchange, said high temperature catalyst carrier is transferred to said terminal heating equipment (9) through said catalyst carrier circulating pump (10).
3. space compound energy energy collecting plate application system according to claim 2 is characterized in that said first compressor (1) has first water jacket (61);
Said first water jacket (61) is connected with said first condenser (11) through the 3rd pipeline (23);
Said terminal heating equipment (9) is connected with said first water jacket (61) through the 7th pipeline (27);
Wherein, first water jacket (61) of said first compressor (1), said the 3rd pipeline (23), said first condenser (11), said the 6th pipeline (26), said catalyst carrier circulating pump (10), said terminal heating equipment (9) and said the 7th pipeline (27) form second closed circuit.
4. space compound energy energy collecting plate application system according to claim 3 is characterized in that,
Said the 3rd pipeline (23) is the pipeline that carries catalyst carrier;
Said the 7th pipeline (27) is to carry the pipeline of being exported and inputed to the catalyst carrier of said first water jacket (61) by said terminal heating equipment (9).
5. space compound energy energy collecting plate application system according to claim 1; It is characterized in that said the 5th pipeline (25) between first output of said second condenser/evaporator (4) and the said space compound energy energy collecting plate (2) is provided with first throttle valve (3).
6. space compound energy energy collecting plate application system according to claim 1 is characterized in that, also comprises:
Second compressor (5) is connected through the 8th pipeline (28) with second output of said second condenser/evaporator (4);
The 3rd condenser (8) is connected through the 9th pipeline (29) with first output of said second compressor (5);
First output of said the 3rd condenser (8) is connected through the 11 pipeline (31) with said second condenser/evaporator (4), and second output of said the 3rd condenser (8) is connected through the 12 pipeline (32) with said catalyst carrier circulating pump (10);
Wherein, said second condenser/evaporator (4), said the 8th pipeline (28), said second compressor (5), said the 9th pipeline (29), said the 3rd condenser (8) and said the 11 pipeline (31) form the 3rd closed circuit.
7. space compound energy energy collecting plate application system according to claim 6 is characterized in that,
Said the 8th pipeline (28) is the pipeline that carries high-temperature low-pressure working medium;
Said the 9th pipeline (29) is the pipeline that carries HTHP working medium, and wherein said HTHP working medium is the HTHP working medium that obtains after said second compressor (5) compresses said high temperature refrigerant;
Said the 11 pipeline (31) is the pipeline that carries liquid refrigerant, and said liquid refrigerant is the liquid refrigerant that obtains after said second condenser/evaporator (4) is lowered the temperature to said HTHP working medium;
Said the 12 pipeline (32) is the pipeline that carries the high temperature catalyst carrier that obtains behind the energy that absorbs said HTHP working medium.
8. space compound energy energy collecting plate application system according to claim 6; It is characterized in that said the 11 pipeline (31) between first output of said the 3rd condenser (8) and said second condenser/evaporator (4) is provided with second choke valve (7).
9. space compound energy energy collecting plate application system according to claim 6; It is characterized in that; Said second compressor (5) has second water jacket (62); Said terminal heating equipment (9) is connected with said second water jacket (62) through the 13 pipeline (33), and said the 3rd condenser (8) is connected with said second water jacket (62) through the tenth pipeline (30); Said the tenth pipeline (30) is the pipeline that carries said catalyst carrier;
Wherein, second water jacket (62) of said second compressor (5), said the tenth pipeline (30), said the 3rd condenser (8), said the 12 pipeline (32), said catalyst carrier circulating pump (10), said terminal heating equipment (9) and said the 13 pipeline (33) form the 4th closed circuit.
10. space compound energy energy collecting plate application system according to claim 9 is characterized in that,
Said the 13 pipeline (33) is to carry the pipeline of being exported and inputed to the catalyst carrier of said second water jacket (62) by said terminal heating equipment (9).
Priority Applications (1)
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CN 201220078376 CN202630196U (en) | 2012-03-05 | 2012-03-05 | Spatial composite energy source collecting plate application system |
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CN 201220078376 CN202630196U (en) | 2012-03-05 | 2012-03-05 | Spatial composite energy source collecting plate application system |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105509125B (en) * | 2016-01-18 | 2018-06-26 | 西安交通大学 | A kind of Trans-critical cycle CO with quickly defrosting function2Heat pump heating system |
-
2012
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105509125B (en) * | 2016-01-18 | 2018-06-26 | 西安交通大学 | A kind of Trans-critical cycle CO with quickly defrosting function2Heat pump heating system |
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