CN103174517A - Cold-source-acting impeller Stirling hot-air engine - Google Patents
Cold-source-acting impeller Stirling hot-air engine Download PDFInfo
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- CN103174517A CN103174517A CN2013100695487A CN201310069548A CN103174517A CN 103174517 A CN103174517 A CN 103174517A CN 2013100695487 A CN2013100695487 A CN 2013100695487A CN 201310069548 A CN201310069548 A CN 201310069548A CN 103174517 A CN103174517 A CN 103174517A
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Abstract
The invention discloses a cold-source-acting impeller Stirling hot-air engine comprising an impeller air compressor, a turbine power mechanism, an affiliated turbine power mechanism, an affiliated impeller air compressor, an external combustion heater, and a cooler. The impeller air compressor, the turbine power mechanism, the affiliated turbine power mechanism, and the affiliated impeller air compressor are sequentially communicated, such that a working medium closed circuit is formed. The external combustion heater is arranged in a communication channel between the working medium outlet of the impeller air compressor and the working medium inlet of the turbine power mechanism. The cooler is arranged in a communication channel between the affiliated turbine power mechanism and the affiliated impeller air compressor. The cold-source-acting impeller Stirling hot-air engine provided by the invention has the advantages of simple structure, high efficiency, low cost, and long service life.
Description
Technical field
The present invention relates to heat energy and power field, especially a kind of low-temperature receiver work doing impeller heat engine.
Background technique
Tradition heat engine compression ratio very low (compression ratio of best Stirling engine is only 2 left and right in the world at present) is having a strong impact on the efficient of motor, so is needing a kind of Novel hot mechanism of qi of invention, is used for improving the efficient of heat engine.
Summary of the invention
In order to address the above problem, the technological scheme that the present invention proposes is as follows:
A kind of low-temperature receiver work doing impeller heat engine comprises impeller gas compressor, turbo-power mechanism, attached turbo-power mechanism, attached impeller gas compressor, external combustion heater and cooler; Described impeller gas compressor, described turbo-power mechanism, described attached turbo-power mechanism and described attached impeller gas compressor are interconnected successively and form the working medium closed-loop path; Described external combustion heater is arranged on communicating passage between the working medium entrance of the sender property outlet of described impeller gas compressor and described turbo-power mechanism; Described cooler is arranged on communicating passage between the working medium entrance of the sender property outlet of described attached turbo-power mechanism and described attached impeller gas compressor.
A kind of low-temperature receiver work doing impeller heat engine comprises impeller gas compressor, turbo-power mechanism, attached turbo-power mechanism, attached impeller gas compressor, internal combustion firing chamber and cooler; Described impeller gas compressor, described turbo-power mechanism, described attached turbo-power mechanism and described attached impeller gas compressor are interconnected successively and form the working medium closed-loop path; Described internal combustion firing chamber is arranged in communicating passage between the working medium entrance of the sender property outlet of described impeller gas compressor and described turbo-power mechanism; Described cooler is arranged on communicating passage between the working medium entrance of the sender property outlet of described attached turbo-power mechanism and described attached impeller gas compressor; On described working medium closed-loop path, the working medium export mouth is set.
A kind of low-temperature receiver work doing impeller heat engine comprises impeller gas compressor, turbo-power mechanism, attached turbo-power mechanism, attached impeller gas compressor, external combustion heater, cooler and reciprocal communicating passage; The sender property outlet of described impeller gas compressor is communicated with the working medium entrance of described turbo-power mechanism, the sender property outlet of described attached turbo-power mechanism is communicated with the working medium entrance of described attached impeller gas compressor, the sender property outlet of the working medium entrance of described impeller gas compressor and described turbo-power mechanism is communicated with an end of described reciprocal communicating passage through control valve respectively, the working medium entrance of described attached turbo-power mechanism and the sender property outlet of described attached impeller gas compressor are communicated with the other end of described reciprocal communicating passage through control valve respectively, form the working medium closed-loop path; Described heater is arranged on communicating passage between the working medium entrance of the sender property outlet of described impeller gas compressor and described turbo-power mechanism; Described cooler is arranged on communicating passage between the working medium entrance of the sender property outlet of described attached turbo-power mechanism and described attached impeller gas compressor.
A kind of low-temperature receiver work doing impeller heat engine comprises impeller gas compressor, turbo-power mechanism, attached turbo-power mechanism, attached impeller gas compressor, internal combustion firing chamber, cooler and reciprocal communicating passage; The sender property outlet of described impeller gas compressor is communicated with the working medium entrance of described turbo-power mechanism, the sender property outlet of described attached turbo-power mechanism is communicated with the working medium entrance of described attached impeller gas compressor, the sender property outlet of the working medium entrance of described impeller gas compressor and described turbo-power mechanism is communicated with an end of described reciprocal communicating passage through control valve respectively, the working medium entrance of described attached turbo-power mechanism and the sender property outlet of described attached impeller gas compressor are communicated with the other end of described reciprocal communicating passage through control valve respectively, form the working medium closed-loop path; Described internal combustion firing chamber is arranged in communicating passage between the working medium entrance of the sender property outlet of described impeller gas compressor and described turbo-power mechanism; Described cooler is arranged on communicating passage between the working medium entrance of the sender property outlet of described attached turbo-power mechanism and described attached impeller gas compressor; On described working medium closed-loop path, the working medium export mouth is set.
Coaxial setting more than two in described impeller gas compressor, described turbo-power mechanism, described attached turbo-power mechanism and described attached impeller gas compressor.
Described low-temperature receiver work doing impeller heat engine also comprises the heat exchanger type regenerator, the sender property outlet of described turbo-power mechanism is communicated with the working medium entrance of described attached turbo-power mechanism through the fluid passage that is cooled of described heat exchanger type regenerator, and the sender property outlet of described attached impeller gas compressor is communicated with the working medium entrance of described impeller gas compressor through the fluid passage that is heated of described heat exchanger type regenerator.
On described reciprocal communicating passage, the material filling type regenerator is set.
The place arranges control valve at described working medium export mouth.
In the present invention, described material filling type regenerator refers to leave the heat of self for filler, the device of the heat that dry load is stored when the cryogenic fluid retrograde flow is crossed territory, porous packing area when high temperature refrigerant flows through the porous aggregate zone.
In the present invention, described cooler refers to make the device of working medium cooling in the present invention, and it can be radiator, can be also heat exchanger.
In the present invention, should according to the known technology in heat energy and power field, necessary parts, unit or system etc. be set in the place of necessity.
Beneficial effect of the present invention is as follows:
The present invention is simple in structure, efficient is high, the low long service life of cost.
Description of drawings
Shown in Figure 1 is the structural representation of the embodiment of the present invention 1;
Shown in Figure 2 is the structural representation of the embodiment of the present invention 2;
Shown in Figure 3 is the structural representation of the embodiment of the present invention 3;
Shown in Figure 4 is the structural representation of the embodiment of the present invention 4;
Shown in Figure 5 is the structural representation of the embodiment of the present invention 5;
Shown in Figure 6 is the structural representation of the embodiment of the present invention 6;
In figure:
1 impeller gas compressor, 2 turbo-power mechanisms, 3 attached turbo-power mechanisms, 4 attached impeller gas compressors, 5 external combustion heaters, 6 coolers, 7 heat exchanger type regenerators, 8 material filling type regenerators, 9 internal combustion firing chambers, 10 working medium export mouths, 11 reciprocal communicating passage, 12 timing control valves, 13 control valves.
Embodiment
Embodiment 1
Low-temperature receiver work doing impeller heat engine as shown in Figure 1 comprises impeller gas compressor 1, turbo-power mechanism 2, attached turbo-power mechanism 3, attached impeller gas compressor 4, external combustion heater 5 and cooler 6; Described impeller gas compressor 1, described turbo-power mechanism 2, described attached turbo-power mechanism 3 and described attached impeller gas compressor 4 are interconnected successively and form the working medium closed-loop path; Described external combustion heater 5 is arranged on communicating passage between the working medium entrance of the sender property outlet of described impeller gas compressor 1 and described turbo-power mechanism 2; Described cooler 6 is arranged on communicating passage between the working medium entrance of the sender property outlet of described attached turbo-power mechanism 3 and described attached impeller gas compressor 4, described impeller gas compressor 1 and the 2 coaxial settings of described turbo-power mechanism, described attached turbo-power mechanism 3 and the coaxial setting of described attached impeller gas compressor 4.
Low-temperature receiver work doing impeller heat engine as shown in Figure 2 comprises impeller gas compressor 1, turbo-power mechanism 2, attached turbo-power mechanism 3, attached impeller gas compressor 4, internal combustion firing chamber 9 and cooler 6; Described impeller gas compressor 1, described turbo-power mechanism 2, described attached turbo-power mechanism 3 and described attached impeller gas compressor 4 are interconnected successively and form the working medium closed-loop path; Described internal combustion firing chamber 9 is arranged in communicating passage between the working medium entrance of the sender property outlet of described impeller gas compressor 1 and described turbo-power mechanism 2; Described cooler 6 is arranged on communicating passage between the working medium entrance of the sender property outlet of described attached turbo-power mechanism 3 and described attached impeller gas compressor 4; On described working medium closed-loop path, working medium export mouth 10 is set, 10 places arrange control valve 13 at described working medium export mouth, particularly, described working medium export mouth 10 is arranged on communicating passage between the working medium entrance of the sender property outlet of described attached impeller gas compressor 4 and described impeller gas compressor 1, described impeller gas compressor 1 and the 2 coaxial settings of described turbo-power mechanism, described attached turbo-power mechanism 3 and the coaxial setting of described attached impeller gas compressor 4.
As disposable mode of execution, described working medium export mouth 10 can be arranged on other any position on described working medium closed-loop path, for example can be arranged on the sender property outlet and the communicating passage between described cooler 6 of described attached turbo-power mechanism 3; Described control valve 13 can not established.
Low-temperature receiver work doing impeller heat engine as shown in Figure 3, itself and embodiment's 1 difference is: described low-temperature receiver work doing impeller heat engine also comprises heat exchanger type regenerator 7, the sender property outlet of described turbo-power mechanism 2 is communicated with the working medium entrance of described attached turbo-power mechanism 3 through the fluid passage that is cooled of described heat exchanger type regenerator 7, and the sender property outlet of described attached impeller gas compressor 4 is communicated with the working medium entrance of described impeller gas compressor 1 through the fluid passage that is heated of described heat exchanger type regenerator 7.
As disposable mode of execution, embodiment 2 and embodiment 4 all can arrange described heat exchanger type regenerator 7 with reference to the present embodiment.
Low-temperature receiver work doing impeller heat engine as shown in Figure 4, itself and embodiment's 1 difference is: described turbo-power mechanism 2 and described impeller gas compressor 1 all are made as two, and the sender property outlet of each described turbo-power mechanism 2 all is communicated with the working medium entrance of described attached turbo-power mechanism 3, and the working medium entrance of each described impeller gas compressor 1 all is communicated with the sender property outlet of described attached impeller gas compressor 4.
As disposable mode of execution, above-described embodiment 1 also can all be made as two with described turbo-power mechanism 2 and described impeller gas compressor 1 with reference to the present embodiment to embodiment 3, and the sender property outlet of each described turbo-power mechanism 2 all is communicated with the working medium entrance of described attached turbo-power mechanism 3, and the working medium entrance of each described impeller gas compressor 1 all is communicated with the sender property outlet of described attached impeller gas compressor 4.
low-temperature receiver work doing impeller heat engine as shown in Figure 5 comprises impeller gas compressor 1, turbo-power mechanism 2, attached turbo-power mechanism 3, attached impeller gas compressor 4, external combustion heater 5, cooler 6 and reciprocal communicating passage 11, the sender property outlet of described impeller gas compressor 1 is communicated with the working medium entrance of described turbo-power mechanism 2, the sender property outlet of described attached turbo-power mechanism 3 is communicated with the working medium entrance of described attached impeller gas compressor 4, the sender property outlet of the working medium entrance of described impeller gas compressor 1 and described turbo-power mechanism 2 is communicated with an end of described reciprocal communicating passage 11 through timing control valve 12 respectively, the working medium entrance of described attached turbo-power mechanism 3 and the sender property outlet of described attached impeller gas compressor 4 are communicated with through the other end of timing control valve 12 with described reciprocal communicating passage 11 respectively, formation working medium closed-loop path, described external combustion heater 5 is arranged on communicating passage between the working medium entrance of the sender property outlet of described impeller gas compressor 1 and described turbo-power mechanism 2, described cooler 6 is arranged on communicating passage between the working medium entrance of the sender property outlet of described attached turbo-power mechanism 3 and described attached impeller gas compressor 4, on described reciprocal communicating passage 11, material filling type regenerator 8 is set, in the present embodiment, described impeller gas compressor 1 and the 2 coaxial settings of described turbo-power mechanism, described attached turbo-power mechanism 3 and the coaxial setting of described attached impeller gas compressor 4.
As mode of execution that can conversion, described material filling type regenerator 8 can not established.
low-temperature receiver work doing impeller heat engine as shown in Figure 6 comprises impeller gas compressor 1, turbo-power mechanism 2, attached turbo-power mechanism 3, attached impeller gas compressor 4, internal combustion firing chamber 9, cooler 6 and reciprocal communicating passage 11, the sender property outlet of described impeller gas compressor 1 is communicated with the working medium entrance of described turbo-power mechanism 2, the sender property outlet of described attached turbo-power mechanism 3 is communicated with the working medium entrance of described attached impeller gas compressor 4, the sender property outlet of the working medium entrance of described impeller gas compressor 1 and described turbo-power mechanism 2 is communicated with an end of described reciprocal communicating passage 11 through timing control valve 12 respectively, the working medium entrance of described attached turbo-power mechanism 3 and the sender property outlet of described attached impeller gas compressor 4 are communicated with through the other end of timing control valve 12 with described reciprocal communicating passage 11 respectively, formation working medium closed-loop path, described internal combustion firing chamber 9 is arranged in communicating passage between the working medium entrance of the sender property outlet of described impeller gas compressor 1 and described turbo-power mechanism 2, described cooler 6 is arranged on communicating passage between the working medium entrance of the sender property outlet of described attached turbo-power mechanism 3 and described attached impeller gas compressor 4, on described working medium closed-loop path, working medium export mouth 10 is set, on described reciprocal communicating passage 11, material filling type regenerator 8 is set, in the present embodiment, described impeller gas compressor 1 and the 2 coaxial settings of described turbo-power mechanism, described attached turbo-power mechanism 3 and the coaxial setting of described attached impeller gas compressor 4,10 places arrange control valve 13 at described working medium export mouth.
As mode of execution that can conversion, described material filling type regenerator 8 and described control valve 13 can be if do not select a setting.
As disposable mode of execution, above-described embodiment 1 can change the set-up mode of described impeller gas compressor 1, described turbo-power mechanism 2, described attached turbo-power mechanism 3 and the axle of described attached impeller gas compressor 4 four: can make four coaxial settings to embodiment 6; Or appoint three coaxial settings selecting among four; Or make all independently settings of axle of four, namely four is not all coaxial; Can also still adopt coaxial in twos mode, just change coaxial structure, for example make described impeller gas compressor 1 and the 3 coaxial settings of described attached turbo-power mechanism, described turbo-power mechanism 2 and the coaxial setting of described attached impeller gas compressor 4.
Obviously, the invention is not restricted to above embodiment, according to known technology and the technological scheme disclosed in this invention of related domain, can derive or association goes out many flexible programs, all these flexible programs also should be thought protection scope of the present invention.
Claims (8)
1. a low-temperature receiver work doing impeller heat engine, is characterized in that: comprise impeller gas compressor (1), turbo-power mechanism (2), attached turbo-power mechanism (3), attached impeller gas compressor (4), external combustion heater (5) and cooler (6); Described impeller gas compressor (1), described turbo-power mechanism (2), described attached turbo-power mechanism (3) and described attached impeller gas compressor (4) are interconnected successively and form the working medium closed-loop path; Described external combustion heater (5) is arranged on communicating passage between the working medium entrance of the sender property outlet of described impeller gas compressor (1) and described turbo-power mechanism (2); Described cooler (6) is arranged on communicating passage between the working medium entrance of the sender property outlet of described attached turbo-power mechanism (3) and described attached impeller gas compressor (4).
2. a low-temperature receiver work doing impeller heat engine, is characterized in that: comprise impeller gas compressor (1), turbo-power mechanism (2), attached turbo-power mechanism (3), attached impeller gas compressor (4), internal combustion firing chamber (9) and cooler (6); Described impeller gas compressor (1), described turbo-power mechanism (2), described attached turbo-power mechanism (3) and described attached impeller gas compressor (4) are interconnected successively and form the working medium closed-loop path; Described internal combustion firing chamber (9) is arranged in communicating passage between the working medium entrance of the sender property outlet of described impeller gas compressor (1) and described turbo-power mechanism (2); Described cooler (6) is arranged on communicating passage between the working medium entrance of the sender property outlet of described attached turbo-power mechanism (3) and described attached impeller gas compressor (4); On described working medium closed-loop path, working medium export mouth (10) is set.
3. a low-temperature receiver work doing impeller heat engine, is characterized in that: comprise impeller gas compressor (1), turbo-power mechanism (2), attached turbo-power mechanism (3), attached impeller gas compressor (4), external combustion heater (5), cooler (6) and reciprocal communicating passage (11), the sender property outlet of described impeller gas compressor (1) is communicated with the working medium entrance of described turbo-power mechanism (2), the sender property outlet of described attached turbo-power mechanism (3) is communicated with the working medium entrance of described attached impeller gas compressor (4), the sender property outlet of the working medium entrance of described impeller gas compressor (1) and described turbo-power mechanism (2) is communicated with through the end of timing control valve (12) with described reciprocal communicating passage (11) respectively, the sender property outlet of the working medium entrance of described attached turbo-power mechanism (3) and described attached impeller gas compressor (4) is communicated with through the other end of timing control valve (12) with described reciprocal communicating passage (11) respectively, formation working medium closed-loop path, described external combustion heater (5) is arranged on communicating passage between the working medium entrance of the sender property outlet of described impeller gas compressor (1) and described turbo-power mechanism (2), described cooler (6) is arranged on communicating passage between the working medium entrance of the sender property outlet of described attached turbo-power mechanism (3) and described attached impeller gas compressor (4).
4. a low-temperature receiver work doing impeller heat engine, is characterized in that: comprise impeller gas compressor (1), turbo-power mechanism (2), attached turbo-power mechanism (3), attached impeller gas compressor (4), internal combustion firing chamber (9), cooler (6) and reciprocal communicating passage (11), the sender property outlet of described impeller gas compressor (1) is communicated with the working medium entrance of described turbo-power mechanism (2), the sender property outlet of described attached turbo-power mechanism (3) is communicated with the working medium entrance of described attached impeller gas compressor (4), the sender property outlet of the working medium entrance of described impeller gas compressor (1) and described turbo-power mechanism (2) is communicated with through the end of timing control valve (12) with described reciprocal communicating passage (11) respectively, the sender property outlet of the working medium entrance of described attached turbo-power mechanism (3) and described attached impeller gas compressor (4) is communicated with through the other end of timing control valve (12) with described reciprocal communicating passage (11) respectively, formation working medium closed-loop path, described internal combustion firing chamber (9) is arranged in communicating passage between the working medium entrance of the sender property outlet of described impeller gas compressor (1) and described turbo-power mechanism (2), described cooler (6) is arranged on communicating passage between the working medium entrance of the sender property outlet of described attached turbo-power mechanism (3) and described attached impeller gas compressor (4), on described working medium closed-loop path, working medium export mouth (10) is set.
5. according to claim 1,2,3 or 4 described low-temperature receiver work doing impeller heat engines, it is characterized in that: the coaxial setting more than two in described impeller gas compressor (1), described turbo-power mechanism (2), described attached turbo-power mechanism (3) and described attached impeller gas compressor (4).
6. described low-temperature receiver work doing impeller heat engine according to claim 1 and 2, it is characterized in that: described low-temperature receiver work doing impeller heat engine also comprises heat exchanger type regenerator (7), the sender property outlet of described turbo-power mechanism (2) is communicated with the working medium entrance of described attached turbo-power mechanism (3) through the fluid passage that is cooled of described heat exchanger type regenerator (7), and the sender property outlet of described attached impeller gas compressor (4) is communicated with the working medium entrance of described impeller gas compressor (1) through the fluid passage that is heated of described heat exchanger type regenerator (7).
7. according to claim 3 or 4 described low-temperature receiver work doing impeller heat engines, is characterized in that: material filling type regenerator (8) is set on described reciprocal communicating passage (11).
8. according to claim 3 or 4 described low-temperature receiver work doing impeller heat engines, is characterized in that: locate to arrange control valve (13) at described working medium export mouth (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013100695487A CN103174517A (en) | 2012-03-26 | 2013-03-05 | Cold-source-acting impeller Stirling hot-air engine |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201210082813.0 | 2012-03-26 | ||
| CN201210082813 | 2012-03-26 | ||
| CN2013100695487A CN103174517A (en) | 2012-03-26 | 2013-03-05 | Cold-source-acting impeller Stirling hot-air engine |
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| CN103174517A true CN103174517A (en) | 2013-06-26 |
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| CN2013100695487A Pending CN103174517A (en) | 2012-03-26 | 2013-03-05 | Cold-source-acting impeller Stirling hot-air engine |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104265455A (en) * | 2013-09-22 | 2015-01-07 | 摩尔动力(北京)技术股份有限公司 | Cold source working impeller air heating machine |
| CN104389693A (en) * | 2013-09-22 | 2015-03-04 | 摩尔动力(北京)技术股份有限公司 | Single-runner rotor engine |
| CN106801621A (en) * | 2015-11-25 | 2017-06-06 | 熵零股份有限公司 | A kind of Contra-rotating rotor mechanism |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0353374A1 (en) * | 1988-07-25 | 1990-02-07 | Abb Stal Ab | Gas turbine unit for combined production of electricity and heat and method for operating such unit |
| JPH05164888A (en) * | 1991-12-13 | 1993-06-29 | Mitsubishi Heavy Ind Ltd | Gas turbine power generating set |
| JPH0610703A (en) * | 1992-05-14 | 1994-01-18 | General Electric Co <Ge> | Gas turbine prime mover and method of increasing output from gas turbine prime mover |
| US20060012406A1 (en) * | 2004-07-15 | 2006-01-19 | Huber Carol A | Output buffer with selectable slew rate |
| CN201002715Y (en) * | 2006-12-14 | 2008-01-09 | 上海交通大学 | Gas turbine Stirling engine electric propulsion device for large-scale vessels high speed sailing |
| CN101988443A (en) * | 2010-10-27 | 2011-03-23 | 靳北彪 | Non-conjugated zero-distance high-low temperature heat source thermomotor |
| CN102086823A (en) * | 2010-08-27 | 2011-06-08 | 靳北彪 | Small temperature-rise low-entropy mixing combustion engine |
| CN102287397A (en) * | 2011-06-02 | 2011-12-21 | 关松生 | Pump with vanes capable of turning |
-
2013
- 2013-03-05 CN CN2013100695487A patent/CN103174517A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0353374A1 (en) * | 1988-07-25 | 1990-02-07 | Abb Stal Ab | Gas turbine unit for combined production of electricity and heat and method for operating such unit |
| JPH05164888A (en) * | 1991-12-13 | 1993-06-29 | Mitsubishi Heavy Ind Ltd | Gas turbine power generating set |
| JPH0610703A (en) * | 1992-05-14 | 1994-01-18 | General Electric Co <Ge> | Gas turbine prime mover and method of increasing output from gas turbine prime mover |
| US20060012406A1 (en) * | 2004-07-15 | 2006-01-19 | Huber Carol A | Output buffer with selectable slew rate |
| CN201002715Y (en) * | 2006-12-14 | 2008-01-09 | 上海交通大学 | Gas turbine Stirling engine electric propulsion device for large-scale vessels high speed sailing |
| CN102086823A (en) * | 2010-08-27 | 2011-06-08 | 靳北彪 | Small temperature-rise low-entropy mixing combustion engine |
| CN101988443A (en) * | 2010-10-27 | 2011-03-23 | 靳北彪 | Non-conjugated zero-distance high-low temperature heat source thermomotor |
| CN102287397A (en) * | 2011-06-02 | 2011-12-21 | 关松生 | Pump with vanes capable of turning |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104265455A (en) * | 2013-09-22 | 2015-01-07 | 摩尔动力(北京)技术股份有限公司 | Cold source working impeller air heating machine |
| CN104389693A (en) * | 2013-09-22 | 2015-03-04 | 摩尔动力(北京)技术股份有限公司 | Single-runner rotor engine |
| CN106801621A (en) * | 2015-11-25 | 2017-06-06 | 熵零股份有限公司 | A kind of Contra-rotating rotor mechanism |
| CN106801621B (en) * | 2015-11-25 | 2019-08-20 | 熵零股份有限公司 | A kind of Contra-rotating rotor mechanism |
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Application publication date: 20130626 |