CN104265505B - Revolution runner engine - Google Patents
Revolution runner engine Download PDFInfo
- Publication number
- CN104265505B CN104265505B CN201410466978.7A CN201410466978A CN104265505B CN 104265505 B CN104265505 B CN 104265505B CN 201410466978 A CN201410466978 A CN 201410466978A CN 104265505 B CN104265505 B CN 104265505B
- Authority
- CN
- China
- Prior art keywords
- runner
- combustion chamber
- engine
- revolution
- cooler
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 238000002485 combustion reaction Methods 0.000 claims abstract description 51
- 230000001914 calming effect Effects 0.000 claims abstract description 15
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 claims description 48
- 238000009833 condensation Methods 0.000 claims description 43
- 230000005494 condensation Effects 0.000 claims description 43
- 239000007789 gas Substances 0.000 claims description 36
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 claims description 34
- 229910002092 carbon dioxide Inorganic materials 0.000 claims description 21
- 239000001569 carbon dioxide Substances 0.000 claims description 21
- 239000011261 inert gas Substances 0.000 claims description 16
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 15
- 230000006835 compression Effects 0.000 claims description 11
- 238000007906 compression Methods 0.000 claims description 11
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims description 8
- 239000012809 cooling fluid Substances 0.000 claims description 7
- 238000001816 cooling Methods 0.000 claims description 6
- 239000007787 solid Substances 0.000 claims description 6
- 239000000203 mixture Substances 0.000 claims description 5
- 229910052786 argon Inorganic materials 0.000 claims description 4
- 229910052734 helium Inorganic materials 0.000 claims description 4
- 239000001307 helium Substances 0.000 claims description 4
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims description 4
- 229910052743 krypton Inorganic materials 0.000 claims description 4
- DNNSSWSSYDEUBZ-UHFFFAOYSA-N krypton atom Chemical compound [Kr] DNNSSWSSYDEUBZ-UHFFFAOYSA-N 0.000 claims description 4
- 229910052754 neon Inorganic materials 0.000 claims description 4
- GKAOGPIIYCISHV-UHFFFAOYSA-N neon atom Chemical compound [Ne] GKAOGPIIYCISHV-UHFFFAOYSA-N 0.000 claims description 4
- 229910052724 xenon Inorganic materials 0.000 claims description 4
- FHNFHKCVQCLJFQ-UHFFFAOYSA-N xenon atom Chemical compound [Xe] FHNFHKCVQCLJFQ-UHFFFAOYSA-N 0.000 claims description 4
- 238000004519 manufacturing process Methods 0.000 abstract description 2
- 239000012530 fluid Substances 0.000 description 8
- 239000000446 fuel Substances 0.000 description 5
- 229910052756 noble gas Inorganic materials 0.000 description 4
- 238000006243 chemical reaction Methods 0.000 description 2
- 238000004891 communication Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000002156 mixing Methods 0.000 description 2
- 238000000053 physical method Methods 0.000 description 2
- GCNLQHANGFOQKY-UHFFFAOYSA-N [C+4].[O-2].[O-2].[Ti+4] Chemical compound [C+4].[O-2].[O-2].[Ti+4] GCNLQHANGFOQKY-UHFFFAOYSA-N 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000003344 environmental pollutant Substances 0.000 description 1
- 230000008520 organization Effects 0.000 description 1
- 239000007800 oxidant agent Substances 0.000 description 1
- 231100000719 pollutant Toxicity 0.000 description 1
- 238000005057 refrigeration Methods 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Landscapes
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
The invention discloses a kind of revolution runner engine, including runner of calming the anger, combustion chamber, jet pipe and rotary body, described calm the anger runner and described combustion chamber is arranged on described rotary body, described jet pipe has square to be arranged on described rotary body, described runner and the described combustion chamber of calming the anger, described combustion chamber connects with described jet pipe, and the bearing capacity of described combustion chamber is more than 3MPa, and described rotary body externally exports power.Revolution runner engine structure disclosed in this invention is simple, low cost of manufacture, and moving component is few, and efficiency is high.
Description
Technical field
The present invention relates to heat energy and dynamic field, especially a kind of revolution runner engine.
Background technology
The efficiency of conventional piston formula internal combustion engine and the conversion of gas turbine hot merit is low, disposal of pollutants is serious.Therefore,
Need a kind of new work engine of invention.
Summary of the invention
In order to solve the problems referred to above, the technical scheme that the present invention proposes is as follows:
Scheme 1, a kind of revolution runner engine, including runner of calming the anger, combustion chamber, jet pipe and rotary body,
Described calming the anger runner and described combustion chamber is arranged on described rotary body, described jet pipe and described rotary body have square
Arrange, described in calm the anger runner and described combustion chamber, described combustion chamber connects with described jet pipe, described combustion
The bearing capacity burning room is more than 3MPa, and described rotary body externally exports power.
Scheme 2, on the basis of scheme 1, described revolution runner engine also includes turbine, described jet pipe
The working medium ejected acts on described turbine and promotes described turbine to rotate.
Scheme 3, on the basis of scheme 1, described jet pipe is set to Laval nozzle.
Scheme 4, on the basis of scheme 1, described jet pipe is set to tapered jet pipe.
Scheme 5, on the basis of scheme 1, sets fuel flow channel on described rotary body, described combustion chamber with
Described fuel flow channel connects.
Scheme 6, on the basis of scheme 1, described revolution runner engine also includes liquid oxygen source, described liquid
Oxygen source and described combustion chamber, described in calm the anger the gas access of runner and the row of described revolution runner engine
Gas port connects through communicating passage, sets condensate cooler, described revolution runner engine in described communicating passage
Cycle fluid more than 50 percent be set to inert gas.
Scheme 7, on the basis of scheme 6, the gas at described condensate cooler and described runner of calming the anger enters
Deep condensation cooler is set in described communicating passage between Kou.
Scheme 8, on the basis of scheme 6, sets condensation-water drain on described condensate cooler.
Scheme 9, on the basis of scheme 6, sets carbon dioxide condensation outlet on described condensate cooler.
Scheme 10, on the basis of scheme 6, sets solid water outlet on described condensate cooler.
Scheme 11, on the basis of scheme 6, sets drikold outlet on described condensate cooler.
Scheme 12, on the basis of scheme 7, sets condensation-water drain on described deep condensation cooler.
Scheme 13, on the basis of scheme 7, sets carbon dioxide condensation on described deep condensation cooler and goes out
Mouthful.
Scheme 14, on the basis of scheme 7, sets solid water outlet on described deep condensation cooler.
Scheme 15, on the basis of scheme 7, sets drikold on described deep condensation cooler and goes out
Mouthful.
Scheme 16, on the basis of scheme 6, described liquid oxygen source leads to through the cooling fluid of described condensate cooler
Road and described combustion chamber.
Scheme 17, on the basis of scheme 6, described condensate cooler is set to hybrid condensate cooler, institute
Stating liquid oxygen source to connect with the cooling fluid inlet of described hybrid condensate cooler, described liquid oxygen source is through described mixed
Box-like condensate cooler and described combustion chamber.
Scheme 18, on the basis of scheme 7, described liquid oxygen source is through the cooling stream of described deep condensation cooler
Body passage and described combustion chamber.
Scheme 19, on the basis of scheme 7, it is cold that described deep condensation cooler is set to hybrid deep condensation
But device, described liquid oxygen source connects with the cooling fluid inlet of described hybrid deep condensation cooler, described liquid
Oxygen source is through described hybrid deep condensation cooler and described combustion chamber.
Scheme 20, on the basis of scheme 1, described revolution runner engine also includes gas compression unit,
The compressed gas outlet of described gas compression unit connects with the gas access of described runner of calming the anger.
Scheme 21, on the basis of scheme 6, described revolution runner engine also includes gas compression unit,
Described gas compression unit is arranged in described communicating passage.
Scheme 22, on the basis of scheme 6, described revolution runner engine also includes carbon dioxide capture list
The inner space of unit, described carbon dioxide capture unit and working medium envelope.
Scheme 23, on the basis of scheme 6, described inert gas be set to helium, neon, argon gas, Krypton,
Xenon or be set to be mixed, by two or more inert gases, the noble gas mixtures that constitutes.
Scheme 24, on the basis of scheme 1 or 6, described combustion chamber is set to combustion chamber during anon-normal.
In the present invention, so-called " runner of calming the anger " refers to fluid passage when rotating with function of calming the anger.
In the present invention, the power pressure of described combustion chamber matches with its bearing capacity, in the most described combustion chamber
The highest power pressure reach its bearing capacity.
In the present invention, so-called " inert gas " includes elemental inert gas and noble gas mixtures.
In the present invention, so-called " molecular weight of inert gas " refers to mean molecule quantity.
In the present invention, so-called " liquid oxygen source " refers to provide the system of liquid oxygen, unit or storage tank.
In the present invention, so-called " liquid oxygen source " refers to the purest liquid oxygen source, also include containing
Liquid oxygen content is not the oxidizer source of absolutely gas.
In the present invention, so-called " condensate cooler " refers to the condensate cooler making water that condensation to occur,
Or can make water and carbon dioxide that the condensate cooler of condensation occurs.
In the present invention, so-called " deep condensation cooler " refers to than heretofore described condensate cooler
The condensate cooler that condensation chilling temperature is lower, described deep condensation cooler can make carbon dioxide further
There is liquefaction or solidification.
In the present invention, so-called " hybrid condensate cooler " refers to that cooling down fluid mixes with cooled fluid
Container.
In the present invention, so-called " hybrid deep condensation cooler " refers to cool down fluid and cooled fluid
The container of mixing.
In the present invention, so-called " working medium envelope " refers to the set of the wall in the space that working medium can arrive, such as:
By the wall in the space accommodating gas working medium in described combustion chamber, or turbine accommodates the space of gas working medium
Wall.
In the present invention, so-called " inner chamber of working medium envelope " refers to the collection of the wall in the space that working medium can arrive
The inner chamber being encircled into.
In the present invention, so-called " carbon dioxide capture unit " refers to isolate carbon dioxide from working medium
The unit come, catches carbon dioxide including using chemical method and/or catches carbon dioxide with physical method
Device, also includes the refrigeration separative element that can separate carbon dioxide, so-called physical method include absorb and
Absorption.
In the present invention, when gas access and the exhaust outlet warp of described revolution runner engine of described runner of calming the anger
When communicating passage connection forms loop, so-called described liquid oxygen source and described combustion chamber refer to described liquid oxygen
Source and described circuit communication, such as, described liquid oxygen source directly with described combustion chamber, or described liquid oxygen source
Connect with the miscellaneous part beyond combustion chamber described in loop or the communicating passage in parts.
In the present invention, so-called " described jet pipe and described rotary body have square to arrange " refers to when described jet pipe sprays
Suffered reaction force produces the set-up mode of moment of torsion to the rotation of described rotary body.
In the present invention, so-called " combustion chamber during anon-normal " refers to that burn time duration exceedes working medium experience engine one
The combustion chamber of duration needed for individual working cycles.
In the present invention, so-called A and B connection refers to that between A and B, working medium flows, and flows to B including working medium from A
Or flow to A from B, or working medium elder generation flows to B from A and flows to A from B again.So-called " connection " includes directly connecting
Logical, indirect communication connects with through operating unit, and described operating unit includes valve, controlling organization, feed mechanism
(pump) and heat exchanger etc..
In the present invention, according to the known technology of heat energy Yu dynamic field, necessity should be set in necessary place
Parts, unit or system etc..
Beneficial effects of the present invention is as follows:
Revolution runner engine structure disclosed in this invention is simple, low cost of manufacture, and moving component is few, effect
Rate is high.
Accompanying drawing explanation
Shown in Fig. 1 is the structural representation of the embodiment of the present invention 1；
Shown in Fig. 2 is the structural representation of the embodiment of the present invention 2；
Shown in Fig. 3 is the structural representation of the embodiment of the present invention 3；
Shown in Fig. 4 is the structural representation of the embodiment of the present invention 3；
Shown in Fig. 5 is the structural representation of the embodiment of the present invention 4；
Shown in Fig. 6 is the structural representation of the embodiment of the present invention 5；
Shown in Fig. 7 is the structural representation of the embodiment of the present invention 6；
Shown in Fig. 8 is the structural representation of the embodiment of the present invention 7；
Shown in Fig. 9 is the structural representation of the embodiment of the present invention 9；
Shown in Figure 10 is the structural representation of the embodiment of the present invention 9；
Shown in Figure 11 is the structural representation of the embodiment of the present invention 11；
Shown in Figure 12 is the structural representation of the embodiment of the present invention 12；
Shown in Figure 13 is the structural representation of the embodiment of the present invention 13；
In figure:
1 calms the anger runner, 101 gas compression unit, 2 combustion chambers, 20 liquid oxygen sources, 3 jet pipes, 31 Bearing scores
Your jet pipe, 32 tapered jet pipes, 4 rotary bodies, 5 turbines, 6 fuel flow channels, 7 communicating passage, 8 condensations are cold
But device, 801 hybrid condensate coolers, 9 deep condensation coolers, 10 condensation-water drains, 11 titanium dioxide
Carbon capture unit.
Detailed description of the invention
Embodiment 1
As it is shown in figure 1, a kind of revolution runner engine, including runner 1 of calming the anger, combustion chamber 2, jet pipe 3
With rotary body 4, it is characterised in that calm the anger runner 1 described in: and described combustion chamber 2 is arranged on described rotary body
On 4, described jet pipe 3 and described rotary body 4 have square to arrange, described in calm the anger runner 1 and described combustion chamber 2
Connection, described combustion chamber 2 connects with described jet pipe 3, and the bearing capacity of described combustion chamber 2 is more than 3MPa,
Described rotary body 4 externally exports power.
Embodiment 2
As in figure 2 it is shown, a kind of revolution runner engine, it is on the basis of embodiment 1, described revolution stream
Road engine also includes that turbine 5, the working medium that described jet pipe 3 ejects act on described turbine 5 and promote described
Turbine 5 rotates.
In the present invention, all embodiments in the specific implementation, all can make described revolution according to the present embodiment
Runner engine also includes that turbine, the working medium that described jet pipe ejects act on described turbine and promote described turbine
Rotate.
Embodiment 3
As it is shown on figure 3, a kind of revolution runner engine, it is on the basis of embodiment 1, described jet pipe 3
It is set to Laval nozzle 31；
Convertiblely, as shown in Figure 4, described jet pipe 3 is set to tapered jet pipe 32.
Embodiment 4
As it is shown in figure 5, a kind of revolution runner engine, it is on the basis of embodiment 1, in described rotation
Setting fuel flow channel 6 on body 4, described combustion chamber 2 connects with described fuel flow channel 6.
Embodiment 5
As shown in Figure 6, a kind of revolution runner engine, it is on the basis of embodiment 1, described revolution stream
Road engine also includes that liquid oxygen source 20, described liquid oxygen source 20 connect with described combustion chamber 2, described pressure gas stream
The gas access in road 1 connects through communicating passage 7, in described company with the exhaust outlet of described revolution runner engine
Set condensate cooler 8 in circulation passage 7,50 the percent of the cycle fluid of described revolution runner engine with
On be set to inert gas.
In the present embodiment, be selectively chosen, described inert gas is set to helium, neon, argon gas,
Krypton, xenon or be set to be mixed, by two or more inert gases, the noble gas mixtures that constitutes.Preferably,
The molecular weight of the described inert gas being filled with in described loop is more than 20.
In the present embodiment, more than 50 the percent of the cycle fluid of described revolution runner engine is set to inertia
Gas, the adiabatic exponent of inert gas is relatively big, is compressed by same volume ratio or is expanded, and its temperature ratio is big,
In this sense, under conditions of a constant temperature ratio, there is the advantage that summation watt rating is high.
Embodiment 6
As it is shown in fig. 7, a kind of revolution runner engine, it is on the basis of embodiment 5, in described condensation
Deep condensation is set cold in described communicating passage 7 between the gas access of cooler 8 and described runner 1 of calming the anger
But device 9.
Embodiment 7
As shown in Figure 8, a kind of revolution runner engine, it is on the basis of embodiment 5, in described condensation
Condensation-water drain 10 is set on cooler；
Selectively, described condensate cooler sets solid water outlet；
Selectively, described condensate cooler sets carbon dioxide condensation outlet；
Selectively, described condensate cooler sets drikold outlet.
Embodiment 8
A kind of revolution runner engine, it is on the basis of embodiment 6, on described deep condensation cooler
If condensation-water drain；
Selectively, described deep condensation cooler sets carbon dioxide condensation outlet；
Selectively, described deep condensation cooler sets solid water outlet；
Selectively, described deep condensation cooler sets drikold outlet.
Embodiment 9
As it is shown in figure 9, a kind of revolution runner engine, it is on the basis of embodiment 5, described liquid oxygen source
20 connect with described combustion chamber 2 through the cooling channels of described condensate cooler 8.
Convertiblely, as shown in Figure 10, described condensate cooler 8 is set to hybrid condensate cooler 801,
Described liquid oxygen source 20 connects with the cooling fluid inlet of described hybrid condensate cooler 801, described liquid oxygen
Source 20 connects with described combustion chamber 2 through described hybrid condensate cooler 801.
Embodiment 10
A kind of revolution runner engine, it is on the basis of embodiment 6, described liquid oxygen source 20 through described deeply
The cooling channels of degree condensate cooler 9 connects with described combustion chamber 2.
Convertiblely, described deep condensation cooler 9 is set to hybrid deep condensation cooler, described liquid oxygen
Source 20 connects with the cooling fluid inlet of described hybrid deep condensation cooler, and described liquid oxygen source 20 is through institute
State hybrid deep condensation cooler to connect with described combustion chamber 2.
Embodiment 11
As shown in figure 11, a kind of revolution runner engine, it is on the basis of embodiment 1, described revolution
Runner engine also includes gas compression unit 101, the compressed gas outlet of described gas compression unit 101
Connect with the described gas access calming the anger runner 1.
Embodiment 12
As shown in figure 12, a kind of revolution runner engine, it is on the basis of embodiment 5, described revolution
Runner engine also includes that gas compression unit 101, described gas compression unit 101 are arranged on described connection
On passage 7.
Embodiment 13
As shown in figure 13, a kind of revolution runner engine, it is on the basis of embodiment 5, described revolution
Runner engine also includes carbon dioxide capture unit 11, described carbon dioxide capture unit 11 and working medium bag
The inner space of network.
In the present invention, all described in calm the anger the gas access of runner and the exhaust outlet of described revolution runner engine
Through communicating passage connection embodiment in the specific implementation, all can optionally select, described revolution stream
Road engine also includes the inner chamber of carbon dioxide capture unit, described carbon dioxide capture unit and working medium envelope
Connection；The molecular weight of described inert gas is the most selectively set more than 20；The most selectively arrange described lazy
Property gas is set to helium, neon, argon gas, Krypton, xenon or is set to by two or more inert gas mixing structures
The noble gas mixtures become.
It is clear that the invention is not restricted to above example, according to techniques known and presently disclosed
Technical scheme, can derive or association goes out many flexible programs, all these flexible programs, also should recognize
For being protection scope of the present invention.
Claims (18)
1. revolution a runner engine, including runner of calming the anger (1), combustion chamber (2), jet pipe (3) and
Rotary body (4), described in calm the anger runner (1) and described combustion chamber (2) are arranged on described rotary body (4)
On, described jet pipe (3) and described rotary body (4) have square to arrange, described in calm the anger runner (1) with described
Combustion chamber (2) connects, and described combustion chamber (2) connect with described jet pipe (3), described rotary body (4)
Externally export power, it is characterised in that: the bearing capacity of described combustion chamber (2) is more than 3MPa, described public affairs
Turn of tidal stream road engine also includes that liquid oxygen source (20), described liquid oxygen source (20) connect with described combustion chamber (2),
The exhaust outlet of the gas access of described runner of calming the anger (1) and described revolution runner engine is through communicating passage (7)
Connection, sets condensate cooler (8), following of described revolution runner engine in described communicating passage (7)
More than 50 the percent of ring working medium is set to inert gas.
2. revolve round the sun runner engine as claimed in claim 1, it is characterised in that: at described condensate cooler
(8) degree of depth is set in the described communicating passage (7) and between the gas access of described runner of calming the anger (1) cold
Solidifying cooler (9).
3. revolve round the sun runner engine as claimed in claim 1, it is characterised in that: at described condensate cooler
On set condensation-water drain (10).
4. revolve round the sun runner engine as claimed in claim 1, it is characterised in that: at described condensate cooler
On set carbon dioxide condensation outlet.
5. revolve round the sun runner engine as claimed in claim 1, it is characterised in that: on described condensate cooler
If solid water exports.
6. revolve round the sun runner engine as claimed in claim 1, it is characterised in that: at described condensate cooler
On set drikold outlet.
7. revolve round the sun runner engine as claimed in claim 2, it is characterised in that: cold at described deep condensation
But condensation-water drain is set on device.
8. revolve round the sun runner engine as claimed in claim 2, it is characterised in that: cold at described deep condensation
But carbon dioxide condensation outlet is set on device.
9. revolve round the sun runner engine as claimed in claim 2, it is characterised in that: cold at described deep condensation
But solid water outlet is set on device.
10. revolve round the sun runner engine as claimed in claim 2, it is characterised in that: cold at described deep condensation
But drikold outlet is set on device.
11. revolution runner engines as claimed in claim 1, it is characterised in that: described liquid oxygen source (20)
Connect with described combustion chamber (2) through the cooling channels of described condensate cooler (8).
12. revolution runner engines as claimed in claim 1, it is characterised in that: described condensate cooler (8)
It is set to hybrid condensate cooler (801), described liquid oxygen source (20) and described hybrid condensate cooler (801)
Cooling fluid inlet connection, described liquid oxygen source (20) through described hybrid condensate cooler (801) with
Described combustion chamber (2) connects.
13. revolution runner engines as claimed in claim 2, it is characterised in that: described liquid oxygen source (20)
Connect with described combustion chamber (2) through the cooling channels of described deep condensation cooler (9).
14. revolution runner engines as claimed in claim 2, it is characterised in that: described deep condensation cools down
Device (9) is set to hybrid deep condensation cooler, and described liquid oxygen source (20) is cold with the described hybrid degree of depth
The cooling fluid inlet connection of solidifying cooler, described liquid oxygen source (20) cools down through described hybrid deep condensation
Device connects with described combustion chamber (2).
15. revolution runner engines as claimed in claim 1, it is characterised in that: described revolution runner starts
Machine also includes that gas compression unit (101), described gas compression unit (101) are arranged on described connection and lead to
On road (7).
16. revolution runner engines as claimed in claim 1, it is characterised in that: described revolution runner starts
Machine also includes the inner space of carbon dioxide capture unit, described carbon dioxide capture unit and working medium envelope.
17. revolution runner engines as claimed in claim 1, it is characterised in that: described inert gas is set to
Helium, neon, argon gas, Krypton, xenon or be set to be mixed, by two or more inert gases, the indifferent gas that constitutes
Body mixture.
18. revolution runner engines as claimed in claim 1, it is characterised in that: described combustion chamber (2)
It is set to combustion chamber during anon-normal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410466978.7A CN104265505B (en) | 2013-09-13 | 2014-09-13 | Revolution runner engine |
Applications Claiming Priority (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310417308.1 | 2013-09-13 | ||
| CN2013104173081 | 2013-09-13 | ||
| CN201310417308 | 2013-09-13 | ||
| CN201410466978.7A CN104265505B (en) | 2013-09-13 | 2014-09-13 | Revolution runner engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104265505A CN104265505A (en) | 2015-01-07 |
| CN104265505B true CN104265505B (en) | 2016-08-24 |
Family
ID=52157062
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410466978.7A Active CN104265505B (en) | 2013-09-13 | 2014-09-13 | Revolution runner engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104265505B (en) |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6981366B2 (en) * | 2003-05-01 | 2006-01-03 | Sharpe Thomas H | Turbineless jet engine |
| CN201635863U (en) * | 2009-05-14 | 2010-11-17 | 靳北彪 | low entropy co-combustion engine |
| WO2012003706A1 (en) * | 2010-07-07 | 2012-01-12 | Jin Beibiao | Supersonic rotor engine |
| CN102588144A (en) * | 2011-07-19 | 2012-07-18 | 陈久斌 | Flywheel turbine |
| CN103133178B (en) * | 2011-12-01 | 2015-08-19 | 摩尔动力(北京)技术股份有限公司 | Twin channel entropy cycle engine |
| CN103075233B (en) * | 2012-01-04 | 2017-02-15 | 摩尔动力(北京)技术股份有限公司 | Low-temperature air intake method for internal combustion engine and engine |
| CN203257540U (en) * | 2013-01-17 | 2013-10-30 | 摩尔动力(北京)技术股份有限公司 | Oxygen-containing gas liquefied product engine |
-
2014
- 2014-09-13 CN CN201410466978.7A patent/CN104265505B/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN104265505A (en) | 2015-01-07 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN107100736B (en) | Combined Gas Turbine System | |
| JP3504946B2 (en) | Heat recovery device | |
| KR100303550B1 (en) | Thermal regeneration device | |
| CN108868930A (en) | Overcritical/critical-cross carbon dioxide association circulating power generation system that afterheat of IC engine utilizes | |
| CN101761368A (en) | Low-grade heat flow prime motor, power generating system and method thereof | |
| CN106661875A (en) | Devices, systems and methods for harnessing thermal energy | |
| CN201546768U (en) | A low-grade heat flow power generation system | |
| CN102032068A (en) | Efficient hot-air engine | |
| CN101988397A (en) | Low-grade heat-flow prime mover, generating system and method thereof | |
| CN101529055A (en) | A heat engine system | |
| CN107605554A (en) | Self-cooled thermal circulation method | |
| JP2018517096A (en) | Novel multi-loop gas turbine and method of operation thereof | |
| CN105114266B (en) | Power device using heat pump technology | |
| CN104373246A (en) | Gas-driving-closed piston type engine | |
| CN104265505B (en) | Revolution runner engine | |
| CN102213161B (en) | Closed gas cycle type thermal power system | |
| CN214464562U (en) | Mixture transcritical circulation solar photo-thermal power generation system | |
| CN212428968U (en) | Supercritical carbon dioxide Brayton cycle system | |
| CN102721033B (en) | Non-metallic energy oil steam generation method and generation device of no-pressure container | |
| CN104234864B (en) | Gas closed engine | |
| CN107476996A (en) | generating set | |
| Cai et al. | Thermodynamic analysis of a near-isothermal compressed air energy storage system based on internal combustion engine assistance | |
| CN120476247A (en) | Thermal energy storage system | |
| CN103775199B (en) | Hot-fluid balance internal-combustion engine UTILIZATION OF VESIDUAL HEAT IN system | |
| CN102900538B (en) | Double-working-medium combined cycle turbine annular combustion phase change chamber |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20200522 Address after: 215000 south of Lianyang road and east of Chang'an Road, Wujiang Economic and Technological Development Zone, Suzhou City, Jiangsu Province (Science and technology entrepreneurship Park) Patentee after: Wujiang science and Technology Pioneer Park Management Service Co., Ltd Address before: 100101, Beijing, Chaoyang District Beiyuan Road, No. 168, Sheng Sheng building, 24 floor Patentee before: MOLECULE POWER BEIJING TECH Co. |
|
| TR01 | Transfer of patent right |