CN103953442A - Fluid-channel rotary engine - Google Patents
Fluid-channel rotary engine Download PDFInfo
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- CN103953442A CN103953442A CN201410101573.3A CN201410101573A CN103953442A CN 103953442 A CN103953442 A CN 103953442A CN 201410101573 A CN201410101573 A CN 201410101573A CN 103953442 A CN103953442 A CN 103953442A
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- rotary engine
- injection channel
- fluid passage
- runner rotary
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Abstract
The invention discloses a fluid-channel rotary engine. The fluid-channel rotary engine comprises a rotor and a combustion chamber. A centrifugal fluid channel is arranged in the rotor. The combustion chamber is arranged in the rotor. The combustion chamber transfers heat to the centrifugal fluid channel. The centrifugal fluid channel is communicated with a working medium inlet of an injection channel. The injection channel and the rotor are arranged at an interval. The rotor outputs power outward. The fluid-channel rotary engine has the advantages of high power density, less pollutant discharge, good fuel diversity and low production cost.
Description
Technical field
The present invention relates to heat energy and power field, especially a kind of runner rotary engine.
Background technique
the energy and environmental problem become more and more important, and conventional engines specific power is low, disposal of pollutants serious, fuel diversity is poor, cost of production is high, therefore need to invent a kind of new work engine.
Summary of the invention
In order to address the above problem, the technological scheme that the present invention proposes is as follows:
Scheme 1: a kind of runner rotary engine, comprise rotor and firing chamber, centrifugal fluid passage is set in described rotor, described firing chamber is arranged in described rotor, conduct heat to described centrifugal fluid passage in described firing chamber, described centrifugal fluid passage is communicated with the working medium entrance of injection channel, and described injection channel and described rotor have square setting, the external outputting power of described rotor.
Scheme 2: on the basis of scheme 1, described runner rotary engine further comprises gas compressor and described rotor integrated setting described in gas compressor, the pressurized gas outlet of described gas compressor is communicated with described firing chamber.
Scheme 3: on the basis of scheme 1, described runner rotary engine further comprises attached injection channel, described attached injection channel and described rotor integrated setting, the gas after conducting heat from described firing chamber and to described centrifugal fluid passage enters described attached injection channel.
Scheme 4: on the basis of scheme 1, described runner rotary engine further comprises gas compressor and described rotor integrated setting described in gas compressor and attached injection channel, described attached injection channel and described rotor integrated setting, the pressurized gas outlet of described gas compressor is communicated with described firing chamber, gas after conducting heat from described firing chamber and to described centrifugal fluid passage enters described attached injection channel, and described fluid supply is communicated with described centrifugal fluid passage.
Scheme 5: on the basis of scheme 3 or scheme 4, further described attached injection channel is made as to turbine.
Scheme 6: on the basis of arbitrary scheme, further described rotor is made as to sleeve rotor in scheme 1 to 5.
Scheme 7: on the basis of scheme 6, further described firing chamber is arranged in the inner chamber of described sleeve rotor.
Scheme 8: on the basis of scheme 6 or 7, further described centrifugal fluid passage is made as to the pipeline in the inner chamber that is arranged on described sleeve rotor.
Scheme 9: on the basis of scheme 6 or 7, further in the inner chamber of described sleeve rotor, pipeline is set, described pipeline is communicated with described centrifugal fluid passage.
Scheme 10: on the basis of scheme 8 or 9, further described pipeline is made as to volute.
Scheme 11: on the basis of scheme 10, further described volute be made as to cylindricality volute or be made as dish type volute.
Scheme 12: in scheme 1 to 11 on the basis of arbitrary scheme, further in described rotor peripheral hardware stationary housings.
Scheme 13: on the basis of arbitrary scheme, described runner rotary engine further comprises fluid supply in scheme 1 to 12, described fluid supply is communicated with described centrifugal fluid passage through swivel joint.
Scheme 14: on the basis of scheme 13 schemes, further described swivel joint is made as to uniform internal diameter swivel joint, is made as along coning conversion adapter, is made as contrary coning conversion adapter or is made as disk rotary joint.
Scheme 15: on the basis of arbitrary scheme, described runner rotary engine further comprises fluid supply in scheme 1 to 12, described fluid supply is sent into mouth through liquid and is communicated with described centrifugal fluid passage.
Scheme 16: in scheme 1 to 12 on the basis of arbitrary scheme, described runner rotary engine further comprises fluid supply, on described rotor, establish rotor fluid passage, in described rotor fluid passage, establish and do not contact with described rotor fluid passage and send into pipe with the built-in liquid of described rotor coaxial line, described fluid supply is sent into pipe through described built-in liquid and is communicated with described rotor fluid passage, and described rotor fluid passage is communicated with described centrifugal fluid passage.
Scheme 17: on the basis of arbitrary scheme, described runner rotary engine further comprises fluid supply in scheme 1 to 12, described fluid supply is communicated with described centrifugal fluid passage through fluid drips entrance.
Scheme 18: on the basis of arbitrary scheme, described runner rotary engine further comprises fluid supply in scheme 1 to 12, described fluid supply is communicated with described centrifugal fluid passage through liquid entry portal.
Scheme 19: on the basis of arbitrary scheme, described runner rotary engine further comprises fluid supply in scheme 1 to 12, and described centrifugal fluid passage is communicated with described fluid supply through centrifugal pump.
Scheme 20: on the basis of arbitrary scheme, further make the bearing capacity of the working medium ingress of described injection channel be greater than 2MPa in scheme 1 to 19.
In the present invention, " described injection channel and described rotor have square setting " refers to that reaction force suffered when described injection channel sprays produces the set-up mode of moment of torsion to the spin axis of described rotor.
In the present invention, in order to improve engine efficiency, optionally according to known technology, on described rotor, establish thermal-protective coating.
In the present invention, in order to improve engine efficiency, optionally according to known technology, on described sleeve rotor and/or in described sleeve rotor, establish thermal-protective coating.
In the present invention, so-called " integrated setting " comprises the set-up mode of be connected setting and whole machine shaping.
In the present invention, described gas compressor can be axial flow, runoff, can be multistage, single-stage.
In the present invention, described turbine can be axial flow, runoff, can be multistage, single-stage.
In the present invention, the fuel that enters described firing chamber can enter by the mode of individual injection described firing chamber, after also can being mixed together with air, enters described firing chamber, can also through swivel joint, be input to described firing chamber by the running shaft of described rotor.
In the present invention, the bearing capacity of the working medium ingress of described injection channel is greater than 2MPa, 2.5MPa, 3MPa, 3.5MPa, 4MPa, 4.5MPa, 5MPa, 5.5MPa, 6MPa, 6.5MPa, 7MPa, 7.5MPa, 8MPa, 8.5MPa, 9MPa, 9.5MPa, 10MPa, 10.5MPa, 11MPa, 11.5MPa, 12MPa, 12.5MPa, 13MPa, 13.5MPa, 14MPa, 14.5MPa, 15MPa, 15.5MPa, 16MPa, 16.5MPa, 17MPa, 17.5MPa, 18MPa, 18.5MPa, 19MPa, 19.5MPa, 20MPa, 20.5MPa, 21MPa, 21.5MPa, 22MPa, 22.5MPa, 23MPa, 23.5MPa, 24MPa, 24.5MPa, 25MPa, 25.5MPa, 26MPa, 26.5MPa, 27Pa, 27.5MPa, 28MPa, 28.5MPa, 29MPa, 29.5MPa or be greater than 30MPa.
In the present invention, the power pressure of the working medium ingress of described injection channel should match with its bearing capacity, and the highest power pressure of the working medium ingress of described injection channel reaches its bearing capacity.
The present invention is in order to improve the working efficiency of described runner rotary engine to the bearing capacity pressure limiting of the working medium ingress of described injection channel.
In the present invention, so-called " centrifugal fluid passage " refers in radial direction has the fluid passage of distribution and by having in the radial direction the fluid passage of distribution and the fluid passage forming in the fluid passage that does not have in the radial direction to distribute, such as completely according to the fluid passage of radial direction setting, by gradually opening or the spiral fluid passage of convergent form setting, having in the radial direction fluid passage repeatedly etc.
In the present invention, so-called " injection channel " refers to that all can spray the passage that fluid obtains reaction force, for example, and subsonic effuser, supersonic nozzle (being Laval nozzle), turbine, turbine or water conservancy diversion injection channel etc.
In the present invention, so-called " attached injection channel " refers to that all can spray the passage that fluid obtains reaction force, for example, and subsonic effuser, supersonic nozzle (being Laval nozzle), turbine, turbine or water conservancy diversion injection channel etc.
In the present invention, the object of described injection channel, described attached injection channel setting is to produce reaction force by Fluid injection.
In the present invention, optionally according to known technology, condensate cooler, regenerator and/or liquor pump and wet tank are set, in being provided with the structure of described condensate cooler, the working medium of being sprayed by described injection channel enters described condensate cooler.
In the present invention, described fluid supply refers to liquid working substance source, device, unit, system or the storage tank of water or other liquid working substance (for example organic Rankine cycle fluid) for example can be provided, for example, the system being formed by wet tank and liquor pump, again for example, wet tank or by the wet tank of gravity force liquid-supply body etc.
In the present invention, the liquid working substance in described fluid supply can optionally be selected water, alkane, freon or alcohols etc.
In the present invention, described fluid supply is optionally made as described mixed-burned gas liquefaction source, mixed-burned gas liquefaction in described mixed-burned gas liquefaction source refers under the standard state being liquefied to be the gas of gaseous state, the gas here refers to that under standard state, its steam divides air pressure to be more than or equal to an atmospheric material, for example, liquefaction nitrogen, liquefied oxygen, liquefied carbon dioxide or liquefied air etc.
In the present invention, so-called A and B are communicated with and refer to that between A and B, working medium occurs to flow, and comprise that working medium flows to B or flows to A from B from A, or working medium first flows to B from A and from B, flows to A again.So-called " connection " comprises direct connection, indirect communication and is communicated with through operating unit, and described operating unit comprises valve, control mechanism, feed mechanism (pump) and heat exchanger etc.
In the present invention, so-called " rotor fluid passage " refers to rotating with described rotor of having that a part of fluid passage and described rotor coaxial line arrange at least, and with at least a portion of that a part of fluid passage of described rotor coaxial line setting be the non-fluid passage along conical liquid passage.
In the present invention, the gradually evolution that so-called " along conical liquid passage " refers to taper is to sending into the consistent conical liquid passage of fluid flow direction in pipe with described built-in liquid.
In the present invention, so-called " non-along conical liquid passage " refer to except the described fluid passage along all shapes conical liquid passage, such as uniform internal diameter fluid passage, non-uniform internal diameter fluid passage, inwall, is provided with the fluid passage of spiral or against conical liquid passage etc.
In the present invention, the gradually evolution that so-called " contrary conical liquid passage " refers to taper is to sending into described built-in liquid the conical liquid passage that fluid flow direction in pipe is contrary.
In the present invention, the gradually evolution that so-called " along coning conversion adapter " refers to taper is to the swivel joint identical with liquid flow direction.
In the present invention, the gradually evolution that so-called " contrary coning conversion adapter " refers to taper is to the swivel joint contrary with liquid flow direction.
In the present invention, so-called " disk rotary joint " refers to that the revolving part in swivel joint is provided with the swivel joint of disk, and the effect of this disk is to reduce leak of liquid.
In the present invention, above and certain the numerical value A of certain numerical value A includes given figure A below.
The inventor thinks according to thermodynamic (al) basic principle and on the observation of universe phenomenon: do not having under the prerequisite of external factor impact, heat can not absolutely convert other any type of energy or material to.In the tradition second law of thermodynamics, only set forth and do not had under the prerequisite of external factor impact, heat can not absolutely be changed successfully, and this law is correct, but is unilateral.Can heat be defined as with popular language to the minimum form of energy, or be the rubbish in universe referred to as this.By analysis, the inventor also thinks: the growing process of any biology (animal, plant, microorganism, virus and bacterium) is all heat release.By analysis, the inventor also thinks: any one process or any one circulation (are not limited to thermodynamic process, for example chemical reaction process, biochemical reaction process, photochemical reaction process, biological growth process, growing process are all included) its maximum acting ability conservation, the inventor thinks does not have photosynthetic growing process can not improve its acting ability, that is to say, the acting ability of bean sprouts is the acting ability sum that impossible add the nutrient of its absorption higher than the acting ability of bean or pea; Why the acting ability of one tree wood is greater than the acting ability of sapling, is because sunlight has participated in the growing process to trees by sapling with photosynthetic form.
The inventor thinks: the basic logic of heat engine work be restrain-be heated-disperse.So-called convergence is the increase process of the density of working medium, and for example condensation, compression all belong to convergence process, and under same pressure, the working medium degree of convergence that temperature is low is large; It is exactly the endothermic process of working medium that what is called is heated; What is called is dispersed the process of the density reduction that refers to working medium, for example, expand or spray.Any one disperses process all can form the reduction of acting ability, and for example, the acting ability of the air of gaseous state will be well below the acting ability of liquid air; The heat that methanol plus water adds moderate temperature generates carbon monoxide and hydrogen, although the carbon monoxide generating and the ignition heat of hydrogen are greater than ignition heat 20% left and right of methyl alcohol, but it is very little that its acting ability is greater than the ratio of acting ability of methyl alcohol, although its reason is this process and inhaled the heat of 20% left and right, the degree of divergence of resultant carbon monoxide and hydrogen is far longer than methyl alcohol.Therefore, utilizing physochlaina infudibularis that temperature is not high to add chemical reaction is the acting ability of having no idea effectively to improve resultant.
The inventor thinks: it is the process that entropy increases that distance increases, and the distance between cold & heat source also affects efficiency, and the little efficiency of distance is high, and the large efficiency of distance is low.
In the present invention, should, according to the known technology in heat energy and power field, in necessary place, necessary parts, unit or system etc. be set.
beneficial effect of the present invention is as follows:
Described runner rotary engine specific power of the present invention is high, disposal of pollutants is few, fuel diversity is good, cost of production is low.
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 4;
Shown in Fig. 5 is the structural representation of the embodiment of the present invention 5;
Shown in Fig. 6 is the structural representation of the embodiment of the present invention 6;
Shown in Fig. 7 is the structural representation of the embodiment of the present invention 7;
Shown in Fig. 8 is the structural representation of the embodiment of the present invention 8;
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 10;
In figure:
1 rotor, 11 centrifugal fluid passages, 12 pipelines, 13 stationary housings, 2 gas compressors, 3 firing chambers, 4 injection channels, 6 attached injection channels, 7 fluid supplies, 10 rotor fluid passages, 101 built-in liquid are sent into pipe.
Embodiment
Embodiment 1
Runner rotary engine as shown in Figure 1, comprise rotor 1 and firing chamber 3, centrifugal fluid passage 11 is set described rotor 1 is interior, described firing chamber 3 is arranged in described rotor 1, conduct heat in described centrifugal fluid passage 11,3 pairs of described firing chambers, described centrifugal fluid passage 11 is communicated with the working medium entrance of injection channel 4, and described injection channel 4 has square setting, the external outputting power of described rotor 1 with described rotor 1.
In the present embodiment, described rotor 1 has been made as sleeve rotor, and described firing chamber 3 is arranged in the inner chamber of described sleeve rotor, and described centrifugal fluid passage 11 is arranged in the sidewall of described sleeve rotor.
Embodiment 2
Runner rotary engine as shown in Figure 2, it further sets up gas compressor 2 on embodiment 1 basis, described gas compressor 2 and described rotor 1 integrated setting, the pressurized gas outlet of described gas compressor 2 is communicated with described firing chamber 3.
Embodiment 3
Runner rotary engine as shown in Figure 3, it is on embodiment 1 basis, further set up attached injection channel 6, described attached injection channel 6 and described rotor 1 integrated setting, the gas after conducting heat from described firing chamber 3 and to described centrifugal fluid passage 11 enters described attached injection channel 6.
Embodiment 4
Runner rotary engine as shown in Figure 4, it is on embodiment 2 basis, further set up attached injection channel 6, described attached injection channel 6 and described rotor 1 integrated setting, the gas after conducting heat from described firing chamber 3 and to described centrifugal fluid passage 11 enters described attached injection channel 6.
Embodiment 5
Runner rotary engine as shown in Figure 5, itself and embodiment's 3 difference is, changes into described centrifugal fluid passage 11 is made as to the pipeline 12 in the inner chamber that is arranged on described sleeve rotor.
Embodiment 6
Runner rotary engine as shown in Figure 6, itself and embodiment's 5 difference is, described pipeline 12 is made as volute.
Embodiment 7
Runner rotary engine as shown in Figure 7, itself and embodiment's 1 difference is, pipeline 12 is set in the inner chamber of described sleeve rotor, and described pipeline 12 is communicated with described centrifugal fluid passage 11.
Embodiment 8
Runner rotary engine as shown in Figure 8, itself and embodiment's 7 difference is, described pipeline 12 is made as volute.
In embodiment 6 and 8, described pipeline has all been made as cylindricality volute, and as the mode of execution that can convert, described pipeline 12 can change and is made as dish type volute.
As the mode of execution that can convert, in above-mentioned all mode of executions of the present invention, the mode of execution can be optionally obtaining with reference to embodiment 5 to 8 and conversion thereof arranges described centrifugal fluid passage 11 and described pipeline 12.
Embodiment 9
Runner rotary engine as shown in Figure 9, it arranges stationary housings 13 in the outer increase of described rotor 1 on embodiment 1 basis.
As the mode of execution that can convert, all of the embodiments of the present invention in the specific implementation, can be with reference to the present embodiment optionally in described rotor 1 peripheral hardware stationary housings 13.
Embodiment 10
Runner rotary engine as shown in figure 10, it is on embodiment 1 basis, set up fluid supply 7, on described rotor 1, establish rotor fluid passage 10, in described rotor fluid passage 10, establish and do not contact with described rotor fluid passage 10 and send into pipe 101 with the built-in liquid of described rotor 1 coaxial line, described fluid supply 7 is sent into pipe 101 through described built-in liquid and is communicated with described rotor fluid passage 10, and described rotor fluid passage 10 is communicated with described centrifugal fluid passage 11.
As the mode of execution that can convert, can change into described centrifugal fluid passage 11 is communicated with described fluid supply 7 through swivel joint, and further optionally described swivel joint is made as to uniform internal diameter swivel joint, be made as along coning conversion adapter, be made as contrary coning conversion adapter or be made as disk rotary joint; Or change into and make described fluid supply 7 send into and mouthful be communicated with described centrifugal fluid passage through liquid; Or change into described fluid supply 7 is communicated with described centrifugal fluid passage through fluid drips entrance; Or change into described fluid supply 7 is communicated with described centrifugal fluid passage through liquid entry portal; Or change into described centrifugal fluid passage 11 is communicated with described fluid supply through centrifugal pump.
As the mode of execution that can convert, all of the embodiments of the present invention all can and arrange the mode of communicating of described fluid supply 7 and described centrifugal fluid passage 11 with reference to the present embodiment at the mode of execution that the basic up conversion of the present embodiment obtains.
In all of the embodiments of the present invention, all by described injection channel 4 concrete be made as supersonic nozzle (being Laval nozzle), as the mode of execution that can convert, the described injection channel 4 in all mode of executions can be made as turbine (comprising turbine), subsonic effuser or change and be made as water conservancy diversion injection channel.
In the present invention in all mode of executions that are provided with described attached injection channel 6, all by described attached injection channel 6 concrete be made as turbine, as the mode of execution that can convert, described attached injection channel 6 can be made as subsonic effuser, supersonic nozzle or change and be made as water conservancy diversion injection channel.
In the embodiment who is provided with described attached injection channel 6 of the present invention, the described runner rotary engine that is arranged so that this embodiment of described attached injection channel 6 can utilize the heat carrying from the working medium to after 11 heat transfers of described centrifugal fluid passage of described firing chamber 3 to increase the acting ability of described rotor 1, raises the efficiency; As the mode of execution that can convert, described attached injection channel 6 in all embodiments that are provided with described attached injection channel 6 can not established, and now from the working medium after being conducted heat in described centrifugal fluid passage 11 of described firing chamber 3, can directly emit or do other purposes.
In above-mentioned all embodiments of the present invention, all by described rotor 1 concrete be made as sleeve rotor, in the concrete inner chamber that is arranged on described sleeve rotor 1 in described firing chamber 3, as the mode of execution that can convert, described rotor 1 can be set to solid rotor, described firing chamber 3, described centrifugal fluid passage 11 can form by the mode of emptying in described solid rotor, and described rotor 1 can also change and is made as other any suitable structures.
All mode of executions that is provided with described gas compressor 2 of the present invention in the specific implementation, can be optionally axial flow by described gas compressor or be made as radial-flow type, can also optionally described gas compressor be made as multistage or be made as single-stage.
All mode of executions that is provided with described turbine of the present invention in the specific implementation, can optionally be made as axial flow by described turbine or be made as radial-flow type and can also optionally described turbine be made as multistage or be made as single-stage.
When all of the embodiments of the present invention is specifically implemented, can optionally the bearing capacity of the working medium ingress of described injection channel 4 be made as and be greater than 2MPa, 2.5MPa, 3MPa, 3.5MPa, 4MPa, 4.5MPa, 5MPa, 5.5MPa, 6MPa, 6.5MPa, 7MPa, 7.5MPa, 8MPa, 8.5MPa, 9MPa, 9.5MPa, 10MPa, 10.5MPa, 11MPa, 11.5MPa, 12MPa, 12.5MPa, 13MPa, 13.5MPa, 14MPa, 14.5MPa, 15MPa, 15.5MPa, 16MPa, 16.5MPa, 17MPa, 17.5MPa, 18MPa, 18.5MPa, 19MPa, 19.5MPa, 20MPa, 20.5MPa, 21MPa, 21.5MPa, 22MPa, 22.5MPa, 23MPa, 23.5MPa, 24MPa, 24.5MPa, 25MPa, 25.5MPa, 26MPa, 26.5MPa, 27Pa, 27.5MPa, 28MPa, 28.5MPa, 29MPa, 29.5MPa or be made as and be greater than 30MPa, thereby improve the efficiency of described runner rotary engine.
Obviously, the invention is not restricted to above embodiment, according to the known technology of related domain and technological scheme disclosed in this invention, can derive or association goes out many flexible programs, all these flexible programs, also should think protection scope of the present invention.
Claims (10)
1. a runner rotary engine, comprise rotor (1) and firing chamber (3), it is characterized in that: centrifugal fluid passage (11) is set in described rotor (1), described firing chamber (3) is arranged in described rotor (1), conduct heat to described centrifugal fluid passage (11) in described firing chamber (3), described centrifugal fluid passage (11) is communicated with the working medium entrance of injection channel (4), described injection channel (4) has square setting with described rotor (1), and described rotor (1) is outputting power externally.
2. runner rotary engine as claimed in claim 1, it is characterized in that: described runner rotary engine also comprises gas compressor (2), described gas compressor (2) and described rotor (1) integrated setting, the pressurized gas outlet of described gas compressor (2) is communicated with described firing chamber (3).
3. runner rotary engine as claimed in claim 1, it is characterized in that: described runner rotary engine also comprises attached injection channel (6), described attached injection channel (6) and described rotor (1) integrated setting, the gas after conducting heat from described firing chamber (3) and to described centrifugal fluid passage (11) enters described attached injection channel (6).
4. runner rotary engine as claimed in claim 1, it is characterized in that: described runner rotary engine also comprises gas compressor (2) and attached injection channel (6), described gas compressor (2) and described rotor (1) integrated setting, described attached injection channel (6) and described rotor (1) integrated setting, the pressurized gas outlet of described gas compressor (2) is communicated with described firing chamber (3), and the gas after conducting heat from described firing chamber (3) and to described centrifugal fluid passage (11) enters described attached injection channel (6).
5. runner rotary engine as claimed in claim 3, is characterized in that: described attached injection channel (6) is made as turbine.
6. runner rotary engine as claimed in claim 4, is characterized in that: described attached injection channel (6) is made as turbine.
7. runner rotary engine as described in any one in claim 1 to 6, is characterized in that: described rotor (1) is made as sleeve rotor.
8. runner rotary engine as claimed in claim 7, is characterized in that: described firing chamber (3) are arranged in the inner chamber of described sleeve rotor.
9. runner rotary engine as claimed in claim 7, is characterized in that: described centrifugal fluid passage (11) is made as the pipeline (12) in the inner chamber that is arranged on described sleeve rotor.
10. runner rotary engine as claimed in claim 7, is characterized in that: pipeline (12) is set in the inner chamber of described sleeve rotor, and described pipeline (12) is communicated with described centrifugal fluid passage (11).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410101573.3A CN103953442B (en) | 2013-03-18 | 2014-03-18 | Runner rotary engine |
Applications Claiming Priority (16)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310085822 | 2013-03-18 | ||
| CN201310085822.X | 2013-03-18 | ||
| CN201310085822X | 2013-03-18 | ||
| CN201310087735.8 | 2013-03-19 | ||
| CN2013100877358 | 2013-03-19 | ||
| CN201310087735 | 2013-03-19 | ||
| CN201310097924.3 | 2013-03-25 | ||
| CN2013100979243 | 2013-03-25 | ||
| CN201310097924 | 2013-03-25 | ||
| CN2013101088091 | 2013-03-29 | ||
| CN201310108809.1 | 2013-03-29 | ||
| CN201310108809 | 2013-03-29 | ||
| CN2013101087436 | 2013-03-30 | ||
| CN201310108743 | 2013-03-30 | ||
| CN201310108743.6 | 2013-03-30 | ||
| CN201410101573.3A CN103953442B (en) | 2013-03-18 | 2014-03-18 | Runner rotary engine |
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| Publication Number | Publication Date |
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| CN103953442A true CN103953442A (en) | 2014-07-30 |
| CN103953442B CN103953442B (en) | 2018-08-21 |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3899874A (en) * | 1974-09-11 | 1975-08-19 | Henry E Bailey | Turbine engine |
| CN1115004A (en) * | 1995-04-20 | 1996-01-17 | 郭颖 | Reaction type jet engine |
| CN2232084Y (en) * | 1994-12-20 | 1996-07-31 | 李红江 | Counter-force external combustion jet engine |
| CN2387274Y (en) * | 1999-09-22 | 2000-07-12 | 蔡盛龙 | Rotary jet shaft engine |
| CN1356454A (en) * | 2000-12-05 | 2002-07-03 | 祝长宇 | Centrifugal engine |
| US20080173592A1 (en) * | 2007-01-24 | 2008-07-24 | Honeywell International Inc. | Oil centrifuge |
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2014
- 2014-03-18 CN CN201410101573.3A patent/CN103953442B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3899874A (en) * | 1974-09-11 | 1975-08-19 | Henry E Bailey | Turbine engine |
| CN2232084Y (en) * | 1994-12-20 | 1996-07-31 | 李红江 | Counter-force external combustion jet engine |
| CN1115004A (en) * | 1995-04-20 | 1996-01-17 | 郭颖 | Reaction type jet engine |
| CN2387274Y (en) * | 1999-09-22 | 2000-07-12 | 蔡盛龙 | Rotary jet shaft engine |
| CN1356454A (en) * | 2000-12-05 | 2002-07-03 | 祝长宇 | Centrifugal engine |
| US20080173592A1 (en) * | 2007-01-24 | 2008-07-24 | Honeywell International Inc. | Oil centrifuge |
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| CN103953442B (en) | 2018-08-21 |
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