CN104265504B - Turn burn engine - Google Patents

Turn burn engine Download PDF

Info

Publication number
CN104265504B
CN104265504B CN201410256319.0A CN201410256319A CN104265504B CN 104265504 B CN104265504 B CN 104265504B CN 201410256319 A CN201410256319 A CN 201410256319A CN 104265504 B CN104265504 B CN 104265504B
Authority
CN
China
Prior art keywords
compression unit
heat extraction
unit
extraction compression
combustion chamber
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
Application number
CN201410256319.0A
Other languages
Chinese (zh)
Other versions
CN104265504A (en
Inventor
靳北彪
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
XUZHOU RUNFENG NEW MATERIALS Co.,Ltd.
Original Assignee
Molecule Power Beijing Technology Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Molecule Power Beijing Technology Co Ltd filed Critical Molecule Power Beijing Technology Co Ltd
Priority to CN201410256319.0A priority Critical patent/CN104265504B/en
Publication of CN104265504A publication Critical patent/CN104265504A/en
Application granted granted Critical
Publication of CN104265504B publication Critical patent/CN104265504B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Supercharger (AREA)

Abstract

The invention discloses one and turn burn engine, including rotational structure body, combustion chamber, injection channel and air compression unit, described combustion chamber is arranged on described rotational structure body, described injection channel and described rotational structure body have square to arrange, described combustion chamber connects with the working medium entrance of described injection channel, described air compression unit includes heat extraction compression unit and non-heat extraction compression unit, the pressure ratio of described heat extraction compression unit is more than 10, at the sender property outlet of described heat extraction compression unit, Temperature of Working is less than 373K, the pressure ratio of described non-heat extraction compression unit is more than 5, the sender property outlet of described heat extraction compression unit connects with the working medium entrance of described non-heat extraction compression unit, the sender property outlet of described non-heat extraction compression unit and described combustion chamber, described rotational structure body externally exports power.The efficiency of heat to power output of the present invention is high, disposal of pollutants is few.

Description

Turn burn engine
Technical field
The present invention relates to heat energy and dynamic field, especially one and turn burn engine.
Background technology
Otto engine or diesel cycle engine carry out that the efficiency of heat to power output is low, disposal of pollutants is tight Weight, accordingly, it would be desirable to 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, one turns burn engine, including rotational structure body, combustion chamber, injection channel and air pressure Contracting unit, described combustion chamber is arranged on described rotational structure body, described injection channel and described rotational structure Body has square to arrange, and described combustion chamber connects with the working medium entrance of described injection channel, described air compression unit Including heat extraction compression unit and non-heat extraction compression unit, the pressure ratio of described heat extraction compression unit is more than 10, described At the sender property outlet of heat extraction compression unit, Temperature of Working is less than 373K, the pressure ratio of described non-heat extraction compression unit More than 5, the sender property outlet of described heat extraction compression unit connects with the working medium entrance of described non-heat extraction compression unit, The sender property outlet of described non-heat extraction compression unit and described combustion chamber, described rotational structure body externally exports Power.
Scheme 2, one turns burn engine, including rotational structure body, combustion chamber, injection channel and air pressure Contracting unit, described combustion chamber is arranged on described rotational structure body, described injection channel and described rotational structure Body has square to arrange, and described combustion chamber connects with the working medium entrance of described injection channel, described air compression unit Including heat extraction compression unit and non-heat extraction compression unit, the pressure ratio of described heat extraction compression unit is more than 10, described At the sender property outlet of heat extraction compression unit, Temperature of Working is less than 373K, the working medium of described non-heat extraction compression unit Exit Temperature of Working is higher than the ignition point of the fuel entering described combustion chamber, the work of described heat extraction compression unit Matter outlet connects with the working medium entrance of described non-heat extraction compression unit, and the working medium of described non-heat extraction compression unit goes out Mouth and described combustion chamber, described rotational structure body externally exports power.
Scheme 3, one turns burn engine, including rotational structure body, combustion chamber, injection channel and air pressure Contracting unit, described combustion chamber is arranged on described rotational structure body, described injection channel and described rotational structure Body has square to arrange, and described combustion chamber connects with the working medium entrance of described injection channel, described air compression unit Including heat extraction compression unit and non-heat extraction compression unit, the pressure ratio of described heat extraction compression unit is more than 10, described At the sender property outlet of heat extraction compression unit, Temperature of Working is less than 373K, the working medium of described non-heat extraction compression unit Exit Temperature of Working is higher than 1000K, and the sender property outlet of described heat extraction compression unit compresses with described non-heat extraction The working medium entrance connection of unit, the sender property outlet of described non-heat extraction compression unit and described combustion chamber, Combustion chemistry reaction occurs in described combustion chamber, and described rotational structure body externally exports power.
Scheme 4, one turns burn engine, including rotational structure body, combustion chamber, injection channel and air pressure Contracting unit, described combustion chamber is arranged on described rotational structure body, described injection channel and described rotational structure Body has square to arrange, and described combustion chamber connects with the working medium entrance of described injection channel, described air compression unit Including heat extraction compression unit and non-heat extraction compression unit, the pressure ratio of described heat extraction compression unit is more than 10, described At the sender property outlet of heat extraction compression unit, Temperature of Working is less than 373K, the working medium of described non-heat extraction compression unit Exit Temperature of Working is higher than 1000K, and the sender property outlet of described heat extraction compression unit compresses with described non-heat extraction The working medium entrance connection of unit, the sender property outlet of described non-heat extraction compression unit and described combustion chamber, Constant temperature combustion chemical reaction occurs in described combustion chamber, and described rotational structure body externally exports power.
Scheme 5, on the basis of aforementioned schemes 1,2,3 or 4, described injection channel is set to jet pipe.
Scheme 6, on the basis of aforementioned schemes 1,2,3 or 4, described heat extraction compression unit is set to include The air injection unit of one-level displacement type compressor, sets cooler at the sender property outlet of described displacement type compressor; Or described heat extraction compression unit is set to the air injection unit of two-stage above displacement type compressor, at least one inter-stage If cooler, at the sender property outlet of displacement type compressor described in final stage, set cooler.
Scheme 7, on the basis of aforementioned schemes 1,2,3 or 4, described heat extraction compression unit is set to include The air injection unit of first-order rate type compressor, sets cooler at the sender property outlet of described velocity profile compressor; Or described heat extraction compression unit is set to the air injection unit of two-stage above velocity profile compressor, at least one inter-stage If cooler, at the sender property outlet of velocity profile compressor described in final stage, set cooler.
Scheme 8, on the basis of aforementioned schemes 1,2,3 or 4, described heat extraction compression unit is set to include The air injection unit of one stage impeller compressor, sets cooler at the sender property outlet of described impeller compressor;Or institute State heat extraction compression unit and be set to the air injection unit of two-stage above impeller compressor, set cooling at least one inter-stage Device, sets cooler at the sender property outlet of impeller compressor described in final stage.
Scheme 9, on the basis of aforementioned schemes 1,2,3 or 4, described heat extraction compression unit is set to include The air injection unit of first stage piston formula compressor, sets cooler at the sender property outlet of described piston compressor; Or described heat extraction compression unit is set to the air injection unit of the above piston compressor of two-stage, at least one inter-stage If cooler, at the sender property outlet of piston compressor described in final stage, set cooler.
Scheme 10, on the basis of aforementioned schemes 1,2,3 or 4, described heat extraction compression unit is set to include The air injection unit of one-level spiral lobe compressor, sets cooler at the sender property outlet of described spiral lobe compressor; Or described heat extraction compression unit is set to the air injection unit of the above spiral lobe compressor of two-stage, at least one inter-stage If cooler, at the sender property outlet of spiral lobe compressor described in final stage, set cooler.
Scheme 11, on the basis of aforementioned schemes 1,2,3 or 4, described non-heat extraction compression unit is set to bag Include one-level or the air injection unit of two-stage above displacement type compressor.
Scheme 12, on the basis of aforementioned schemes 1,2,3 or 4, described non-heat extraction compression unit is set to bag Include one-level or the air injection unit of two-stage above velocity profile compressor.
Scheme 13, on the basis of aforementioned schemes 1,2,3 or 4, described non-heat extraction compression unit is set to bag Include one-level or the air injection unit of two-stage above vane type compressor.
Scheme 14, on the basis of aforementioned schemes 1,2,3 or 4, described non-heat extraction compression unit is set to bag Include one-level or the air injection unit of the above piston compressor of two-stage.
Scheme 15, on the basis of aforementioned schemes 1,2,3 or 4, described non-heat extraction compression unit is set to bag Include one-level or the air injection unit of the above spiral lobe compressor of two-stage.
Inventors believe that, the work basic logic of heat engine be restrain-be heated-dissipate, during these three Any one degree carried out is the highest on the premise of other two processes are identical, and the efficiency of heat engine is the highest.This If three processes represent with A, B, C respectively, then efficiency has positive relationship (institute with the product of A, B, C The positive relationship of meaning refers to that both growing directions are identical, reduces direction the most identical, such as, if we say X and Y is positive relationship, refers to also increase along with the growth Y of X, otherwise, along with the reduction Y of X also reduces). Degree of convergence is relevant with pressure and temp, and the biggest degree of convergence of pressure is the biggest, and temperature is the lowest, and degree of convergence is the biggest, Under same pressure, temperature height person, degree of convergence is low, the low person of temperature, and degree of convergence is high.For difference Working medium, under same temperature and pressure, adiabatic exponent big person degree of convergence is big, and the little person of adiabatic exponent restrains Degree is little.Improve the efficiency of heat engine, particularly will be on the premise of working medium maximum temperature keeps below certain value The fundamental way improving efficiency of heat engine is to improve degree of convergence.And improve degree of convergence and carry out certain compression and be Necessary, but phase heat release is even more important before compression, and phase heat release just can make the effect of heat engine the most before compression Rate reaches top.
The present invention can effectively in diesel cycle and Alto be circulated in association between temperature and pressure Being split, pressure is higher, temperature relative (relative in above-mentioned two circulations to make working medium burning be in before being heated With under equal pressure) relatively low state, after such expansion work, the temperature drop of working medium is relatively big, and efficiency increases substantially, Owing to being continuous burning, it is possible to effectively reduce the discharge of the pollutants such as PM2.5.
In the present invention, " described injection channel and described rotational structure body have square to arrange " refers to described injection channel Reaction force suffered during injection produces the set-up mode of moment of torsion to the rotation of described rotational structure body.
In the present invention, so-called injection channel refers to that all can spray fluid and obtain the passage of reaction force, Such as, subsonic effuser, supersonic nozzle (i.e. Laval nozzle), turbine (including turbine) or water conservancy diversion Injection channel etc..
In the present invention, the purpose that described injection channel is arranged is to produce reaction force by fluid injection.
In the present invention, described heat extraction compression unit refers in compression procedure and/or upon compression except having for protecting Also have outside the necessary cooling procedure of card mechanism normal operation for the purpose of reducing work done during compression by compression work Matter (air) carries out cooling down the compression unit of the process making the external heat extraction of working medium, and such as, cascade EDFA is many Level compression unit, entrance cooling multi-stage compression unit, entrance cooling cascade EDFA multi-stage compression unit, The multi-stage compression unit of outlet cooling and the multi-stage compression unit etc. of the cascade EDFA of outlet cooling;Described heat extraction Compression unit can be velocity profile, displacement type or both combine, such as piston type, vane type, screw, Piston and impeller serial formula, impeller and screw rod tandem or piston and screw rod tandem etc..
In the present invention, described non-heat extraction compression unit refer in compression procedure and/or upon compression except have for Ensure not include for the purpose of reducing work done during compression being compressed outside the necessary cooling procedure of mechanism's normal operation Working medium (air) carries out cooling down the compression unit of the process making the external heat extraction of working medium, such as single stage compress unit The coldest multi-stage compression unit etc.;Described non-heat extraction compression unit can be velocity profile, displacement type or both Combining, such as piston type, vane type, screw, piston are connected with screw rod with impeller serial formula, impeller Formula or piston and screw rod tandem etc..
In the present invention, described constant temperature combustion chemical reaction refers to that working medium constantly expands in combustion and makes burning The temperature rise combustion system less than 500K.
In the present invention, so-called rotational structure body refers to all structures that can rotate, as flywheel, The bar that can rotate and the loop configuration body etc. that can rotate.
In the present invention, so-called cooler refers to all devices can lowered the temperature gas, such as, dispel the heat Device, the hybrid cooler device of gas temperature (mix with cold flow body reduce) etc., its objective is will Gas compressed, gas in compression process and gas compressed lower the temperature.
In the present invention, the pressure ratio of described heat extraction compression unit more than 10,11,12,13,14,15,16, 17,18,19 or more than 20.
In the present invention, the pressure ratio of described non-heat extraction compression unit more than 5,6,7,8,9,10,11,12, 13,14,15,16,17,18,19 or more than 20.
In the present invention, certain more than numerical value A and certain below numerical value A all includes this number A.
The present inventor thinks according to thermodynamic (al) general principle and the observation to universe phenomenon: do not having outside On the premise of factor impact, heat can not absolutely be converted into other any type of energy or material. Conventional thermal mechanics second law only elaborating, heat can not percent on the premise of not having external factor impact The conversion success of hundred, this law is correct, but is unilateral.Can be fixed by heat with popular language Justice is the minimum form of energy, or referred to as this is the rubbish in universe.Through analyzing, the present inventor is additionally considered that: The growth course of any biology (animal, plant, microorganism, virus and bacterium) is all heat release.Through dividing Analysis, the present inventor is additionally considered that: any one process or any one circulation (be not limited to thermodynamic process, Such as chemical reaction process, biochemical reaction process, photochemical reaction process, biological growth process, plant Thing growth course is included) its maximum acting ability conservation, inventors believe that the most photosynthetic Growing process can not improve its acting ability, say, that the acting ability of bean sprouts is impossible The acting ability sum of its nutrient absorbed is added higher than the acting ability of bean or pea;Why the doing of one tree wood Function power is greater than the acting ability of sapling, be because sunlight with photosynthetic form take part in by sapling to The growth course of trees.
Present inventors believe that the basic logic that heat engine works be restrain-be heated-dissipate.So-called convergence is working medium The increase process of density, such as condense, compress and all belong to convergence process, under same pressure, temperature is low Working medium degree of convergence big;It is exactly the endothermic process of working medium that what is called is heated;What is called dissipates the density referring to working medium The process reduced, such as, expand or spray.Any one dissipates process all can form the reduction of acting ability, Such as, the acting ability of the air of gaseous state will be well below the acting ability of liquid air;During methanol plus water adds Equitemperature be thermally generated carbon monoxide and hydrogen, although the carbon monoxide generated and the combustion heat of hydrogen are more than The combustion heat about 20% of methyl alcohol, but its acting ability the most micro-more than the ratio of acting ability of methyl alcohol its Micro-, although its reason is this process and has inhaled the heat of about 20%, but product carbon monoxide and hydrogen Degree of divergence be far longer than methyl alcohol.Therefore, it is to have no idea that the physochlaina infudibularis utilizing temperature the highest adds chemical reaction It is effectively improved the acting ability of product.
Present inventors believe that distance increase is the process that entropy increases, the distance between Cooling and Heat Source also affects efficiency, High apart from little efficiency, low apart from big efficiency.
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:
The efficiency of the heat to power output of the present invention is high, disposal of pollutants is few.
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;
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;
Shown in Figure 14 is the structural representation of the embodiment of the present invention 14;
Shown in Figure 15 is the structural representation of the embodiment of the present invention 15;
Shown in Figure 16 is the structural representation of the embodiment of the present invention 16.
Detailed description of the invention
Embodiment 1
As shown in Figure 1 turn burn engine, including rotational structure body 1, combustion chamber 2, injection channel 3 and Air compression unit 4, described combustion chamber 2 is arranged on described rotational structure body 1, described injection channel 3 Having square to arrange with described rotational structure body 1, described combustion chamber 2 connects with the working medium entrance of described injection channel 3 Logical, described air compression unit 4 includes heat extraction compression unit 41 and non-heat extraction compression unit 42, described row The pressure ratio of thermal compression unit 41 is more than 10, and at the sender property outlet of described heat extraction compression unit 41, Temperature of Working is low In 373K, the pressure ratio of described non-heat extraction compression unit 42 is more than 5, the working medium of described heat extraction compression unit 41 Outlet connects with the working medium entrance of described non-heat extraction compression unit 42, the work of described non-heat extraction compression unit 42 Matter outlet connects with described combustion chamber 2, and described rotational structure body 1 externally exports power.
Embodiment 2
As shown in Figure 2 turn burn engine, including rotational structure body 1, combustion chamber 2, injection channel 3 and Air compression unit 4, described combustion chamber 2 is arranged on described rotational structure body 1, described injection channel 3 Having square to arrange with described rotational structure body 1, described combustion chamber 2 connects with the working medium entrance of described injection channel 3 Logical, described air compression unit 4 includes heat extraction compression unit 41 and non-heat extraction compression unit 42, described row The pressure ratio of thermal compression unit 41 is more than 10, and at the sender property outlet of described heat extraction compression unit 41, Temperature of Working is low In 373K, at the sender property outlet of described non-heat extraction compression unit 42, Temperature of Working is higher than entering described combustion chamber The ignition point of the fuel of 2, the sender property outlet of described heat extraction compression unit 41 and described non-heat extraction compression unit The working medium entrance connection of 42, the sender property outlet of described non-heat extraction compression unit 42 connects with described combustion chamber 2, Described rotational structure body 1 externally exports power.
Embodiment 3
One as shown in Figure 3 turns burn engine, including rotational structure body 1, combustion chamber 2, injection channel 3 With air compression unit 4, it is characterised in that: described combustion chamber 2 is arranged on described rotational structure body 1, Described injection channel 3 has square to arrange with described rotational structure body 1, described combustion chamber 2 and described injection channel The working medium entrance connection of 3, described air compression unit 4 includes that heat extraction compression unit 41 and non-heat extraction compression are single Unit 42, the pressure ratio of described heat extraction compression unit 41 is more than 10, and the working medium of described heat extraction compression unit 41 goes out At Kou, Temperature of Working is less than 373K, and at the sender property outlet of described non-heat extraction compression unit 42, Temperature of Working is higher than 1000K, the sender property outlet of described heat extraction compression unit 41 enters with the working medium of described non-heat extraction compression unit 42 Mouth connection, the sender property outlet of described non-heat extraction compression unit 42 connects with described combustion chamber 2, in described combustion Combustion chemistry reaction occurs in burning room 2, and described rotational structure body 1 externally exports power.
Embodiment 4
As shown in Figure 4 turn burn engine, including rotational structure body 1, combustion chamber 2, injection channel 3 and Air compression unit 4, described combustion chamber 2 is arranged on described rotational structure body 1, described injection channel 3 Having square to arrange with described rotational structure body 1, described combustion chamber 2 connects with the working medium entrance of described injection channel 3 Logical, described air compression unit 4 includes heat extraction compression unit 41 and non-heat extraction compression unit 42, described row The pressure ratio of thermal compression unit 41 is more than 10, and at the sender property outlet of described heat extraction compression unit 41, Temperature of Working is low In 373K, at the sender property outlet of described non-heat extraction compression unit 42, Temperature of Working is higher than 1000K, described row The sender property outlet of thermal compression unit 41 connects with the working medium entrance of described non-heat extraction compression unit 42, described non- The sender property outlet of heat extraction compression unit 42 connects with described combustion chamber 2, and perseverance occurs in described combustion chamber 2 Temperature combustion chemistry reaction, described rotational structure body 1 externally exports power.
Embodiment 5
As shown in Figure 5 turn burn engine, the difference with embodiment 1 is, described heat extraction compression unit 41 It is set to include the air injection unit of one-level displacement type compressor, such as roots-type compressor.Non-heat extraction compression unit sets For the compression unit of displacement type compressor, such as roots-type compressor.
Embodiment 6
As shown in Figure 6 turn burn engine, the difference with embodiment 5 is, at described displacement type compressor Sender property outlet at set cooler;Or described heat extraction compression unit 41 is set to two-stage above displacement type compressor Air injection unit, set cooler at least one inter-stage, at the sender property outlet of displacement type compressor described in final stage Place sets cooler.
As disposable embodiment, described heat extraction compression unit is optionally set to sieve of more than two-stage Thatch formula compressor, arranges cooler at the sender property outlet of first order roots-type compressor, or at second level sieve At thatch formula blower outlet, cooling is set, cooling is set at the sender property outlet of third level roots-type compressor Device.
Embodiment 7
As shown in Figure 7 turn burn engine, the difference with embodiment 5 is, described heat extraction compression unit 41 It is set to include the air injection unit of first-order rate type compressor, sets at the sender property outlet of described velocity profile compressor Cooler.
As disposable embodiment, described heat extraction compression unit 41 is optionally set to include one-level The air injection unit of impeller compressor, sets cooler at the sender property outlet of described impeller compressor.
As disposable embodiment, described non-heat extraction compression unit 42 is optionally set to vane type Compressor.
Embodiment 8
As shown in Figure 8 turn burn engine, the difference with embodiment 7 is, described heat extraction compression unit 41 It is set to the air injection unit of two-stage above impeller compressor, sets cooler at least one inter-stage, described in final stage Cooler is set at the sender property outlet of impeller compressor.
As disposable embodiment, described heat extraction compression unit is optionally set to the leaf of more than two-stage Wheel compressor, arranges cooler at the sender property outlet of first order impeller compressor, or in second level impeller pressure Mechanism of qi exit arranges cooling, arranges cooler at the sender property outlet of third level impeller compressor.
Embodiment 9
As shown in Figure 9 turn burn engine, the difference with embodiment 7 is, described heat extraction compression unit 41 It is set to include the air injection unit of first stage piston formula compressor, sets at the sender property outlet of described piston compressor Cooler;Described non-heat extraction compression unit 42 is set to piston compressor.
Embodiment 10
As shown in Figure 10 turn burn engine, the difference with embodiment 9 is, described heat extraction compression unit 41 air injection unit being set to the above piston compressor of two-stage, set cooler at least one inter-stage, in final stage Cooler is set at the sender property outlet of described piston compressor.
As disposable embodiment, described heat extraction compression unit is optionally set to the work of more than two-stage Plug compressor, arranges cooler at the sender property outlet of first order piston compressor, or lives in the second level Cooler is set at plug blower outlet, or arranges cold at the sender property outlet of third level piston compressor But device.
Embodiment 11
As shown in figure 11 turn burn engine, the difference with embodiment 5 is, described heat extraction compression unit 41 are set to include the air injection unit of one-level spiral lobe compressor, at the sender property outlet of described spiral lobe compressor If cooler;Described non-heat extraction compression unit 42 is set to the air injection unit of one-level spiral lobe compressor.
Embodiment 12
As shown in figure 12 turn burn engine, the difference with embodiment 11 is, described heat extraction compression unit 41 air injection unit being set to the above spiral lobe compressor of two-stage, set cooler at least one inter-stage, in final stage Cooler is set at the sender property outlet of described spiral lobe compressor.
As disposable embodiment, described heat extraction compression unit 41 is optionally set to more than two-stage Spiral lobe compressor, cooler is set at the sender property outlet of first order screw mechanism of qi, or in the second level Spiral lobe compressor exit arranges cooling, or arranges cold at the sender property outlet of third level spiral lobe compressor But device.
Embodiment 13
Turning burn engine as shown in fig. 13 that, the difference with embodiment 1 is, described non-heat extraction compression is single Unit 42 is set to include one-level or the air injection unit of two-stage above displacement type compressor.
As disposable embodiment, described non-heat extraction compression unit is optionally set to displacement type and calms the anger Machine, such as roots-type compressor.
All of the embodiments of the present invention all can refer to the present embodiment non-heat extraction compression unit 42 and is set to include one Level or the air injection unit of two-stage above roots-type compressor.
Embodiment 14
As shown in figure 14 turn burn engine, the difference with embodiment 1 is, described non-heat extraction compression is single Unit 42 is set to include one-level or the air injection unit of two-stage above velocity profile compressor.
As disposable embodiment, described non-heat extraction compression unit is optionally set to more than two-stage Vane type compressor.
As disposable embodiment, described non-heat extraction compression unit 42 is optionally set to include one Level or the air injection unit of two-stage above vane type compressor.
All of the embodiments of the present invention all can refer to the present embodiment non-heat extraction compression unit 42 and is set to include one Level or the air injection unit of two-stage above vane type compressor.
Embodiment 15
As shown in figure 15 turn burn engine, the difference with embodiment 1 is, described non-heat extraction compression is single Unit 42 is set to include one-level or the air injection unit of the above piston compressor of two-stage.
All of the embodiments of the present invention all can refer to the present embodiment non-heat extraction compression unit 42 and is set to include one Level or the air injection unit of the above piston compressor of two-stage.
Embodiment 16
As shown in figure 16 turn burn engine, the difference with embodiment 1 is, described non-heat extraction compression is single Unit 42 is set to include one-level or the air injection unit of the above spiral lobe compressor of two-stage.
All of the embodiments of the present invention all can refer to the present embodiment non-heat extraction compression unit 42 and is set to include one Level or the air injection unit of the above spiral lobe compressor of two-stage.
As disposable embodiment, in above-mentioned all embodiments of the present invention, can selective Described injection channel 3 is made to be set to jet pipe.
As the embodiment that can convert, the above-mentioned all embodiments in the present invention the most selectively make The pressure ratio of described heat extraction compression unit 41 changes into more than 11,12,13,14,15,16,17,18,19, Or more than 20.
Can as the embodiment that can convert, embodiment 1 and the embodiment on the basis of embodiment 1 Optionally to make the pressure ratio of described non-heat extraction compression unit 42 change into more than 6,7,8,9,10,11, 12,13,14,15,16,17,18,19 or more than 20.
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 (15)

1. turn a burn engine, including rotational structure body (1), combustion chamber (2), injection channel (3) With air compression unit (4), it is characterised in that: described combustion chamber (2) are arranged on described rotational structure body (1), on, described injection channel (3) and described rotational structure body (1) have square to arrange, described combustion chamber (2) the working medium entrance with described injection channel (3) connects, and described air compression unit (4) includes row Thermal compression unit (41) and non-heat extraction compression unit (42), the pressure ratio of described heat extraction compression unit (41) More than 10, at the sender property outlet of described heat extraction compression unit (41), Temperature of Working is less than 373K, described non- The pressure ratio of heat extraction compression unit (42) is more than 5, the sender property outlet of described heat extraction compression unit (41) and institute State the working medium entrance connection of non-heat extraction compression unit (42), the working medium of described non-heat extraction compression unit (42) Outlet connects with described combustion chamber (2), and described rotational structure body (1) externally exports power.
2. turn a burn engine, including rotational structure body (1), combustion chamber (2), injection channel (3) With air compression unit (4), it is characterised in that: described combustion chamber (2) are arranged on described rotational structure body (1), on, described injection channel (3) and described rotational structure body (1) have square to arrange, described combustion chamber (2) the working medium entrance with described injection channel (3) connects, and described air compression unit (4) includes row Thermal compression unit (41) and non-heat extraction compression unit (42), the pressure ratio of described heat extraction compression unit (41) More than 10, at the sender property outlet of described heat extraction compression unit (41), Temperature of Working is less than 373K, described non- At the sender property outlet of heat extraction compression unit (42), Temperature of Working is higher than the fuel entering described combustion chamber (2) Ignition point, the sender property outlet of described heat extraction compression unit (41) and described non-heat extraction compression unit (42) The connection of working medium entrance, the sender property outlet of described non-heat extraction compression unit (42) and described combustion chamber (2) Connection, described rotational structure body (1) externally exports power.
3. turn a burn engine, including rotational structure body (1), combustion chamber (2), injection channel (3) With air compression unit (4), it is characterised in that: described combustion chamber (2) are arranged on described rotational structure body (1), on, described injection channel (3) and described rotational structure body (1) have square to arrange, described combustion chamber (2) the working medium entrance with described injection channel (3) connects, and described air compression unit (4) includes row Thermal compression unit (41) and non-heat extraction compression unit (42), the pressure ratio of described heat extraction compression unit (41) More than 10, at the sender property outlet of described heat extraction compression unit (41), Temperature of Working is less than 373K, described non- At the sender property outlet of heat extraction compression unit (42), Temperature of Working is higher than 1000K, described heat extraction compression unit (41) Sender property outlet connect with the working medium entrance of described non-heat extraction compression unit (42), described non-heat extraction compression is single The sender property outlet of unit (42) connects with described combustion chamber (2), burns in described combustion chamber (2) Chemical reaction, described rotational structure body (1) externally exports power.
4. turn a burn engine, including rotational structure body (1), combustion chamber (2), injection channel (3) With air compression unit (4), it is characterised in that: described combustion chamber (2) are arranged on described rotational structure body (1), on, described injection channel (3) and described rotational structure body (1) have square to arrange, described combustion chamber (2) the working medium entrance with described injection channel (3) connects, and described air compression unit (4) includes row Thermal compression unit (41) and non-heat extraction compression unit (42), the pressure ratio of described heat extraction compression unit (41) More than 10, at the sender property outlet of described heat extraction compression unit (41), Temperature of Working is less than 373K, described non- At the sender property outlet of heat extraction compression unit (42), Temperature of Working is higher than 1000K, described heat extraction compression unit (41) Sender property outlet connect with the working medium entrance of described non-heat extraction compression unit (42), described non-heat extraction compression is single The sender property outlet of unit (42) connects with described combustion chamber (2), and constant temperature occurs in described combustion chamber (2) Combustion chemistry is reacted, and described rotational structure body (1) externally exports power.
5. as according to any one of Claims 1-4, turn burn engine, it is characterised in that: described injection is led to Road (3) is set to jet pipe.
6. as according to any one of Claims 1-4, turn burn engine, it is characterised in that: described heat extraction pressure Contracting unit (41) is set to include the air injection unit of one-level displacement type compressor, at described displacement type compressor Cooler is set at sender property outlet;Or described heat extraction compression unit (41) is set to two-stage above displacement type compressor Air injection unit, set cooler at least one inter-stage, at the sender property outlet of displacement type compressor described in final stage Place sets cooler.
7. as according to any one of Claims 1-4, turn burn engine, it is characterised in that: described heat extraction pressure Contracting unit (41) is set to include the air injection unit of first-order rate type compressor, at described velocity profile compressor Cooler is set at sender property outlet;Or described heat extraction compression unit (41) is set to two-stage above velocity profile compressor Air injection unit, set cooler at least one inter-stage, at the sender property outlet of velocity profile compressor described in final stage Place sets cooler.
8. as according to any one of Claims 1-4, turn burn engine, it is characterised in that: described heat extraction pressure Contracting unit (41) is set to include the air injection unit of one stage impeller compressor, in the working medium of described impeller compressor Exit sets cooler;Or described heat extraction compression unit (41) is set to calming the anger of two-stage above impeller compressor Unit, sets cooler at least one inter-stage, sets cooling at the sender property outlet of impeller compressor described in final stage Device.
9. as according to any one of Claims 1-4, turn burn engine, it is characterised in that: described heat extraction pressure Contracting unit (41) is set to include the air injection unit of first stage piston formula compressor, at described piston compressor Cooler is set at sender property outlet;Or described heat extraction compression unit (41) is set to the above piston compressor of two-stage Air injection unit, set cooler at least one inter-stage, at the sender property outlet of piston compressor described in final stage Place sets cooler.
10. as according to any one of Claims 1-4, turn burn engine, it is characterised in that: described heat extraction Compression unit (41) is set to include the air injection unit of one-level spiral lobe compressor, at described spiral lobe compressor Sender property outlet at set cooler;Or described heat extraction compression unit (41) is set to the above screw of two-stage and calms the anger The air injection unit of machine, sets cooler at least one inter-stage, and the working medium at spiral lobe compressor described in final stage goes out Cooler is set at Kou.
11. turn burn engine as according to any one of Claims 1-4, it is characterised in that: described non-heat extraction Compression unit (42) is set to include one-level or the air injection unit of two-stage above displacement type compressor.
12. turn burn engine as according to any one of Claims 1-4, it is characterised in that: described non-heat extraction Compression unit (42) is set to include one-level or the air injection unit of two-stage above velocity profile compressor.
13. turn burn engine as according to any one of Claims 1-4, it is characterised in that: described non-heat extraction Compression unit (42) is set to include one-level or the air injection unit of two-stage above vane type compressor.
14. turn burn engine as according to any one of Claims 1-4, it is characterised in that: described non-heat extraction Compression unit (42) is set to include one-level or the air injection unit of the above piston compressor of two-stage.
15. turn burn engine as according to any one of Claims 1-4, it is characterised in that: described non-heat extraction Compression unit (42) is set to include one-level or the air injection unit of the above spiral lobe compressor of two-stage.
CN201410256319.0A 2013-08-07 2014-06-10 Turn burn engine Active CN104265504B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410256319.0A CN104265504B (en) 2013-08-07 2014-06-10 Turn burn engine

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
CN2013103411542 2013-08-07
CN201310341154.2 2013-08-07
CN201310341154 2013-08-07
CN201410256319.0A CN104265504B (en) 2013-08-07 2014-06-10 Turn burn engine

Publications (2)

Publication Number Publication Date
CN104265504A CN104265504A (en) 2015-01-07
CN104265504B true CN104265504B (en) 2016-08-24

Family

ID=52157061

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410256319.0A Active CN104265504B (en) 2013-08-07 2014-06-10 Turn burn engine

Country Status (1)

Country Link
CN (1) CN104265504B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108104942A (en) * 2016-10-29 2018-06-01 熵零技术逻辑工程院集团股份有限公司 A kind of solid fuel rotary power engine

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5282356A (en) * 1993-01-07 1994-02-01 Abell Irwin R Flywheel engine
US5408824A (en) * 1993-12-15 1995-04-25 Schlote; Andrew Rotary heat engine
CN102278233A (en) * 2010-07-07 2011-12-14 靳北彪 Supersonic rotor engine
CN102900535A (en) * 2011-09-08 2013-01-30 摩尔动力(北京)技术股份有限公司 Turbocharging gas turbine

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5282356A (en) * 1993-01-07 1994-02-01 Abell Irwin R Flywheel engine
US5408824A (en) * 1993-12-15 1995-04-25 Schlote; Andrew Rotary heat engine
CN102278233A (en) * 2010-07-07 2011-12-14 靳北彪 Supersonic rotor engine
CN102900535A (en) * 2011-09-08 2013-01-30 摩尔动力(北京)技术股份有限公司 Turbocharging gas turbine

Also Published As

Publication number Publication date
CN104265504A (en) 2015-01-07

Similar Documents

Publication Publication Date Title
CN105317484A (en) Method for saving energy by vacuum power
CN103397933B (en) Extreme heat machine and method of work thereof
CN104912691A (en) Internal combustion closed-loop hydrocarbon fuel thermo-motive system
CN104265504B (en) Turn burn engine
CN104832287B (en) Speed holds turbine engine
CN103867242B (en) Ultralow temperature heat-source engine
CN103994014B (en) Hydraulic system and use its vehicle
CN101787930A (en) Thermal circulation process of gas turbine based on pure oxygen or oxygen-enriched combustion
CN208686440U (en) The generating integrated biphase gas and liquid flow gravity heat engine of biphase gas and liquid flow gravity heat engine, wastewater treatment
CN203717159U (en) External-heating engine
CN104234834A (en) Turbine engine
CN109578098A (en) The Natural Gas Co-generation electrification technique of zero carbon emission
CN202811058U (en) Continuous combustion piston type internal combustion engine
CN203809128U (en) Constant-pressure heating thermodynamic cycling system of prime motor
CN103867335B (en) External combustion working medium heater
CN104791084A (en) Deep expansion internal combustion engine
CN104948339B (en) Displacement type splits engine
CN104879237B (en) Reciprocating-piston mechanism electromotor
CN105971765A (en) Bias engine
CN103775239B (en) Nearly constant temperature pressure low-temperature receiver heat engine
CN104131914A (en) Air-compressing nozzle propulsion engine
CN104863644B (en) Become boundary's hydraulic mechanism electromotor
CN104775902A (en) Multi-graded volume mechanism engine
CN105971756A (en) Air inlet structure of cryogenic air inlet type two-stroke engine
CN202690215U (en) Efficient thermo-power system

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
TR01 Transfer of patent right

Effective date of registration: 20201016

Address after: 221000 Ma Shan Village, Liguo Town, Tongshan District, Xuzhou City, Jiangsu Province

Patentee after: XUZHOU RUNFENG NEW MATERIALS Co.,Ltd.

Address before: 100101, Beijing, Chaoyang District Beiyuan Road, No. 168, Sheng Sheng building, 24 floor

Patentee before: MOLECULE POWER BEIJING TECH Co.