CN205955838U - Steam turbo formula internal -combustion engine - Google Patents

Steam turbo formula internal -combustion engine Download PDF

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Publication number
CN205955838U
CN205955838U CN201620841464.XU CN201620841464U CN205955838U CN 205955838 U CN205955838 U CN 205955838U CN 201620841464 U CN201620841464 U CN 201620841464U CN 205955838 U CN205955838 U CN 205955838U
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CN
China
Prior art keywords
air inlet
hybrid channel
turbine
combustion engine
combustion chamber
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Expired - Fee Related
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CN201620841464.XU
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Chinese (zh)
Inventor
李雷
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Individual
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Individual
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Priority to CN201620841464.XU priority Critical patent/CN205955838U/en
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Expired - Fee Related legal-status Critical Current
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Abstract

The utility model discloses a steam turbo formula internal -combustion engine, including compression mixing pipe way, the combustion chamber, the hybrid channel, turbine and power output system, the combustion chamber is provided with the combustion chamber air inlet, fire maker, water jet and combustion chamber gas outlet, compression mixing pipe says and links to each other with the combustion chamber air inlet, the water jet sets up at the combustion chamber top, the hybrid channel is provided with hybrid channel air inlet and hybrid channel gas outlet, the hybrid channel air inlet links to each other with the combustion chamber gas outlet, be spiral pathway between hybrid channel air inlet and the hybrid channel gas outlet, the turbine includes the turbine air inlet, output and gas vent, the hybrid channel gas outlet links to each other with the turbine air inlet, the output links to each other with power output system. The utility model discloses can improve the work efficiency of turbine formula internal -combustion engine, it is just whole small, can effectively reduce the energy consumption. The utility model discloses be fit for in the field wide application of small -size turbine formula internal -combustion engine.

Description

Steam boosting turbine type internal combustion engine
Technical field
This utility model is related to technical field of internal combustion engines, specifically a kind of steam boosting turbine type internal combustion engine.
Background technology
Current internal combustion engine mainly has internal-combustion piston engine and turbine type internal combustion engine, because internal-combustion piston engine is to utilize power The reverse torsion of square is completing three auxiliary movements, therefore power loss is larger, and the piston rod due to internal-combustion piston engine, song Three driving members of axle connect into "the" shape structure, and when internal combustion engine does work outburst high pressure, the arm of force did not really stretch, It is all tiltedly askew promotion, increased friction and pressure mill, greatly reduce the effectively utilizes of power, although therefore internal-combustion piston engine body Long-pending little, convenient, flexible, but less efficient, 30% about;And although the current turbine type internal combustion engine thermal efficiency is high, its structure Especially complex, volume is larger.
Utility model content
The technical problems to be solved in the utility model, is to provide a kind of steam boosting turbine type internal combustion engine, can solve the problem that existing There are the problems referred to above in the presence of technology.
For reaching above-mentioned purpose, the technical solution of the utility model is realized in:
A kind of steam boosting turbine type internal combustion engine, including compression gaseous mixture pipeline, combustor, hybrid channel, turbine and Power output system, described combustor is provided with air inlet of combustion chamber, fire maker, water jet and combustor gas outlet, described pressure Contracting gaseous mixture pipeline is connected with described air inlet of combustion chamber, and described water jet is arranged on described top of combustion chamber, and described mixing is led to Road is provided with hybrid channel air inlet and hybrid channel gas outlet, described hybrid channel air inlet and described combustor gas outlet phase Even, it is spirality channel between described hybrid channel air inlet and described hybrid channel gas outlet, described turbine includes turbine Machine air inlet, outfan and air vent, described hybrid channel gas outlet is connected with described turbine air inlet, described outfan with Described power output system is connected.
As restriction, also include air compressor and combustible mixing duct, the compression of described air compressor output is empty The combustible that gas is exported with described combustible mixing duct enters described compression gaseous mixture pipeline after mixing.
As further limiting, for gasoline, diesel oil, natural gas or ethanol in described combustible mixing duct.
Limit as another kind of, described water jet is uniformly arranged on described top of combustion chamber and sprays water for atomized water.
Limit as another kind of, described hybrid channel air inlet is arranged on the bottom of described mixing duct, described mixing is led to Road gas outlet is arranged on the top of described mixing duct.
Limit as another kind of, described fire maker is arranged on described combustor near described compression gaseous mixture pipeline side On the wall of side, described air inlet of combustion chamber is arranged on described top of combustion chamber and is located at the side near described fire maker.
Limit as another kind of, described air vent is arranged on the upside of described turbine.
As further limiting, described power output system is gear train.
This utility model due to employing above-mentioned structure, its compared with prior art, acquired technological progress is:
Mixed compression gaseous mixture is sprayed into combustor by compressing gaseous mixture pipeline by this utility model, then by striking sparks Device is lighted, and compression gaseous mixture, in burning Indoor Combustion, discharges a large amount of heat energy, then sprays atomization by the indoor water jet of burning Water, atomized water evaporates rapidly and heats up, and absorbs a large amount of heat energy, rapid spatial expansion, and produces high-temperature vapor, high-temperature vapor Enter hybrid channel with the high-temperature gas after fuel combustion, because hybrid channel is spiral type, can be sufficiently mixed, rear High Temperature High Pressure Gas enters turbine and promotes rotating turbine, and gas internal energy is converted into mechanical energy, drives power output system operating, complete The waste gas after acting is become to be discharged by air vent.This utility model by adopting said structure, can make internal combustion engine compact overall structure, Small volume, by hybrid channel is set to spiral type, can be sufficiently mixed gas further, improve working efficiency of internal combustion engine, fall Low energy expenditure, energy-conserving and environment-protective.
To sum up, this utility model structure is simple, disclosure satisfy that small volume, efficiency high, pollution is low, oil consumption is few internal combustion engine Demand, and good service behaviour can be reached.
Brief description
Accompanying drawing is used for providing further understanding to of the present utility model, and constitutes a part for description, with this practicality New embodiment is used for explaining this utility model together, does not constitute to restriction of the present utility model.
Fig. 1 is the steam boosting turbine type Structure of Internal-Combustion Engine schematic diagram described in this utility model embodiment;
Fig. 2 is the schematic diagram of another structure of steam boosting turbine type internal combustion engine described in the utility model.
In figure:1st, compress gaseous mixture pipeline;2nd, combustor;21st, air inlet of combustion chamber;22nd, combustor gas outlet;3rd, mix Passage;31st, hybrid channel air inlet;32nd, hybrid channel gas outlet;4th, turbine;41st, turbine air inlet;42nd, outfan; 43rd, air vent;5th, power output system;6th, air compressor;7th, combustible mixing duct.
Specific embodiment
With reference to the accompanying drawings and examples, this utility model is expanded on further.
In the following detailed description, only by way of explanation, some exemplary implementations of the present utility model are described Example.Undoubtedly, those of ordinary skill in the art will be consequently realised that, in the feelings without departing from spirit and scope of the present utility model Under condition, can by with various different in the way of described embodiment is modified.Therefore, accompanying drawing and description are inherently said Bright property, rather than be used for limiting scope of the claims.
As shown in figure 1, according to the steam boosting turbine type internal combustion engine of this utility model embodiment, including compression mixture pipe Road 1, combustor 2, hybrid channel 3, turbine 4 and power output system 5.
Combustor 2 is provided with air inlet of combustion chamber 21, fire maker, water jet and combustor gas outlet 22, compresses gaseous mixture Pipeline 1 is connected with described air inlet of combustion chamber 21, and water jet is arranged on described combustor 2 top, and hybrid channel 3 is provided with mixing Channel inlet mouth 31 and hybrid channel gas outlet 32, hybrid channel air inlet 31 is connected with combustor gas outlet 22, hybrid channel It is spirality channel between air inlet 31 and hybrid channel gas outlet 32, turbine 4 includes turbine air inlet 41, outfan 42 With air vent 43, hybrid channel gas outlet 32 is connected with turbine air inlet 41, and outfan 42 is connected with power output system 5.
In this utility model, by compressing gaseous mixture pipeline 1, mixed compression gaseous mixture is sprayed into combustor 2, so Lighted by fire maker afterwards, compression gaseous mixture burns in combustor 2, discharges a large amount of heat energy, then by the water jet in combustor 2 Spray atomized water, atomized water evaporates rapidly and heats up, absorb a large amount of heat energy, rapid spatial expansion, and produce high-temperature vapor, high High-temperature gas after temperature steam and fuel combustion enters hybrid channel 3, because hybrid channel 3 is spiral type, can be sufficiently mixed High temperature and high pressure gas enter turbine 4 and promote turbine 4 to rotate afterwards, and gas internal energy is converted into mechanical energy, drive power defeated Go out system 5 to operate, the waste gas after completing to do work is discharged by air vent 43, is so designed that, can make internal combustion engine compact overall structure, body Long-pending little, by hybrid channel 3 is set to spiral type, gas can be sufficiently mixed further, improve working efficiency of internal combustion engine, reduce Energy resource consumption, energy-conserving and environment-protective.
As another structure of the present embodiment, as shown in Fig. 2 it can also include air compressor 6 and combustible Mixing duct 7.The combustible that the compressed air of air compressor 6 output is exported with combustible mixing duct 7 enters pressure after mixing Contracting gaseous mixture pipeline 1.
In this utility model, by air compressor 6 compressed air, then combustible is mixed to compressed air, after mixing The mixture being formed passes through to compress gaseous mixture pipeline 1 entrance combustor 2, can improve the mixing efficiency of compressed air and combustible, And mix homogeneously, high combustion efficiency.
For gasoline, diesel oil, natural gas or ethanol in combustible mixing duct 7.
In embodiment of the present utility model, gasoline, diesel oil, natural gas or ethanol have preferable combustion efficiency, can make combustion Burn high-temperature vapor rapid spatial expansion in room 2, improve turbine 4 rotational efficienty.
Water jet is uniformly arranged on described combustor 2 top and sprays water for atomized water.So, by pushing up in combustor 2 Portion is uniformly arranged water jet, and sprays atomized water, atomized water evaporation rate can be made fast, atomized water absorbs a large amount of heat energy, volume is swollen Swollen rapid.
Hybrid channel air inlet 31 is arranged on the bottom of mixing duct 3, and hybrid channel gas outlet 32 is arranged on mixing duct 3 Top.So, the high-temperature gas after hybrid channel 3 bottom is passed through high-temperature vapor and fuel combustion, mixed gas are passed through Spirality channel is discharged from hybrid channel 3 top, can lengthen spiral type hybrid channel length, makes the more equal of mixed gas mixing It is expelled to turbine 4 after even, improve turbine 4 work efficiency further.
Fire maker is arranged on described combustor 2 on the side wall stating compression gaseous mixture pipeline 1 side, air inlet of combustion chamber 21 are arranged on combustor 2 top and are located at the side near fire maker.It is arranged such, can make that air inlet of combustion chamber 21 is passed through is mixed Close gas directly to light by fire maker, conveniently light.
Air vent 43 is arranged on the upside of described turbine 4.
Power output system 5 is gear train.
Therefore, mixed compression gaseous mixture is sprayed into combustor 2 by compressing gaseous mixture pipeline 1 by this utility model, so Lighted by fire maker afterwards, compression gaseous mixture burns in combustor 2, discharges a large amount of heat energy, then by the water jet in combustor 2 Spray atomized water, atomized water evaporates rapidly and heats up, absorb a large amount of heat energy, rapid spatial expansion, and produce high-temperature vapor, high High-temperature gas after temperature steam and fuel combustion enters hybrid channel 3, because hybrid channel 3 is spiral type, can be sufficiently mixed High temperature and high pressure gas enter turbine 4 and promote turbine 4 to rotate afterwards, and gas internal energy is converted into mechanical energy, drive power defeated Go out system 5 to operate, the waste gas after completing to do work is discharged by air vent 43, can make internal combustion engine compact overall structure, small volume, pass through Hybrid channel 3 is set to spiral type, gas can be sufficiently mixed further, improve working efficiency of internal combustion engine, reduce energy resource consumption, Energy-conserving and environment-protective.
Steam boosting turbine type internal combustion engine small volume of the present utility model, efficiency high, pollute simultaneously low, consumption lubricating oil few, Durable in use.
The foregoing is only the schematic specific embodiment of this utility model, be not limited to model of the present utility model Enclose.Any those skilled in the art, the equivalent change made on the premise of without departing from design of the present utility model and principle Change and modification, the scope of this utility model protection all should be belonged to.

Claims (8)

1. a kind of steam boosting turbine type internal combustion engine it is characterised in that:It includes compressing gaseous mixture pipeline, combustor, mixes and lead to Road, turbine and power output system, described combustor is provided with air inlet of combustion chamber, fire maker, water jet and combustor and goes out QI KOU, compression gaseous mixture pipeline is connected with air inlet of combustion chamber, and water jet is arranged on top of combustion chamber, and hybrid channel is provided with mixed Close channel inlet mouth and hybrid channel gas outlet, hybrid channel air inlet is connected with combustor gas outlet, hybrid channel air inlet It is spirality channel and the gas outlet of hybrid channel between, turbine includes turbine air inlet, outfan and air vent, and mixing is logical Road gas outlet is connected with turbine air inlet, and outfan is connected with power output system.
2. steam boosting turbine type internal combustion engine according to claim 1 it is characterised in that:It also include air compressor and Combustible mixing duct, the combustible that the compressed air that air compressor exports is exported with combustible mixing duct enters after mixing Compression gaseous mixture pipeline.
3. steam boosting turbine type internal combustion engine according to claim 2 it is characterised in that:In described combustible mixing duct For gasoline, diesel oil, natural gas or ethanol.
4. steam boosting turbine type internal combustion engine according to claim 1 and 2 it is characterised in that:Water jet is uniformly arranged on Top of combustion chamber and spray water be atomized water.
5. steam boosting turbine type internal combustion engine according to claim 1 and 2 it is characterised in that:Hybrid channel air inlet sets Put the bottom in mixing duct, hybrid channel gas outlet is arranged on the top of mixing duct.
6. steam boosting turbine type internal combustion engine according to claim 1 and 2 it is characterised in that:Fire maker is arranged on burning On the side wall of compression gaseous mixture pipeline side, air inlet of combustion chamber is arranged on top of combustion chamber and is located near fire maker for room Side.
7. steam boosting turbine type internal combustion engine according to claim 1 and 2 it is characterised in that:Air vent is arranged on described On the upside of turbine.
8. steam boosting turbine type internal combustion engine according to claim 1 and 2 it is characterised in that:Power output system is tooth Wheel system.
CN201620841464.XU 2016-08-05 2016-08-05 Steam turbo formula internal -combustion engine Expired - Fee Related CN205955838U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620841464.XU CN205955838U (en) 2016-08-05 2016-08-05 Steam turbo formula internal -combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620841464.XU CN205955838U (en) 2016-08-05 2016-08-05 Steam turbo formula internal -combustion engine

Publications (1)

Publication Number Publication Date
CN205955838U true CN205955838U (en) 2017-02-15

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Family Applications (1)

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Country Status (1)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106089436A (en) * 2016-08-05 2016-11-09 李雷 Steam boosting turbine type internal combustion engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106089436A (en) * 2016-08-05 2016-11-09 李雷 Steam boosting turbine type internal combustion engine

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C14 Grant of patent or utility model
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CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20170215

Termination date: 20180805

CF01 Termination of patent right due to non-payment of annual fee