CN102003284A - Hydrogen-blended gas fuel engine - Google Patents
Hydrogen-blended gas fuel engine Download PDFInfo
- Publication number
- CN102003284A CN102003284A CN 201010590793 CN201010590793A CN102003284A CN 102003284 A CN102003284 A CN 102003284A CN 201010590793 CN201010590793 CN 201010590793 CN 201010590793 A CN201010590793 A CN 201010590793A CN 102003284 A CN102003284 A CN 102003284A
- Authority
- CN
- China
- Prior art keywords
- combustion chamber
- hydrogen
- impeller
- gun
- main combustion
- 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.)
- Granted
Links
Images
Abstract
The invention discloses a hydrogen-blended gas fuel engine, which is characterized in that the hydrogen-blended gas fuel engine comprises an impeller assembly for a steam turbine, and the impeller assembly consists of a shell, an impeller shaft and an impeller; jetting inlets uniformly distributed on the outer circumference surface of the impeller in the shell are respectively provided with a corresponding jetting gun, and muzzles of the jetting guns correspond to blades of the impeller; the jetting gun is composed of a main combustion chamber, a subsidiary combustion chamber, and an airflow guide gun-barrel, wherein a hydrogen nozzle and an igniter are arranged on the rear wall of the ellipsoidal subsidiary combustion chamber, the front part of the subsidiary combustion chamber is connected with an inlet at one end of a long axis of the main combustion chamber with an ellipsoidal inner wall by a collapsible tube, an outlet at the other end of the long axis of the main combustion chamber is connected with an arc airflow guide gun-barrel, and an end part of the guide gun-barrel is provided with a muzzle; and a compressed air nozzle is arranged on the outlet chamber wall of the main combustion chamber, and a high-temperature vaporized gas nozzle is arranged on the wall of the main combustion chamber. The hydrogen-blended gas fuel engine of the invention has the advantages of reasonable structure, simple control process, stable fuel combustion, stable power output, less hydrogen dosage, high output power, less mechanical components, no complicated lubricating system, and capability of simplifying the mechanical structure and improving energy conversion efficiency, and is simple in maintenance.
Description
Technical field
The invention belongs to employing with the power engine of hydrogen, particularly hydrogen mixed gas fuels and energy machine with relevant gas fuel combination.
Background technique
Traditional combustion power machine complicated in mechanical structure, mechanical engagement part precision prescribed height, lubrication system complexity.Combustion power machine whole control process is very complicated, and mechanical loss is big, and mechanical efficiency is low.And behind the use hydrogen fuel, pure hydrogen power engine output power is low, and optimization fuel and mixing can make control procedure more complicated, require higher, there is significant limitation in the hydrogen fuel power machine of research at present, occurs pre-ignition or abnormal combustion in the course of the work, causes power output lower or unstable, lack practicability, and be difficult to promote.
Summary of the invention
The object of the present invention is to provide a kind of hydrogen mixed gas fuels and energy machine, simplified mechanical structure, it is rational in infrastructure, and control procedure is fairly simple, fuel combustion is stable, can improve the conversion efficiency of energy, power output is stable, and hydrogen usage is few, the output power height, mechanical assembly is few, and is easy to maintenance, need not to adopt complicated lubrication system.
The object of the present invention is achieved like this: a kind of hydrogen mixed gas fuels and energy machine, comprise the turbine rotor group, by casing, impeller shaft and impeller constitute, the uniform jet ingress of impeller outer peripheral surface is being provided with corresponding ejecting gun respectively in casing, the spray gun port of ejecting gun is corresponding with impeller blade, ejecting gun is by the master, the gentle conductance of subsidiary combustion chamber constitutes to gun barrel, hydrogen nozzle and igniter that the hydrogen suction tude connects are being set on the rear wall of axiolitic subsidiary combustion chamber, the front portion of subsidiary combustion chamber is connecting the longitudinal end inlet that inwall is axiolitic main combustion chamber by collapsible tube, the outlet of the main combustion chamber major axis the other end is connecting and is being camber line shape air-flow guiding gun barrel, guiding gun barrel end is being provided with spray gun port, the compressed-air atomizer that compressed air inlet pipe connects is being set on the outlet locular wall of main combustion chamber, the vaporization gas nozzle that high-temperature evaporation gas steam inlet pipe connects is being set on the locular wall of main combustion chamber.
The present invention is that the high-temperature high-pressure air flow that is sprayed by A gas injection lance promotes impeller rotation acting.Its working procedure is: earlier pressurized air is fed in the main combustion chamber, charging into the compressed-air actuated while to subsidiary combustion chamber, pressurized air also flows to the guiding gun barrel, after pressurized air impacts muzzle, spray into impeller blade and casing by mechanical seal and the formed static air pressure sealing of pressurized gas, form a complete relatively relative seal space, make the increased pressure of subsidiary combustion chamber, also in gun barrel, form the vent plug that density is very high simultaneously.This moment, hydrogen was sprayed into subsidiary combustion chamber, when ever-increasing hydrogen and pressurized air mix, lighted by igniter and produce detonation, mixed gas is in the process of subsidiary combustion chamber reaction, temperature and pressure is also constantly increasing, and spread to the muzzle direction, at this moment in main combustion chamber, spray into the water vapor of high-temperature evaporation, the water vapor that is in the thermolysis transition point is further vaporized by high temperature in main combustion chamber and is decomposited hydrogen and oxygen, further mix, burning, chemical reaction process repeatedly discharges higher temperature and pressure, and high-energy fluid impacts muzzle and promotes the impeller rotation.After impeller turns over a tooth phase angle when the second tooth position, just entered between the relative sealing merit of next acting, carrying out above-mentioned hydrogen and pressurized air mixes, igniter is lighted detonation, and high-temperature water vapor decomposes in main combustion chamber, mixes, the process of burning, the active force of detonation gas generation continuously continuously promotes follow-up blade continuously works impeller.Waste gas is discharged from relief opening, participates in the process of producing of high-temperature water vapor or enters steam generating system.Hydrogen is to split water into hydrogen and oxygen by hydrogen generator, sends in the different ejecting guns by distributor after the hydrogen pump pressurization through the hydrogen after cooling.High-temperature water vapor sprays into ejecting gun by high-pressure service pump pressurization back vaporization.
Key problem in technology of the present invention is that mixed gas forms certain first pressing in sufficiently long gun barrel, ignite the source by very a spot of hydrogen as High Temperature High Pressure, and in a single day formed the vent plug of high pressure high density by supercharging repeatedly through reaction repeatedly, will produce bigger impulse force to load.Though appearances such as the chemical reaction that is taken place in ejecting gun approaches compression adds the adiabatic expansion process, but the rear end is because the length and the formed vent plug of pressurized air of gun barrel, the last ejecting gun outlet pressure of its process remains approximate isopiestic process, but right-about has taken place in its energy properties, this mainly is that pressurized air has not only produced mixing of first pressing and hydrogen, improved the burning energy of hydrogen, also reduce simultaneously the reacting dose and the rapid diffusion of hydrogen, the more important thing is the density that has increased mixed gas in the gun barrel.
The present invention has simplified mechanical structure, and it is rational in infrastructure, and control procedure is fairly simple, and fuel combustion is stable, improved the conversion efficiency of energy, power output is stable, and hydrogen usage is few, the output power height, mechanical assembly is few, and is easy to maintenance, need not to adopt complicated lubrication system.
Description of drawings
The invention will be further described below in conjunction with accompanying drawing, and accompanying drawing is a structural representation of the present invention.
Embodiment
A kind of hydrogen mixed gas fuels and energy machine, as shown in drawings, comprise the turbine rotor group, by casing, impeller shaft and impeller constitute, the uniform jet ingress of impeller 1 outer peripheral surface is being provided with corresponding ejecting gun 11 in casing, the spray gun port of ejecting gun 11 is corresponding with impeller blade 2, ejecting gun 11 is by the master, subsidiary combustion chamber 7,8 gentle conductances constitute to gun barrel 5, hydrogen nozzle 10 and igniter 9 that the hydrogen suction tude connects are being set on the rear wall of axiolitic subsidiary combustion chamber 8, the front portion of subsidiary combustion chamber 8 is connecting the longitudinal end inlet that inwall is axiolitic main combustion chamber 7 by collapsible tube, the outlet of the main combustion chamber 7 major axis the other ends is connecting and is being camber line shape air-flow guiding gun barrel 5, guiding gun barrel 5 ends are being provided with spray gun port, the compressed-air atomizer 6 that compressed air inlet pipe connects is being set on the outlet locular wall of main combustion chamber 7, the vaporization gas nozzle 16 that high-temperature evaporation gas steam inlet pipe connects is being set on the locular wall of main combustion chamber 7.The place ahead of uniform ejecting gun guiding gun barrel 5 is being provided with detonation chamber 3 respectively in casing, and detonation chamber 3 its small ends that inwall resembles a pear in shape are being provided with jetburner and are matching with impeller blade 2.On the hydrogen air inlet pipeline that subsidiary combustion chamber hydrogen nozzle 10 connects, distributor 13 and one-way valve 12 are being set.On the hydrogen air inlet pipeline that high-temperature evaporation gas nozzle 16 connects, distributor 15 and one-way valve 14 are being set.Uniform 2-10 impellers 1 that are installed with on turbine shaft are separated by the dividing plate that is provided with between the uniform impeller 1.Uniform 3-12 ejecting guns 11 that are being provided with on the casing of every impeller 1 circumference.On the compressed air inlet pipe road that compressed-air atomizer 6 connects, distributor 17 and one-way valve 18 are being set.
Claims (7)
1. hydrogen mixed gas fuels and energy machine, comprise the turbine rotor group, by casing, impeller shaft and impeller constitute, it is characterized in that: the uniform jet ingress of impeller in casing (1) outer peripheral surface is being provided with corresponding ejecting gun (11) respectively, the spray gun port of ejecting gun (11) is corresponding with impeller blade (2), ejecting gun (11) is by the master, subsidiary combustion chamber (7,8) gentle conductance constitutes to gun barrel (5), hydrogen nozzle (10) and igniter (9) that the hydrogen suction tude connects are being set on the rear wall of axiolitic subsidiary combustion chamber (8), the front portion of subsidiary combustion chamber (8) is connecting the longitudinal end inlet that inwall is axiolitic main combustion chamber (7) by collapsible tube, the outlet of main combustion chamber (7) the major axis the other end is connecting and is being camber line shape air-flow guiding gun barrel (5), guiding gun barrel (5) end is being provided with spray gun port, the compressed-air atomizer (6) that compressed air inlet pipe connects is being set on the outlet locular wall of main combustion chamber (7), the vaporization gas nozzle (16) that high-temperature evaporation gas steam inlet pipe connects is being set on the locular wall of main combustion chamber (7).
2. hydrogen mixed gas fuels and energy machine according to claim 1, it is characterized in that: the place ahead of uniform ejecting gun guiding gun barrel (5) is being provided with detonation chamber (3) respectively in casing, and its small end of detonation chamber (3) that inwall resembles a pear in shape is being provided with jetburner and is matching with impeller blade (2).
3. hydrogen mixed gas fuels and energy machine according to claim 1 is characterized in that: on the hydrogen air inlet pipeline that subsidiary combustion chamber hydrogen nozzle (10) connects distributor (13) and one-way valve (12) are being set.
4. hydrogen mixed gas fuels and energy machine according to claim 1 is characterized in that: on the vaporization gas admission passage that high-temperature evaporation gas nozzle (16) connects distributor (15) and one-way valve (14) are being set.
5. hydrogen mixed gas fuels and energy machine according to claim 1 is characterized in that: uniform 2-10 impellers (1) that are installed with on turbine shaft, separate by the dividing plate that is provided with between the uniform impeller (1).
6. hydrogen mixed gas fuels and energy machine according to claim 1 is characterized in that: uniform 3-12 ejecting guns (11) that are being provided with on the casing of every impeller (1) circumference.
7. hydrogen mixed gas fuels and energy machine according to claim 1 is characterized in that: on the compressed air inlet pipe road that compressed-air atomizer (6) connects distributor (17) and one-way valve (18) are being set.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201010590793 CN102003284B (en) | 2010-12-16 | 2010-12-16 | Hydrogen-blended gas fuel engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201010590793 CN102003284B (en) | 2010-12-16 | 2010-12-16 | Hydrogen-blended gas fuel engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN102003284A true CN102003284A (en) | 2011-04-06 |
| CN102003284B CN102003284B (en) | 2013-03-06 |
Family
ID=43810936
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201010590793 Expired - Fee Related CN102003284B (en) | 2010-12-16 | 2010-12-16 | Hydrogen-blended gas fuel engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102003284B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103343712A (en) * | 2013-04-09 | 2013-10-09 | 罗厚兵 | Gear-type engine |
| CN114486273A (en) * | 2021-12-27 | 2022-05-13 | 国网浙江省电力有限公司电力科学研究院 | Park flexibility reforms transform unit hydrogen and burns test device thoughtlessly |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1144045A (en) * | 1951-10-17 | 1957-10-08 | Mototecnica Soc | Improvements to turbojets and gas turbines, particularly for the propulsion of air, land and marine vehicles |
| US3321911A (en) * | 1965-02-12 | 1967-05-30 | Myles Tommie Lynn | Gas turbine engine with rotating combustion chamber |
| FR2680385A1 (en) * | 1991-08-12 | 1993-02-19 | Rignault Jean | Turbine engine with orthogonal circular reaction |
| US5636509A (en) * | 1995-10-20 | 1997-06-10 | Abell; Irwin R. | Flywheel engine improvements |
| CA2426353A1 (en) * | 2003-04-25 | 2004-10-25 | Klaus Eduard Schmid | Hydrogen turbine |
| CN201884128U (en) * | 2010-12-16 | 2011-06-29 | 梁屹 | Hydrogen-mixed gas fuel power machine |
-
2010
- 2010-12-16 CN CN 201010590793 patent/CN102003284B/en not_active Expired - Fee Related
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1144045A (en) * | 1951-10-17 | 1957-10-08 | Mototecnica Soc | Improvements to turbojets and gas turbines, particularly for the propulsion of air, land and marine vehicles |
| US3321911A (en) * | 1965-02-12 | 1967-05-30 | Myles Tommie Lynn | Gas turbine engine with rotating combustion chamber |
| FR2680385A1 (en) * | 1991-08-12 | 1993-02-19 | Rignault Jean | Turbine engine with orthogonal circular reaction |
| US5636509A (en) * | 1995-10-20 | 1997-06-10 | Abell; Irwin R. | Flywheel engine improvements |
| CA2426353A1 (en) * | 2003-04-25 | 2004-10-25 | Klaus Eduard Schmid | Hydrogen turbine |
| CN201884128U (en) * | 2010-12-16 | 2011-06-29 | 梁屹 | Hydrogen-mixed gas fuel power machine |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103343712A (en) * | 2013-04-09 | 2013-10-09 | 罗厚兵 | Gear-type engine |
| CN103343712B (en) * | 2013-04-09 | 2016-03-02 | 罗厚兵 | gear type engine |
| CN114486273A (en) * | 2021-12-27 | 2022-05-13 | 国网浙江省电力有限公司电力科学研究院 | Park flexibility reforms transform unit hydrogen and burns test device thoughtlessly |
Also Published As
| Publication number | Publication date |
|---|---|
| CN102003284B (en) | 2013-03-06 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN110718843B (en) | Air-breathing type continuous rotation detonation combustion driven premixing type carbon dioxide pneumatic laser | |
| CN102619645A (en) | Charge engine injected with low-entropy mixed-combustion liquefied gas | |
| WO2014152320A4 (en) | Power-producing apparatus and method | |
| CN110067637A (en) | The air supply system of gas engine pre-burning component, the cylinder containing the component and cylinder | |
| CN102003284B (en) | Hydrogen-blended gas fuel engine | |
| CN201884128U (en) | Hydrogen-mixed gas fuel power machine | |
| CN101825041B (en) | Gas piston pulse engine | |
| CN102619642B (en) | Efficient turbojet engine | |
| CN102606343B (en) | Detonation chamber of pulse detonation engine | |
| CN103512047A (en) | Radial rotational flow double fuel nozzle for chemical regenerative cycle | |
| CN101382292B (en) | Alcohol based burning machine, alcohol based combustion nozzle thereof and pneumatic power shearing knife | |
| CN201991616U (en) | Scramjet double-working substance steam turbine | |
| CN209228489U (en) | A kind of clean energy resource water circulation zero-discharging rocket engine burner electricity generation system | |
| CN203717126U (en) | Turbine engine | |
| CN112211724A (en) | Engine and aircraft | |
| CN219529158U (en) | Vortex double-spray synergistic gas turbine capable of preventing extreme high temperature | |
| CN103775201A (en) | Impeller engine using regenerative propellant | |
| CN201103494Y (en) | Air injection rotor engine | |
| RU70965U1 (en) | KNOCK POWER INSTALLATION | |
| CN109268169A (en) | A kind of clean energy resource water circulation zero-discharging rocket engine burner electricity generation system | |
| CN117189316A (en) | Energy recovery system and car | |
| RU2236610C2 (en) | Jet engine | |
| WO2017015775A1 (en) | Internal combustion engine using water as auxiliary power | |
| CN219762320U (en) | Portable pulse smoke sprayer capable of spraying smoke rapidly | |
| CN220892230U (en) | Fire pumping device and burner using same |
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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130306 Termination date: 20191216 |