CN108412615A - Vortex-spraying type power generation combustor - Google Patents
Vortex-spraying type power generation combustor Download PDFInfo
- Publication number
- CN108412615A CN108412615A CN201810377764.0A CN201810377764A CN108412615A CN 108412615 A CN108412615 A CN 108412615A CN 201810377764 A CN201810377764 A CN 201810377764A CN 108412615 A CN108412615 A CN 108412615A
- Authority
- CN
- China
- Prior art keywords
- shell
- exhaust
- air
- gas
- tail end
- 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.)
- Pending
Links
- 238000005507 spraying Methods 0.000 title claims abstract description 16
- 238000010248 power generation Methods 0.000 title abstract description 8
- 230000005611 electricity Effects 0.000 claims abstract description 21
- 239000000446 fuel Substances 0.000 claims abstract description 21
- 230000008878 coupling Effects 0.000 claims abstract description 9
- 238000010168 coupling process Methods 0.000 claims abstract description 9
- 238000005859 coupling reaction Methods 0.000 claims abstract description 9
- 239000007789 gas Substances 0.000 claims description 76
- 238000002485 combustion reaction Methods 0.000 claims description 29
- 238000009423 ventilation Methods 0.000 claims description 16
- 241000883990 Flabellum Species 0.000 claims description 11
- 239000010763 heavy fuel oil Substances 0.000 claims description 9
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 8
- 239000001301 oxygen Substances 0.000 claims description 8
- 229910052760 oxygen Inorganic materials 0.000 claims description 8
- 239000003921 oil Substances 0.000 claims description 4
- 239000007921 spray Substances 0.000 claims description 4
- 231100000331 toxic Toxicity 0.000 claims description 4
- 230000002588 toxic effect Effects 0.000 claims description 4
- 125000006850 spacer group Chemical group 0.000 claims description 3
- 241001075561 Fioria Species 0.000 claims 1
- 206010016766 flatulence Diseases 0.000 description 2
- 230000008450 motivation Effects 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000000567 combustion gas Substances 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000004992 fission Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000001727 in vivo Methods 0.000 description 1
- 230000000505 pernicious effect Effects 0.000 description 1
- 231100000614 poison Toxicity 0.000 description 1
- 230000007096 poisonous effect Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/057—Control or regulation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Abstract
The present invention relates to vortex-spraying type power generation combustors, including shell, the flange being set on shell, tail end exhaust driven gas turbine, air inlet turbofan, the shell one end are suction end, and the other end is exhaust end；It is cavity structure in the shell, shell suction end is that opening is arranged with exhaust end, center is worn there are one main shaft in the shell, main shaft one end is equipped with air inlet turbofan, the main shaft other end is equipped with tail end exhaust driven gas turbine, and fuel feeding duct and nozzle are equipped in shell, ignition system is additionally provided in shell, it is equipped with shaft coupling in main shaft one end, shaft coupling is by exporting one generator of axis connection.By turbine design shape air-breathing and jet, to form turbine, and then main shaft rotation is driven, the main shaft of rotation provides torque to generator, and generator is made to send out electricity.
Description
Technical field
The present invention relates to a kind of vortex-spraying type power generation combustors, belong to heat, Electricity Federation is total to field.
Background technology
Generator is the mechanical equipment at electric energy by the energy conversion of other forms, it is by the hydraulic turbine, steam turbine, diesel engine
Or the driving of other dynamic power machines, it converts the energy that flow, air-flow, fuel combustion or nuclear fission generate to mechanical energy and is transmitted to
Generator, then electric energy is converted to by generator.The combustion powered of current fuel-fired power generation mode is usually active rotation, i.e.,
Fuel feed system generally use exterior power drives main shaft to rotate to form active rotation, and power is provided by combustion gas to piston
Body is discharged；Power is provided by oil spout, provides torque to generator, and then generator is made to send out electricity；And due to fuel combustion
When the air capacity that enters it is different, air burn incompletely and high-temp combustion will produce the pernicious gases such as CO, NOx after combustion, make
At seriously polluted and harm health.
Invention content
In order to provide torque to generator, generator is set to send out electricity, the object of the present invention is to provide a kind of sprays of whirlpool
Formula power generation combustor so as to control the ability of burning, and then is fired by turbine design shape air-breathing and jet by fuel
The gas that burning generates drives line shaft rotation to be finally reached generator and sends out electricity, while providing thermal energy.
To achieve the goals above, the technical solution adopted in the present invention is：Vortex-spraying type power generation combustor, including shell,
Flange, tail end exhaust driven gas turbine, air inlet turbofan, the shell one end being set on shell are suction end, and the other end is exhaust end；
It is cavity structure in the shell, shell suction end is that opening is arranged with exhaust end, and center wears that there are one main in the shell
Axis, main shaft one end are equipped with air inlet turbofan, and the main shaft other end is equipped with tail end exhaust driven gas turbine, fuel feeding duct, shell are equipped in shell
It is additionally provided with ignition system in vivo；It is equipped with shaft coupling in main shaft one end, shaft coupling is by exporting on one motor of axis connection；
The tail end exhaust driven gas turbine and air inlet turbofan is the exhaust flabellum with angle of inclination.
The exhaust driven gas turbine and each self-forming multilayered structure gas vent of air inlet turbofan.
The tail end exhaust driven gas turbine is different with the angle of inclination of air inlet turbofan gas vent；The tail end exhaust driven gas turbine
The inclined direction of exhaust level is flaring according to gas guide direction；The inclined direction of the exhaust level of the air inlet turbofan is according to gas
Body guide direction is to close up towards housing cavity；
The blade quantity of the tail end exhaust driven gas turbine exhaust flabellum is less than the exhaust flabellum of air inlet turbofan；
By turbine design shape air-breathing and jet, to form turbine, the rotation of gas push turbine, and then main shaft rotation is driven
Turn, the main shaft of rotation provides torque to generator, so that generator is sent out electricity, while providing thermal energy；
Further, it is boundary with main shaft in housing hollow, is respectively equipped with spacer structure successively, the housing cavity is divided into three
Layer channel form, including separate ventilation road, combustion chamber and central ventilation road；
The oil spout into combustion chamber from fuel feed pipe, by ignition system fires, Indoor Combustion of burning, gas drastically expands, swollen
Flatulence body is discharged by tail end rapidly, since tail end exhaust driven gas turbine angle and quantity are less than the quantity of air inlet turbofan, is made swollen after burning
Flatulence body overcomes pressure acting to be forced caudad discharge directions discharge, forms turbine, the rotation of gas push turbine；Turbine rotates
After coming, air inlet turbofan absorbs air from outside, is mixing air, a large amount of gas when air is drawn into combustion chamber, the combustion chamber in
Body and flame drive turbine rotation to spray, this part is burn incompletely, not will produce toxic and harmful gas；When air is absorbed
To central ventilation road, central ventilation road is cold air, and the unburnt gas of ejection, oxygen has exhausted, but the inside also has
Part of fuel provides oxygen when after by tail end exhaust driven gas turbine to before shell exhaust end marginal position by center air duct,
Residual fuel is ignited by secondary, and residual fuel is formed abundant burning by this part again, in order to avoid generate toxic and harmful gas；Work as sky
After gas absorbs arrival tail end exhaust driven gas turbine from separate ventilation road, to shell exhaust end marginal position after by tail end exhaust driven gas turbine
When before, progress is secondary to ignite, and equally, residual fuel is formed abundant burning by this part again, in order to avoid generate poisonous and harmful gas
Body；Finally, reach after the fuel combustion in shell and cmpletely burn, the safe gas after burning is subjected to extraneous emptying, is subtracted
Few atmosphere pollution.
Further, in order to more preferably realize the ability of control flame combustion, air inflow is equipped in air inlet turbofan outer end
Damper is pumped into outside air and provides oxygen；
The upper and lower side of the air inflow damper connect with the upper and lower side of shell suction end and is equipped with gap respectively；
The air inflow damper open up the independent open-celled structure of multilayer, it can be achieved that part layer trepanning opening and closing, lead to
The size of air door open cell content is overregulated, the abundant degree of fuel combustion, and then the size of control mode can be controlled, it is final to control
The generated energy of generator.
Advantageous effect caused by the technical solution adopted in the present invention is：
By turbine design shape air-breathing and jet, to form turbine, and then main shaft rotation is driven, the main shaft of rotation is to power generation
Machine provides torque, and generator is made to send out electricity；By the inner cavity of layered structure, reaching different ventilating ducts can realize that fuel fully fires
It burns, reaches no pollution discharge；The design of air inflow damper from main regulation by realizing that the number of openings controls the big of intake
It is small, it is therefore an objective to control the ability of flame.
Description of the drawings
Fig. 1 is the structural diagram of the present invention.
In figure, 1, flange, 2, tail end exhaust driven gas turbine, 3, fuel feeding duct, 4, ignition system, 5, shell, 6, into gas eddy
Fan, 7, air inflow damper.8, main shaft, 9, central ventilation road, 10, combustion chamber, 11, separate ventilation road, 12, shaft coupling, 13, electricity
Motivation, 14, output shaft.
Specific implementation mode
The present invention will be described in detail with reference to the accompanying drawings.In figure, vortex-spraying type generator, including shell 5, it is set to shell
On flange 1, tail end exhaust driven gas turbine 2, air inlet turbofan 6,5 one end of the shell be suction end, the other end is exhaust end；The shell
It is cavity structure in body 5, shell inlet end is that opening is arranged with exhaust end, and center is worn there are one main shaft 8 in the shell 5,
8 one end of main shaft is equipped with air inlet turbofan 6, and 8 other end of main shaft is equipped with tail end exhaust driven gas turbine 2, fuel feeding duct 3 is equipped in shell 5,
Ignition system 4 is additionally provided in shell 5；It is equipped with shaft coupling 12 in 8 one end of main shaft, shaft coupling 12 connects an electricity by output shaft 14
13 in motivation；
The tail end exhaust driven gas turbine 2 and air inlet turbofan 6 is the exhaust flabellum with angle of inclination.
6 each self-forming multilayered structure gas vent of the exhaust driven gas turbine 2 and air inlet turbofan.
The tail end exhaust driven gas turbine 2 is vented exhaust flabellum of the blade quantity less than air inlet turbofan 6 of flabellum；
The tail end exhaust whirlpool 2 wheel exhaust flabellum is 2 layers, and the exhaust flabellum of the air inlet turbofan 6 is 3 layers,
By turbine design shape air-breathing and jet, to form turbine, the rotation of gas push turbine, and then main shaft rotation is driven
Turn, the main shaft of rotation provides torque to generator, and generator is made to send out electricity；
Further, it is boundary with main shaft in 5 cavity of shell, is respectively equipped with spacer structure successively, the housing cavity is divided into
Three layers of channel form, including separate ventilation road 11, combustion chamber 10 and central ventilation road 9；
It from the oil spout into combustion chamber 10 of fuel feed pipe 3, is lighted a fire by ignition system 4, burning, gas are drastically swollen in combustion chamber 10
It is swollen, since tail end exhaust driven gas turbine angle and quantity are less than the quantity of air inlet turbofan, make the gas expanded after burning that pressure be overcome to do
Work(is forced caudad discharge directions discharge, forms turbine, the rotation of gas push turbine；After turbine rotates, air inlet turbofan 6 from
Outside absorbs air, is mixing air, a large amount of gas and fire drive turbine when air is drawn into combustion chamber 10, the combustion chamber in
Rotation sprays, this part is burn incompletely；When air is absorbed into central ventilation road 9, central ventilation road 9 is cold air, no
Completely burned, oxygen has exhausted gas, but there be part of fuel the inside, is vented to shell after by tail end exhaust driven gas turbine
When before end margin position, residual fuel is ignited by secondary, and residual fuel is formed abundant burning by this part again, in order to avoid generate
Toxic and harmful gas；When air from separate ventilation road 11 suck reach tail end exhaust driven gas turbine 2 after, by tail end exhaust driven gas turbine 2 it
When afterwards to before shell exhaust end marginal position, carry out it is secondary ignites, equally, residual fuel is formed by this part again fully to be fired
It burns；Finally, reach after the fuel combustion in shell and cmpletely burn, heat supply is discharged in the safe gas after burning, reduce big
Gas pollutes.
Further, in order to more preferably realize the ability of control flame combustion, air inflow is equipped in 6 outer end of air inlet turbofan
Damper 7 absorbs heat outside air and provides oxygen；
The upper and lower side of the air inflow damper 7 connect with the upper and lower side of 5 suction end of shell and is equipped with gap respectively；
The air inflow damper open up the independent open-celled structure of multilayer, it can be achieved that part layer trepanning opening and closing, lead to
The size of air door open cell content is overregulated, the abundant degree of fuel combustion, and then the size of control mode can be controlled, it is final to control
The generated energy and heating load of generator.
The air inflow damper 7 is designed to that shutter form, shutter adjust shutter by the way that adjusting rod is arranged
Direction switch, while the angle of regulation blade.
It is that main shaft 8 is made to form passive rotation that the present invention, which is installed into gas eddy fan 6, and passive rotation is to be pumped into more skies
Gas does not need extraneous electricity generation system and provides power.
Claims (10)
- The combustor 1. vortex-spraying type generates electricity, it is characterised in that：Including shell, the flange being set on shell, tail end exhaust driven gas turbine, into Gas eddy fan, the shell one end are suction end, and the other end is exhaust end；Be cavity structure in the shell, shell suction end with Exhaust end is that opening is arranged, and center is worn there are one main shaft in the shell, and main shaft one end is equipped with air inlet turbofan, the main shaft other end Equipped with tail end exhaust driven gas turbine, it is equipped with fuel feeding duct and nozzle in shell, ignition system is additionally provided in shell, in main shaft one end Equipped with shaft coupling, shaft coupling is by exporting one generator of axis connection.
- The combustor 2. vortex-spraying type according to claim 1 generates electricity, it is characterised in that the tail end exhaust driven gas turbine and air inlet Turbofan is the exhaust flabellum with angle of inclination.
- The combustor 3. vortex-spraying type according to claim 1 generates electricity, it is characterised in that the exhaust driven gas turbine and air inlet turbofan are each Self-forming multilayered structure gas vent.
- The combustor 4. vortex-spraying type according to claim 3 generates electricity, it is characterised in that the tail end exhaust driven gas turbine and air inlet The angle of inclination of turbofan gas vent is different；The inclined direction of the exhaust level of the tail end exhaust driven gas turbine is according to gas guide direction For flaring；The inclined direction of the exhaust level of the air inlet turbofan is to close up towards housing cavity according to gas guide direction.
- The combustor 5. vortex-spraying type according to claim 1 generates electricity, it is characterised in that the tail end exhaust driven gas turbine exhaust fan The blade quantity of leaf is less than the exhaust flabellum of air inlet turbofan.
- The combustor 6. vortex-spraying type according to claim 5 generates electricity, it is characterised in that the tail end exhaust driven gas turbine exhaust fan Leaf is 2 layers, and the exhaust flabellum of the air inlet turbofan is 3 layers, can increase and decrease adjusting according to the requirement to rotating speed and output power.
- The combustor 7. vortex-spraying type according to claim 1 generates electricity, it is characterised in that with main shaft to demarcate in housing hollow, It is respectively equipped with spacer structure successively, the housing cavity is divided into three layers of channel form, including separate ventilation road, combustion chamber and center lead to Air duct.
- The combustor 8. vortex-spraying type according to claim 5 generates electricity, it is characterised in that sprayed from fuel feed pipe into combustion chamber Oil, by ignition system fires, Indoor Combustion of burning, gas drastically expands, and expanding gas is discharged by tail end rapidly, due to tail end Exhaust driven gas turbine angle and quantity are less than the quantity of air inlet turbofan, and expanding gas overcomes pressure acting to be forced caudad to arrange after making burning Gas direction is discharged, and forms turbine, the rotation of gas push turbine；After turbine rotates, air inlet turbofan absorbs air from outside, when Air is drawn into combustion chamber, is mixing air in combustion chamber, and a large amount of gas and flame drive turbine rotation to spray, this part For burn incompletely, toxic and harmful gas not will produce；When air is absorbed into central ventilation road, central ventilation road is cold sky Gas, middle flame imperfect combustion, oxygen has exhausted, but there be part of fuel the inside, to shell after by tail end exhaust driven gas turbine When before body exhaust end marginal position, oxygen is provided by central passage, residual fuel is ignited, this part by residual fuel again Form fully burning；After air is absorbed from separate ventilation road reaches tail end exhaust driven gas turbine, after by tail end exhaust driven gas turbine extremely When before shell exhaust end marginal position, progress is secondary to ignite, and equally, residual fuel is formed abundant burning by this part again； Finally, reach after the fuel combustion in shell and cmpletely burn, the safe gas after burning is discharged, it is dirty to reduce air Dye.
- The combustor 9. vortex-spraying type according to claim 1 generates electricity, it is characterised in that be equipped with air inflow in air inlet turbofan outer end Outside air is pumped into housing cavity and provides oxygen by damper.
- The combustor 10. vortex-spraying type according to claim 1 generates electricity, it is characterised in that the air inflow damper it is upper Lower end connect with the upper and lower side of shell suction end and is equipped with gap respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810377764.0A CN108412615A (en) | 2018-04-25 | 2018-04-25 | Vortex-spraying type power generation combustor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810377764.0A CN108412615A (en) | 2018-04-25 | 2018-04-25 | Vortex-spraying type power generation combustor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108412615A true CN108412615A (en) | 2018-08-17 |
Family
ID=63136758
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810377764.0A Pending CN108412615A (en) | 2018-04-25 | 2018-04-25 | Vortex-spraying type power generation combustor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108412615A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111749791A (en) * | 2020-01-07 | 2020-10-09 | 姚长水 | Three-dimensional multidirectional jet cutting jet aircraft engine and using method thereof |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2696078A (en) * | 1952-08-30 | 1954-12-07 | Waitzman Simon | Jet propulsion apparatus having a combination ram-jet and turbojet engine |
| GB919113A (en) * | 1960-03-11 | 1963-02-20 | Alexander Davidson Garden | Improvements in or relating to aircraft propulsive means |
| FR2605679A1 (en) * | 1986-10-24 | 1988-04-29 | Culica Georges Francois | Multi-spool multi-bypass turbo jet engine with a drum rotor |
| WO2001048365A1 (en) * | 1999-12-23 | 2001-07-05 | Mathias Meyer | Turbojet engine |
| CN104863751A (en) * | 2015-03-27 | 2015-08-26 | 冯志新 | Circular jet-propelled double-rotor turbofan aero-engine |
| CN208267965U (en) * | 2018-04-25 | 2018-12-21 | 大连恒通和科技有限公司 | A kind of vortex-spraying type power generation combustor |
-
2018
- 2018-04-25 CN CN201810377764.0A patent/CN108412615A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2696078A (en) * | 1952-08-30 | 1954-12-07 | Waitzman Simon | Jet propulsion apparatus having a combination ram-jet and turbojet engine |
| GB919113A (en) * | 1960-03-11 | 1963-02-20 | Alexander Davidson Garden | Improvements in or relating to aircraft propulsive means |
| FR2605679A1 (en) * | 1986-10-24 | 1988-04-29 | Culica Georges Francois | Multi-spool multi-bypass turbo jet engine with a drum rotor |
| WO2001048365A1 (en) * | 1999-12-23 | 2001-07-05 | Mathias Meyer | Turbojet engine |
| CN104863751A (en) * | 2015-03-27 | 2015-08-26 | 冯志新 | Circular jet-propelled double-rotor turbofan aero-engine |
| CN208267965U (en) * | 2018-04-25 | 2018-12-21 | 大连恒通和科技有限公司 | A kind of vortex-spraying type power generation combustor |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111749791A (en) * | 2020-01-07 | 2020-10-09 | 姚长水 | Three-dimensional multidirectional jet cutting jet aircraft engine and using method thereof |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106285945A (en) | Rotate pinking electromotor continuously | |
| CN208267965U (en) | A kind of vortex-spraying type power generation combustor | |
| CN108518673B (en) | Vortex spraying type burner | |
| CN102353038B (en) | A kind of combined combustion boiler | |
| CN203533532U (en) | Biomass combustion furnace | |
| CN206205999U (en) | Continuous rotation pinking generator | |
| CN108412615A (en) | Vortex-spraying type power generation combustor | |
| CN104963774B (en) | A kind of turbine | |
| CN206205998U (en) | Continuous rotation pinking tank | |
| CN208269123U (en) | A kind of vortex-spraying type combustor | |
| CN201297767Y (en) | Environment-friendly intelligent remote control automobile air heater | |
| CN203190446U (en) | Hot-wind high-temperature gas stove | |
| CN103591573A (en) | Biomass combustion furnace | |
| CN106931451A (en) | Spiral-flow type incinerator | |
| CN216079751U (en) | Pulse combustion superheated steam generator | |
| CN217482994U (en) | Energy-saving type burner of hot blast stove | |
| JP3215513U (en) | Rechargeable burner | |
| CN207661765U (en) | Jet flow combustor | |
| CN211290100U (en) | Burner of reducing gas producer | |
| CN106337738B (en) | Continuous rotation pinking tank | |
| CN109945177B (en) | Supercharged combustion machine | |
| CN208711376U (en) | A kind of processing of combustion tail gas and heat reclaim unit | |
| CN206755182U (en) | Spiral-flow type incinerator | |
| TWI725268B (en) | Jet burner | |
| JP3215938U (en) | Jet burner |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| CB02 | Change of applicant information |
Address after: Room 1501, Block A, Pioneering Building, 32 Torch Road, Dalian High-tech Park, Liaoning Province, 116000 Applicant after: DALIAN HENGTONGHE SCIENCE & TECHNOLOGY CO.,LTD. Address before: Room 609, 6th Floor, No. 1 Gaoxin Street, Dalian Hi-tech Industrial Park, Liaoning Province Applicant before: DALIAN HENGTONGHE SCIENCE & TECHNOLOGY CO.,LTD. |
|
| CB02 | Change of applicant information | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180817 |