CN106437963A - Novel negative-pressure high-temperature automatic regenerative purifier for exhausted gas of diesel engine - Google Patents

Novel negative-pressure high-temperature automatic regenerative purifier for exhausted gas of diesel engine Download PDF

Info

Publication number
CN106437963A
CN106437963A CN201610732582.1A CN201610732582A CN106437963A CN 106437963 A CN106437963 A CN 106437963A CN 201610732582 A CN201610732582 A CN 201610732582A CN 106437963 A CN106437963 A CN 106437963A
Authority
CN
China
Prior art keywords
outer pipe
zone
outer tube
tail gas
pressure high
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
Application number
CN201610732582.1A
Other languages
Chinese (zh)
Inventor
余岳珠
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.)
Depew Ningbo Foster Environmental Protection Technology Co Ltd
Original Assignee
Depew Ningbo Foster Environmental Protection 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 Depew Ningbo Foster Environmental Protection Technology Co Ltd filed Critical Depew Ningbo Foster Environmental Protection Technology Co Ltd
Priority to CN201610732582.1A priority Critical patent/CN106437963A/en
Publication of CN106437963A publication Critical patent/CN106437963A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N3/00Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
    • F01N3/08Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous
    • F01N3/10Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust
    • F01N3/24Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust characterised by constructional aspects of converting apparatus
    • F01N3/28Construction of catalytic reactors
    • F01N3/2882Catalytic reactors combined or associated with other devices, e.g. exhaust silencers or other exhaust purification devices
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N3/00Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
    • F01N3/08Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous
    • F01N3/10Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust
    • F01N3/18Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust characterised by methods of operation; Control
    • F01N3/20Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust characterised by methods of operation; Control specially adapted for catalytic conversion ; Methods of operation or control of catalytic converters
    • F01N3/2006Periodically heating or cooling catalytic reactors, e.g. at cold starting or overheating
    • F01N3/2033Periodically heating or cooling catalytic reactors, e.g. at cold starting or overheating using a fuel burner or introducing fuel into exhaust duct
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N3/00Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
    • F01N3/08Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous
    • F01N3/10Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust
    • F01N3/24Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust characterised by constructional aspects of converting apparatus
    • F01N3/28Construction of catalytic reactors
    • F01N3/2892Exhaust flow directors or the like, e.g. upstream of catalytic device
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N9/00Electrical control of exhaust gas treating apparatus
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2240/00Combination or association of two or more different exhaust treating devices, or of at least one such device with an auxiliary device, not covered by indexing codes F01N2230/00 or F01N2250/00, one of the devices being
    • F01N2240/14Combination or association of two or more different exhaust treating devices, or of at least one such device with an auxiliary device, not covered by indexing codes F01N2230/00 or F01N2250/00, one of the devices being a fuel burner
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2260/00Exhaust treating devices having provisions not otherwise provided for
    • F01N2260/06Exhaust treating devices having provisions not otherwise provided for for improving exhaust evacuation or circulation, or reducing back-pressure
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/40Engine management systems

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Health & Medical Sciences (AREA)
  • Toxicology (AREA)
  • Exhaust Gas After Treatment (AREA)

Abstract

The invention discloses a novel negative-pressure high-temperature automatic regenerative purifier for exhausted gas of a diesel engine. The purifier comprises a central control system, a burning jetting zone, a heat flow mixing zone, a catalytic filtering zone and a discharging zone; and the burning jetting zone (that is, a thin and round outer pipe), the heat flow mixing zone (that is, a long-funnel-shaped outer pipe), the catalytic filtering zone (that is, a thick and round outer pipe) and the discharging zone (that is, a short-funnel-shaped outer pipe) are sequentially and fixedly connected through flanges and then are combined with the central control system to form the complete negative-pressure high-temperature automatic regenerative purifier for the exhausted gas of the diesel engine. The internal structure of the purifier is changed through innovation, the beneficial effects of complete mixing, sufficient burning, uniform catalytic purification and adaptation to any environments are realized, and the purifier has the advantages of being efficient, energy-saving, environment-friendly and low-carbon and is certainly popular in the market.

Description

A kind of novel diesel tail gas negative pressure high temperature automatic regeneration clarifier
Technical field
The present invention relates to environmental purification field, especially relate to a kind of novel diesel tail gas negative pressure high temperature automatic regeneration net Change device.
Background technology
Traditional exhaust gas cleaner is mostly cavity sidewalls oil spout and lights burning setting again, because it is that cavity sidewalls is lighted Mode, in tail gas flow at high speed, exists and is not easy to light, and half side partial combustion burns insufficient, purifies not exclusively, and It is difficult to, under temperature environment at the bottom of winter, deficiencies such as lighting, all can directly influence the clean-up effect to tail gas.
Content of the invention
The technical problem to be solved is automatic by a kind of novel diesel tail gas negative pressure high temperature of scientific design Regenerative purifier, is changed the internal structure of clarifier by innovation, increases bullet-headed negative pressure high temperature combustion chamber assembly set, and increases Hybrid turbine, then through thermally induced flow plate uniformly through oxidation catalyst filter carrier, reaches to be thoroughly mixed, fully burning, homogeneous catalyst purify Beneficial effect, solve conventional exhaust purifier burning insufficient, purification efficiency is low, be difficult to deficiencies such as lighting.
The technical scheme that the present invention solves that above-mentioned technical problem used is:A kind of novel diesel tail gas negative pressure high temperature is certainly Dynamic regenerative purifier, including central control system, combustion jet district, hot-fluid mixed zone, catalytic filtering zone and discharge region;Described Combustion jet district includes thin circular outer pipe, combustion chamber assembly set, and described combustion chamber assembly set is axially fixedly installed on institute by support The inner chamber central authorities of the thin circular outer pipe stated, described combustion chamber assembly set outer wall forms cavity folder with described thin circular outer pipe inwall Layer;Described thin circular outer pipe one sidewall is provided with pressurised oil tracheae, supercharging tracheae, device for igniting and described combustion chamber assembly set The fixing connection of one sidewall correspondence position.
Described combustion chamber assembly set is arranged to bullet shape, in head end one STH and the described increasing of sub warhead taper The corresponding fixing connection of force feed tracheae, the other end in hole is arranged to funnel-form small openings at the inner chamber of sub warhead taper, forms mist Change atomizer;Sub warhead conical section is arranged to inside and outside double wall, described inside and outside double wall and described combustion chamber assembly set Rectangle part in form the triangular cavity that a circle does not completely encloses between nosing, described inwall and described interior nosing it Between form a circle annular air outlet, the side of described outer wall is corresponding with described supercharging tracheae fixing to be connected, formation air inlet pipe; The rectangle part one sidewall fixing connection corresponding with described device for igniting of described combustion chamber assembly set.
Described central control system includes master controller, pressure oil pump, pressure oil pump damper, supercharging air pump, supercharging Air pump damper, described device for igniting, temperature sensor T1, temperature sensor T2, pressure sensor P1, pressure sensor P2, Pressure device and data wire;Described master controller connects the coordination work between the above-mentioned each parts of control monitoring by described data wire Make.
Described hot-fluid mixed zone includes long infundibulate outer tube, hybrid turbine, described temperature sensor T1, thermally induced flow Plate, described pressure sensor P1;Described hybrid turbine is fixedly installed in the neck of described long infundibulate outer tube, described Temperature sensor T1 and described pressure sensor P1 be fixedly installed on the pan side of described long infundibulate outer tube successively In, described thermally induced flow plate is fixedly installed on the uncovered middle position of pan of pipe at described long infundibulate.
Described catalytic filtering zone includes thick circular outer pipe, oxidation catalyst filter carrier;Described thick circular outer pipe is by neck bush Layer and enclosing cover layer inside and outside fix sheathed combining, and described oxidation catalyst filter carrier is fixed on described thick circle by retaining collar In shape outer tube.
Described discharge region includes funnel shape outer tube, and is fixedly installed on the pan of described funnel shape outer tube successively Described pressure sensor P2 in side and described temperature sensor T2, is fixedly installed on described funnel shape outer tube The back flow plate of pan central authorities.
Described combustion jet district (i.e. described thin circular outer pipe), described hot-fluid mixed zone (i.e. described long funnel Shape outer tube), catalytic filtering zone (i.e. described thick circular outer pipe), discharge region (i.e. described funnel shape outer tube) pass sequentially through method Blue fixing connection, then it is combined into a kind of novel diesel tail gas negative pressure high temperature of complete set certainly with described central control system Dynamic regenerative purifier.
Its technical characterstic and operation principle:
The tail gas inlet port in described combustion jet district (i.e. described thin circular outer pipe) is close with the blast pipe of diesel engine Sealing connects surely, and tail gas is decomposed by bullet-headed described combustion chamber assembly set, in institute after being entered by described tail gas air inlet Combustion chamber assembly set outer wall and the described thin circular outer pipe inwall stated form the flowing of cavity interlayer high speed, total to described combustion room Set of internal cavity forms gas turbulence, thus forms negative pressure;It is subject to when tail gas flows at a high speed described oxidation catalyst filter carrier Certain resistance air pressure can raise, and when reaching certain force value, force value can be transferred to institute by described pressure sensor P1 The master controller stated, described master controller starts described pressure oil pump and the work of described supercharging air pump, by oil gas high pressure The gas mixture that mixing is fully atomized from described atomizing fuel spray nozzle ejection through described pressurised oil tracheae;Described supercharging gas Pump forms a circle circle air space by described supercharging tracheae from described annular air outlet ejection air simultaneously, both for burning Sufficient oxygen is provided, provides cooling protection for described device for igniting again;Described master controller starts described lighting immediately The gas mixture of atomization lighted by device, by the not sufficiently combusted impurity in tail gas, particle, harmful substance high-temp combustion again, Described hybrid turbine rotate under the drive of air-flow be sufficiently mixed combustion-supporting.
Tail gas after again burning is led through described heat in described hot-fluid mixed zone (i.e. described long infundibulate outer tube) Even into catalytic filtering zone (i.e. described thick circular outer pipe) after stream plate shunting, by described oxidation catalyst filter carrier layer by layer Oxidation catalyst filter becomes the clean gas after purifying described through arrange in described discharge region (i.e. described funnel shape outer tube) again Back flow plate decompression, cooling, extinguish and discharge after Mars, reach the effect purifying.
Owing to being provided with described temperature sensor in described hot-fluid mixed zone (i.e. described long infundibulate outer tube) T1 and described pressure sensor P1, when described temperature sensor T1 detects described hot-fluid mixed zone (i.e. described length Infundibulate outer tube) in temperature when reaching setting value, described master controller can reduce the operating frequency of described pressure oil pump, Thus reach the balance of described hot-fluid mixed zone (i.e. described long infundibulate outer tube) interior temperature.When described pressure sensor P1 detects that described hot-fluid mixed zone (i.e. described long infundibulate outer tube) interior pressure detects with described pressure sensor P2 To described discharge region (i.e. described funnel shape outer tube) interior pressure in pressure device setting value when, described master controller stops Only described pressure oil pump and the work of described device for igniting, complete the working procedure of an automatic regeneration.Now described master control Device processed intermittent can send a pulse signal and connect to described supercharging air pump damper, described supercharging air pump damper High pressure gas know from experience and intermittent be carried out to described pressurised oil tracheae and described atomizing fuel spray nozzle, prevent blocking existing As.
Compared with prior art, it is an advantage of the current invention that:
A kind of novel diesel tail gas negative pressure high temperature automatic regeneration clarifier of the present invention, is changed in clarifier by innovation Portion's structure, reaches to be thoroughly mixed, fully burning, homogeneous catalyst purify, adapt to the beneficial effect of any environment, it is energy-efficient, The advantage of environmental protection low-carbon (LC), will be liked by market.
Brief description
Fig. 1 is the overall schematic of the present invention;
Fig. 2 is the longitudinal sectional structure schematic diagram of purification operative body part of the present invention;
Fig. 3 is longitudinal sectional structure schematic diagram of the combustion chamber assembly set of the present invention;
Fig. 4 is the hybrid turbine front view of the present invention.
Detailed description of the invention
Below in conjunction with accompanying drawing embodiment, the present invention is described in further detail.
In this particular embodiment, as shown in Figure 1 and Figure 2, a kind of novel diesel tail gas negative pressure high temperature automatic regeneration purifies Device, including central control system, combustion jet district A, hot-fluid mixed zone B, catalytic filtering zone C and discharge region D;Described burning spray Penetrating district A and including that the 10th, thin circular outer pipe fires chamber assembly set 17, described combustion chamber assembly is overlapped 17 and is axially fixedly installed on institute by support The inner chamber central authorities of the thin circular outer pipe 10 stated, described combustion chamber assembly set 17 outer walls are formed with described thin circular outer pipe 10 inwall Cavity interlayer;Described thin circular outer pipe 10 1 sidewall be provided with pressurised oil tracheae the 14th, supercharging tracheae the 15th, device for igniting 16 with described The fixing connection of a sidewall correspondence position of combustion chamber assembly set 17.
In this particular embodiment, as shown in Figure 2 and Figure 3, described combustion chamber assembly set 17 is arranged to bullet shape, The head end one STH fixing connection corresponding with described pressurised oil tracheae 14 of sub warhead taper, the other end in hole is at bullet nose cone The inner chamber of shape is arranged to funnel-form small openings, forms atomizing fuel spray nozzle 29;Sub warhead conical section is arranged to interior 32nd, outer 33 pairs Layer wall, forms a circle between nosing 34 in the rectangle part of described interior 32nd, outer 33 double walls and described combustion chamber assembly set 17 The triangular cavity not completely enclosed, forms a circle annular air outlet 30 between described inwall 32 and described interior nosing 34, The fixing connection corresponding with described supercharging tracheae 15 of the side of described outer wall 33, forms air inlet pipe;Described combustion chamber assembly set The rectangle part one sidewall fixing connection corresponding with described device for igniting 16 of 17.
In this particular embodiment, as shown in Figure 1 and Figure 2, described central control system includes master controller the 7th, pressurised oil The 4th, described device for igniting the 16th, the temperature sensor T1 of pump the 3rd, pressure oil pump damper the 2nd, supercharging air pump the 5th, supercharging air pump damper is the 19th, Temperature sensor T2 the 27th, pressure sensor P1 the 21st, pressure sensor P2 the 26th, pressure device 8 and data wire 6;Described main control Device 7 connects the co-ordination between the above-mentioned each parts of control monitoring by described data wire 6.
In this particular embodiment, as shown in Figure 1, Figure 2, Figure 4 shows, described hot-fluid mixed zone B includes long infundibulate outer tube 11st, the 20th, the described pressure sensor P1 21 of the 18th, described temperature sensor T1 the 19th, the thermally induced flow plate of hybrid turbine;Described is mixed Close in the neck that turbine 18 is fixedly installed on described long infundibulate outer tube 11, described temperature sensor T1 19 and described Pressure sensor P1 21 is fixedly installed in the pan side of described long infundibulate outer tube 11 successively, described thermally induced flow plate The 20 uncovered middle positions of pan being fixedly installed on pipe 11 at described long infundibulate.
In this particular embodiment, as shown in Figure 1 and Figure 2, described catalytic filtering zone C includes that the 12nd, thick circular outer pipe is catalyzed Filtration supports 24;Described thick circular outer pipe 12 is inside and outside fixed sheathed combining by liner jacket layer 22 and enclosing cover layer 23, described Oxidation catalyst filter carrier 24 be fixed in described thick circular outer pipe 12 by retaining collar 25.
In this particular embodiment, as shown in Figure 1 and Figure 2, described discharge region D includes funnel shape outer tube 13, and successively It is fixedly installed on the described pressure sensor P2 26 in the pan side of described funnel shape outer tube 13 and described temperature Sensor T2 27, is fixedly installed on the described back flow plate 28 of the pan central authorities of described funnel shape outer tube 13.
In this particular embodiment, as shown in Figure 1 and Figure 2, described combustion jet district A (i.e. described thin circular outer pipe 10), described hot-fluid mixed zone B (i.e. described long infundibulate outer tube 11), catalytic filtering zone C (i.e. described thick circular outer pipe 12), discharge region D (i.e. described funnel shape outer tube 13) passes sequentially through the fixing connection of flange 31, then controls with described central authorities System in combination becomes a kind of novel diesel tail gas negative pressure high temperature automatic regeneration clarifier of complete set.
Its technical characterstic and operation principle:
In this particular embodiment, as shown in Figure 1, Figure 2, Figure 3, Figure 4, described combustion jet district A (i.e. described thin circle Shape outer tube 10) the blast pipe of tail gas air inlet 1 end and diesel engine seal fixing connection, tail gas passes through described tail gas air inlet By bullet-headed described combustion chamber assembly set 17 decomposition after 1 entrance, overlap 17 outer walls and described thin circle at described combustion chamber assembly Shape outer tube 10 inwall forms the flowing of cavity interlayer high speed, forms gas turbulence to the internal cavity of described combustion chamber assembly set 17, Thus form negative pressure;Can be raised by certain resistance air pressure when tail gas flows at a high speed described oxidation catalyst filter carrier 24, reach During to certain force value, force value can be transferred to described master controller 7 by described pressure sensor P1 21, described Master controller 7 starts described pressure oil pump 3 and described supercharging air pump 5 works, by oil gas high pressure mixing through described supercharging Oil/Gas Pipe 14 sprays the gas mixture of fully atomization from described atomizing fuel spray nozzle 29;Described supercharging air pump 5 passes through simultaneously Described supercharging tracheae 15 sprays air from described annular air outlet 30 and forms a circle circle air space, both fills for offer of burning The oxygen of foot, provides cooling protection for described device for igniting 16 again;Described master controller 7 starts described device for igniting 16 immediately Light the gas mixture of atomization, by the not sufficiently combusted impurity in tail gas, particle, harmful substance high-temp combustion again, institute The hybrid turbine 18 stated rotate under the drive of air-flow be sufficiently mixed combustion-supporting.
In this particular embodiment, as shown in Figure 1, Figure 2, Figure 3, Figure 4, the tail gas after again burning mixes through described hot-fluid Even into catalytic filtering zone C (i.e. institute after thermally induced flow plate 20 shunting described in closing district B (i.e. described long infundibulate outer tube 11) The thick circular outer pipe 12 stated), become the clean gas after purifying again by the oxidation catalyst filter layer by layer of described oxidation catalyst filter carrier 24 Described back flow plate 28 through arranging in described discharge region D (i.e. described funnel shape outer tube 13) reduces pressure, lowers the temperature, extinguishes fire Discharge after star, reach the effect purifying.
In this particular embodiment, as shown in Figure 1, Figure 2, Figure 3, Figure 4, due to (i.e. described at described hot-fluid mixed zone B Long infundibulate outer tube 11) in be provided with described temperature sensor T1 19 and described pressure sensor P1 21, when described Temperature sensor T1 19 detect that the temperature in described hot-fluid mixed zone B (i.e. described long infundibulate outer tube 11) reaches During setting value, described master controller 7 can reduce the operating frequency of described pressure oil pump 3, thus reach described hot-fluid and mix Close the balance of district B (i.e. described long infundibulate outer tube 11) interior temperature.Described in detecting as described pressure sensor P1 21 Hot-fluid mixed zone B (i.e. described long infundibulate outer tube 11) interior pressure and described pressure sensor P2 26 detect described When discharge region D (i.e. described funnel shape outer tube 13) interior pressure is in pressure device 8 setting value, described master controller 7 stops Described pressure oil pump 3 and described device for igniting 16 work, and complete the working procedure of an automatic regeneration.Now described master control Device 7 processed intermittent can send a pulse signal to described supercharging air pump damper 4, described supercharging air pump damper 4 The high pressure gas cognition of connection is intermittent to be carried out to described pressurised oil tracheae 14 and described atomizing fuel spray nozzle 29, prevents Clogging.
Compared with prior art, it is an advantage of the current invention that:
A kind of novel diesel tail gas negative pressure high temperature automatic regeneration clarifier of the present invention, is changed in clarifier by innovation Portion's structure, reaches to be thoroughly mixed, fully burning, homogeneous catalyst purify, adapt to the beneficial effect of any environment, it is energy-efficient, The advantage of environmental protection low-carbon (LC), will be liked by market.
Finally it should be noted that:Specific embodiment described herein is only explanation for example to present invention spirit. Those skilled in the art can to described have embodiment make various modification or supplement or Similar mode is used to substitute, but without departing from the spirit of the present invention or surmount model defined in appended claims Enclose.
Although more employing combustion jet district A, hot-fluid mixed zone B, catalytic filtering zone C, discharge region D, tail gas herein Air inlet the 1st, pressure oil pump damper the 2nd, pressure oil pump the 3rd, supercharging air pump damper the 4th, supercharging air pump the 5th, data wire the 6th, master controller 7th, the 8th, pressure device purifies gas gas outlet the 9th, thin circular outer pipe the 10th, long infundibulate outer tube the 11st, thick circular outer pipe the 12nd, funnel shape outer tube 13rd, the 19th, the 16th, pressurised oil tracheae the 14th, supercharging tracheae the 15th, device for igniting fire chamber assembly set the 17th, hybrid turbine the 18th, temperature sensor T1 Thermally induced flow plate the 20th, pressure sensor P1 the 21st, liner jacket layer the 22nd, enclosing cover layer the 23rd, oxidation catalyst filter carrier the 24th, retaining collar the 25th, pressure Sensor P2 the 26th, temperature sensor T2 the 27th, back flow plate the 28th, atomizing fuel spray nozzle the 29th, annular air outlet the 30th, flange the 31st, inwall is the 32nd, Outer wall the 33rd, the terms such as interior nosing 34, but it is not precluded from using the possibility of other terms.These terms are used to be only used to more Describe and explain the structure of the present invention, the beneficial effect assembling and reaching easily, be construed as any attached The restriction adding is all contrary with spirit of the present invention.

Claims (7)

1. a novel diesel tail gas negative pressure high temperature automatic regeneration clarifier, it is characterised in that:Including central control system, combustion Burn inlet zone, hot-fluid mixed zone, catalytic filtering zone and discharge region;Described combustion jet district includes that thin circular outer pipe, combustion room are total Complete, described combustion chamber assembly set is axially fixedly installed on the inner chamber central authorities of described thin circular outer pipe by support, described Combustion chamber assembly set outer wall forms cavity interlayer with described thin circular outer pipe inwall;Described thin circular outer pipe one sidewall is provided with Pressurised oil tracheae, supercharging tracheae, device for igniting are fixing with a sidewall correspondence position of described combustion chamber assembly set to be connected.
2. a kind of novel diesel tail gas negative pressure high temperature automatic regeneration clarifier according to claim 1, it is characterised in that: Described combustion chamber assembly set is arranged to bullet shape, at head end one STH and the described pressurised oil tracheae of sub warhead taper Corresponding fixing connection, the other end in hole is arranged to funnel-form small openings at the inner chamber of sub warhead taper, forms atomizing fuel spray nozzle; Sub warhead conical section is arranged to inside and outside double wall, the rectangle part of described inside and outside double wall and described combustion chamber assembly set Form the triangular cavity that a circle does not completely encloses between interior nosing, between described inwall and described interior nosing, form a circle Annular air outlet, the fixing connection corresponding with described supercharging tracheae of the side of described outer wall, form air inlet pipe;Described combustion room The fixing connection corresponding with described device for igniting of total set of rectangle part one sidewall.
3. a kind of novel diesel tail gas negative pressure high temperature automatic regeneration clarifier according to claim 1, it is characterised in that: Described central control system includes master controller, pressure oil pump, pressure oil pump damper, supercharging air pump, supercharging air pump damping Device, described device for igniting, temperature sensor T1, temperature sensor T2, pressure sensor P1, pressure sensor P2, pressure device and Data wire;Described master controller connects the co-ordination between the above-mentioned each parts of control monitoring by described data wire.
4. a kind of novel diesel tail gas negative pressure high temperature automatic regeneration clarifier according to claim 1, it is characterised in that: Described hot-fluid mixed zone includes long infundibulate outer tube, hybrid turbine, temperature sensor T1, thermally induced flow plate, pressure sensor P1; Hybrid turbine is fixedly installed in the neck of described long infundibulate outer tube, and described temperature sensor T1 and described pressure pass Sensor P1 is fixedly installed in the pan side of described long infundibulate outer tube successively, and described thermally induced flow plate is fixedly installed on institute The uncovered middle position of pan of pipe at the long infundibulate stated.
5. a kind of novel diesel tail gas negative pressure high temperature automatic regeneration clarifier according to claim 1, it is characterised in that: Described catalytic filtering zone includes thick circular outer pipe, oxidation catalyst filter carrier;Described thick circular outer pipe is by liner jacket layer and outer cover Layer inside and outside fixes sheathed combining, and described oxidation catalyst filter carrier is fixed on described thick circular outer pipe by retaining collar In.
6. a kind of novel diesel tail gas negative pressure high temperature automatic regeneration clarifier according to claim 1, it is characterised in that: Described discharge region includes funnel shape outer tube, and is fixedly installed on successively in the pan side of described funnel shape outer tube Pressure sensor P2 and temperature sensor T2, is fixedly installed on the back flow plate of the pan central authorities of described funnel shape outer tube.
7. a kind of novel diesel tail gas negative pressure high temperature automatic regeneration clarifier according to claim 1, it is characterised in that: Described combustion jet district (i.e. described thin circular outer pipe), described hot-fluid mixed zone (i.e. described long infundibulate outer tube), It is fixing even that catalytic filtering zone (i.e. described thick circular outer pipe), discharge region (i.e. described funnel shape outer tube) pass sequentially through flange Connect, then to be combined into a kind of novel diesel tail gas negative pressure high temperature automatic regeneration of complete set net with described central control system Change device.
CN201610732582.1A 2016-08-22 2016-08-22 Novel negative-pressure high-temperature automatic regenerative purifier for exhausted gas of diesel engine Pending CN106437963A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610732582.1A CN106437963A (en) 2016-08-22 2016-08-22 Novel negative-pressure high-temperature automatic regenerative purifier for exhausted gas of diesel engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610732582.1A CN106437963A (en) 2016-08-22 2016-08-22 Novel negative-pressure high-temperature automatic regenerative purifier for exhausted gas of diesel engine

Publications (1)

Publication Number Publication Date
CN106437963A true CN106437963A (en) 2017-02-22

Family

ID=58182939

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610732582.1A Pending CN106437963A (en) 2016-08-22 2016-08-22 Novel negative-pressure high-temperature automatic regenerative purifier for exhausted gas of diesel engine

Country Status (1)

Country Link
CN (1) CN106437963A (en)

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5826428A (en) * 1995-02-09 1998-10-27 J. Eberspacher Gmbh & Co. Burner for the thermal regeneration of a particle filter in an exhaust gas aftertreatment system of an internal combustion engine, especially a diesel engine
CN101178020A (en) * 2006-11-10 2008-05-14 烟台华龙商用机器有限公司 Diesel engine exhaust emission purifying system
CN101929371A (en) * 2009-06-19 2010-12-29 Tems有限公司 Burner for diesel particulate filter regeneration
KR20120122559A (en) * 2011-04-29 2012-11-07 주식회사 크린어스 Apparatus for regeneration of diesel particulate filter and apparatus for reduction of diesel particulate matter having the same
JP2013245609A (en) * 2012-05-25 2013-12-09 Hino Motors Ltd Burner for exhaust gas cleaning device
CN104975912A (en) * 2014-04-02 2015-10-14 清净绿能科技股份有限公司 Purifying treatment device for discharged smoke
CN205955801U (en) * 2016-03-15 2017-02-15 瑞胜精密工业股份有限公司 Purifying treatment device for black smoke and waste gas discharged by vehicle
CN206071693U (en) * 2016-08-22 2017-04-05 宁波德普福斯特环保科技有限公司 A kind of novel diesel tail gas negative pressure high temperature automatic regeneration depurator

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5826428A (en) * 1995-02-09 1998-10-27 J. Eberspacher Gmbh & Co. Burner for the thermal regeneration of a particle filter in an exhaust gas aftertreatment system of an internal combustion engine, especially a diesel engine
CN101178020A (en) * 2006-11-10 2008-05-14 烟台华龙商用机器有限公司 Diesel engine exhaust emission purifying system
CN101929371A (en) * 2009-06-19 2010-12-29 Tems有限公司 Burner for diesel particulate filter regeneration
KR20120122559A (en) * 2011-04-29 2012-11-07 주식회사 크린어스 Apparatus for regeneration of diesel particulate filter and apparatus for reduction of diesel particulate matter having the same
JP2013245609A (en) * 2012-05-25 2013-12-09 Hino Motors Ltd Burner for exhaust gas cleaning device
CN104975912A (en) * 2014-04-02 2015-10-14 清净绿能科技股份有限公司 Purifying treatment device for discharged smoke
CN205955801U (en) * 2016-03-15 2017-02-15 瑞胜精密工业股份有限公司 Purifying treatment device for black smoke and waste gas discharged by vehicle
CN206071693U (en) * 2016-08-22 2017-04-05 宁波德普福斯特环保科技有限公司 A kind of novel diesel tail gas negative pressure high temperature automatic regeneration depurator

Similar Documents

Publication Publication Date Title
CN106437982B (en) Axis goes out cartridge type post-processing assembly into axis
CN103822207B (en) Variable pressure and variable working condition oil burner
CN104411931B (en) Burner and filter regenerating apparatus
CN106837478A (en) Combustion-supporting and catalytic regeneration system the burner of diesel engine vent gas oil spout
CN206071693U (en) A kind of novel diesel tail gas negative pressure high temperature automatic regeneration depurator
JP3193010U (en) Smart type filter
RU2571706C2 (en) Ice exhaust gas heater
CN107620962B (en) A kind of biogas low NO
CN107355786A (en) The more level air-distributions of industrial combustion gas kiln are oxygen-enriched with burning burner special
CN105042594B (en) A kind of Energy saving burning nozzle of high-speed stirred fuel combination
CN110273731A (en) A kind of burner meeting grain catcher DPF worst cold case highly efficient regeneration
CN106762225A (en) A kind of rocket engine anti-backfire nozzle
CN206668366U (en) Diesel engine vent gas oil spout is combustion-supporting and the burner of catalytic regeneration system
CN106437963A (en) Novel negative-pressure high-temperature automatic regenerative purifier for exhausted gas of diesel engine
CN104624425A (en) Air atomization spray gun for denitration
CN209100117U (en) Improved black smoke purifying and regenerating device for diesel engine
TWM524389U (en) Vehicle smoke exhausting and waste gas purification treatment device
CN205591986U (en) Flame projecting structure is prevented to muffler
CN211230585U (en) Burner capable of achieving efficient regeneration of DPF of particulate filter under low-temperature working condition
CN205977333U (en) Black cigarette of diesel oil engine purifies and regenerating unit
CN109404986A (en) A kind of " W " burning type energy-saving gas cooker
CN104501207B (en) Gas-turbine combustion chamber nozzle
CN207247203U (en) The more level air-distributions of industrial combustion gas kiln are oxygen-enriched with burning burner special
CN208347864U (en) A kind of mixer applied to diesel engine initiative regeneration control system
CN203822418U (en) Exhaust purification treatment device

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20170222