CN110657052A - High-pressure common-rail explosion-proof diesel engine air inlet system - Google Patents

High-pressure common-rail explosion-proof diesel engine air inlet system Download PDF

Info

Publication number
CN110657052A
CN110657052A CN201911098196.1A CN201911098196A CN110657052A CN 110657052 A CN110657052 A CN 110657052A CN 201911098196 A CN201911098196 A CN 201911098196A CN 110657052 A CN110657052 A CN 110657052A
Authority
CN
China
Prior art keywords
air
water tank
explosion
air inlet
proof
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.)
Withdrawn
Application number
CN201911098196.1A
Other languages
Chinese (zh)
Inventor
傅佳明
金奇才
吴春良
陈甲尉
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.)
JIANGYIN CARRIAGE MACHINERY CO Ltd
Original Assignee
JIANGYIN CARRIAGE MACHINERY 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 JIANGYIN CARRIAGE MACHINERY CO Ltd filed Critical JIANGYIN CARRIAGE MACHINERY CO Ltd
Priority to CN201911098196.1A priority Critical patent/CN110657052A/en
Publication of CN110657052A publication Critical patent/CN110657052A/en
Withdrawn legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M35/00Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
    • F02M35/10Air intakes; Induction systems
    • F02M35/1015Air intakes; Induction systems characterised by the engine type
    • F02M35/10157Supercharged engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01PCOOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P11/00Component parts, details, or accessories not provided for in, or of interest apart from, groups F01P1/00 - F01P9/00
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B29/00Engines characterised by provision for charging or scavenging not provided for in groups F02B25/00, F02B27/00 or F02B33/00 - F02B39/00; Details thereof
    • F02B29/04Cooling of air intake supply
    • F02B29/0406Layout of the intake air cooling or coolant circuit
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D11/00Arrangements for, or adaptations to, non-automatic engine control initiation means, e.g. operator initiated
    • F02D11/06Arrangements for, or adaptations to, non-automatic engine control initiation means, e.g. operator initiated characterised by non-mechanical control linkages, e.g. fluid control linkages or by control linkages with power drive or assistance
    • F02D11/08Arrangements for, or adaptations to, non-automatic engine control initiation means, e.g. operator initiated characterised by non-mechanical control linkages, e.g. fluid control linkages or by control linkages with power drive or assistance of the pneumatic type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D9/00Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits
    • F02D9/08Throttle valves specially adapted therefor; Arrangements of such valves in conduits
    • F02D9/10Throttle valves specially adapted therefor; Arrangements of such valves in conduits having pivotally-mounted flaps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M35/00Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
    • F02M35/02Air cleaners
    • F02M35/04Air cleaners specially arranged with respect to engine, to intake system or specially adapted to vehicle; Mounting thereon ; Combinations with other devices
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M35/00Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
    • F02M35/10Air intakes; Induction systems
    • F02M35/10242Devices or means connected to or integrated into air intakes; Air intakes combined with other engine or vehicle parts
    • F02M35/10275Means to avoid a change in direction of incoming fluid, e.g. all intake ducts diverging from plenum chamber at acute angles; Check valves; Flame arrestors for backfire prevention
    • 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
    • Y02T10/12Improving ICE efficiencies

Abstract

The invention relates to a high-pressure common-rail explosion-proof diesel engine air inlet system which is characterized by sequentially comprising an air filter, an explosion-proof supercharger, an inter-cooling device, an air inlet air door assembly, an air inlet flame arrester and an explosion-proof air inlet manifold from front to back, wherein an air outlet of the air filter is connected with an air inlet of the explosion-proof supercharger, a supercharging air outlet of the explosion-proof supercharger is connected with an air inlet of the inter-cooling device through a first supercharging air inlet pipe, an air outlet of the inter-cooling device is connected with an air inlet of the air inlet air door assembly through a second supercharging air inlet pipe, an air outlet of the air inlet air door assembly is connected with an air inlet of the air inlet flame. The air inlet system of the high-pressure common-rail explosion-proof diesel engine has the advantages of saving energy, reducing emission, reducing noise and improving safety performance, and realizes efficient environment-friendly operation of underground operation through strict control of various parameters.

Description

High-pressure common-rail explosion-proof diesel engine air inlet system
Technical Field
The invention relates to an air inlet system of a high-pressure common-rail explosion-proof diesel engine.
Background
The first generation of the fuel injection system adopted by the high-power diesel engine is a control mode of a mechanical fuel injection pump and a speed regulator, the fuel injection quantity is controlled by changing the position of a rack of the fuel injection pump through the speed regulator, and the high pressure of injection is generated by a cam of an oil pump; the second generation is a control mode of an electric control injection pump and an electric injection controller, the starting point and the injection quantity of oil injection can be flexibly controlled by controlling the opening time and the opening duration of an electromagnetic valve of the electric control pump, and the high pressure of injection is generated by an oil pump cam.
The latest fuel injection technology is a third generation high-pressure common rail fuel injection system, a fuel injection pump independently installed near each cylinder of a diesel engine is omitted, the high pressure of fuel injection is generated by the independent high-pressure common rail pump, high-pressure fuel is conveyed to each cylinder by a high-pressure common rail pipe, and the control of fuel injection is realized by driving an electric control fuel injector installed in each cylinder by an electronic injection controller.
The working process of the diesel engine is the same as that of the gasoline engine, and each working cycle also goes through four strokes of air intake, compression, work application and exhaust. However, the fuel for diesel engine is diesel oil, which has higher viscosity than gasoline and is not easy to evaporate, and its self-ignition temperature is lower than gasoline, so the formation and ignition mode of combustible mixture are different from that of gasoline engine.
The diesel engine sucks pure air in an intake stroke. When the compression stroke is close to the end, the oil pressure of the diesel oil is increased to more than 10MPa through an oil injection pump, the diesel oil is injected into the cylinder through an oil injector, and the diesel oil is mixed with the compressed high-temperature air in a short time to form combustible mixed gas. Because the compression ratio of the diesel engine is high (generally 16-22), the air pressure in the cylinder can reach 3.5-4.5MPa and the temperature can reach 750-1000K at the same time when the compression is finished (while the mixed air pressure of the gasoline engine at the moment can reach 0.6-1.2MPa and the temperature can reach 600-700K), which greatly exceeds the self-ignition temperature of the diesel oil. Therefore, after the diesel oil is injected into the cylinder, the diesel oil is mixed with the air in a short time and then is immediately ignited and combusted. The air pressure in the cylinder rises to 6-9MPa rapidly, and the temperature also rises to 2000-2500K. Under the push of high-pressure gas, the piston moves downwards and drives the crankshaft to rotate to do work, and the waste gas is exhausted into the atmosphere through the exhaust pipe.
The common diesel engine is driven by an engine camshaft, and diesel oil is delivered to a fuel chamber of each cylinder by a high-pressure oil pump. This fuel supply method is changed according to the change of the engine speed, and the optimum fuel supply amount at various speeds cannot be achieved. The common rail injection system of the electric control diesel engine which is more and more commonly adopted at present can better solve the problem.
The common rail injection type oil supply system consists of a high-pressure oil pump, a public oil supply pipe, an oil injector, an Electronic Control Unit (ECU) and a plurality of pipeline pressure sensors, wherein each oil injector in the system is connected with the public oil supply pipe through a respective high-pressure oil pipe, and the public oil supply pipe plays a hydraulic pressure accumulation role on the oil injector. When the high-pressure oil pump works, fuel oil is conveyed to the public oil supply pipe by the high pressure oil pump, the high-pressure oil pump, the pressure sensor and the ECU form closed-loop work, the oil pressure in the public oil supply pipe is accurately controlled, and the phenomenon that the oil supply pressure changes along with the rotating speed of an engine is thoroughly changed. The method is mainly characterized by comprising the following three aspects:
1. the fuel injection timing is completely separated from the fuel metering, and the fuel injection pressure and the fuel injection process are timely controlled by the ECU.
2. The pressure, initial point and duration of oil injection of each cylinder can be adjusted according to the working condition of the engine, so that the optimal control point of oil injection is pursued.
3. Can realize high oil injection pressure and can realize the pre-injection of diesel oil.
Because the high-pressure common rail diesel engine system is already used on the land and has better effect, but the equipment for working under the condition is still generally provided with the traditional diesel engine system, how to perform explosion-proof transformation on the high-pressure common rail diesel engine system which is already widely used on the land is suitable for underground operation, and the formation of a new high-pressure common rail explosion-proof diesel engine air inlet system is particularly important.
Disclosure of Invention
The invention aims to overcome the defects and provide a novel high-pressure common-rail explosion-proof diesel engine air inlet system which is suitable for underground operation and is formed by carrying out explosion-proof transformation on a high-pressure common-rail diesel engine system which is widely used on land.
The purpose of the invention is realized as follows:
the utility model provides an explosion-proof diesel engine air intake system of high pressure common rail, its characterized in that includes in the past to the back in proper order has the air filter, explosion-proof booster, well cold charge device, the air intake door assembly and the spark arrester of admitting air are up to explosion-proof air intake manifold, wherein the air inlet of explosion-proof booster is connected to the gas outlet of air filter, the pressure boost gas outlet of explosion-proof booster passes through the air inlet of first pressure boost intake-tube connection well cold charge device, the air inlet of air intake door assembly is connected through second pressure boost intake-tube to well cold charge device's gas outlet, the air inlet of the spark arrester of admitting air is connected to the gas outlet of air intake assembly.
Preferably, the intercooling device comprises an intercooling heat exchange cavity body, connecting angle steels are arranged on the left side and the right side of the intercooling heat exchange cavity body, the intercooling heat exchange cavity body is connected to one surface, far away from the explosion-proof diesel engine body, of the heat dissipation water tank through the two connecting angle steels, an intercooling first interface and an intercooling second interface are arranged at the top of the intercooling heat exchange cavity body, the intercooling first interface is an air inlet of the intercooling device and is connected with a first supercharging air inlet pipe, the intercooling second interface is an air outlet of the intercooling device, and the intercooling second interface is connected with a second supercharging air inlet pipe.
Preferably, the caliber of the intercooling air inlet connecting section positioned at the top of the intercooling heat exchange chamber body is gradually reduced inwards from the intercooling first interface, and the caliber of the intercooling air outlet connecting section positioned at the top of the intercooling heat exchange chamber body is gradually reduced inwards from the intercooling second interface.
Preferably, the radiator tank comprises a core, the upper side, the lower side, the left side and the right side of the core are respectively connected with a radiator tank top shell, a radiator tank bottom shell, a radiator tank left side plate and a radiator tank right side plate, the radiator tank left side plate and the radiator tank right side plate are respectively and tightly attached to the left side and the right side of the core, the radiator tank top shell is arranged at the top of the core, the radiator tank top shell is in a hollow state, an upper sealing gasket is further arranged between the bottom of the radiator tank top shell and the top of the core, the top of the radiator tank top shell is provided with two compound water feeding port covers, one side of the radiator tank top shell is connected with a first water return end and a second water return end, the radiator tank bottom shell is erected at the bottom of the core, the radiator tank bottom shell is in a hollow state, an engine oil cooler is, one side of the heat dissipation water tank bottom shell is provided with two water discharging switches, the other side of the heat dissipation water tank bottom shell is connected with a first water discharging end and a second water discharging end, the upper half sections of the outer side surfaces of the heat dissipation water tank left side plate and the heat dissipation water tank right side plate are respectively provided with a handle, the lower half sections of the outer side surfaces of the heat dissipation water tank left side plate and the heat dissipation water tank right side plate are respectively provided with a heat dissipation water tank supporting base, the joints between the heat dissipation water tank supporting base and the heat dissipation water tank left side plate and between the heat dissipation water tank right side plate are provided with reinforcing ribs, one side of the heat dissipation water tank, which is close to the explosion-proof diesel engine main body, is provided with a wind scoop.
Preferably, the air inlet door assembly comprises a door pipeline, an air inlet and an air outlet of the door pipeline are respectively provided with an air inlet connecting flange and an air outlet connecting flange, the top of the outer side of the door pipeline is vertically connected with a door supporting seat in the horizontal direction, an air door cylinder is arranged above the door supporting seat, and a circular air door matched with the inner wall of the door pipeline is arranged in the door pipeline.
As an optimization, the air door is upwards connected with an air door rotating rod, the air door rotating rod upwards extends out of an air door pipeline and an air door supporting seat, the telescopic end of the air door cylinder is connected with the upper end of the air door rotating rod through a swing rod, and the air door can be controlled to be opened and closed through the stretching of the air door cylinder.
Compared with the prior art, the invention has the beneficial effects that:
the high-pressure common rail anti-explosion diesel engine air inlet system is suitable for underground operation, has the advantages of saving energy, reducing emission, reducing noise and improving safety performance, and realizes high-efficiency and environment-friendly operation of underground operation through strict control of various parameters.
Drawings
Fig. 1 is a structural schematic diagram of a high-pressure common-rail explosion-proof diesel engine system.
Fig. 2 is another view of fig. 1.
Fig. 3 is a schematic diagram of the high-pressure common rail system mounted on the explosion-proof diesel engine main body.
FIG. 4 is a schematic diagram of a high pressure common rail system.
Fig. 5 is a schematic diagram of the intercooler device and the radiator tank.
Fig. 6 is another view of fig. 5.
Fig. 7 is a schematic view of an intercooler device.
FIG. 8 is a schematic view of a tail gas treatment tank.
FIG. 9 is a front view of the exhaust treatment housing of FIG. 8 with the front panel removed.
FIG. 10 is a perspective view of the exhaust treatment housing of FIG. 8 with the front panel removed.
FIG. 11 is a front view, in half section, of an intake section within the exhaust treatment housing.
Fig. 12 is a perspective view, in half section, of the intake section within the exhaust treatment housing.
FIG. 13 is another perspective view of the intake section within the exhaust treatment housing.
FIG. 14 is a schematic view of a flow equalization gas guide mechanism.
Fig. 15 is a schematic view of the mounting of the anti-explosion barrier to the barrier mount.
Fig. 16 is a schematic view of an explosion-proof fence.
FIG. 17 is a schematic view of a bar compact.
FIG. 18 is a schematic view of an intake damper assembly.
Fig. 19 is a table for selecting rail pressure.
Fig. 20 is a table for selecting the base injection angle.
Fig. 21 is a table for selecting a water temperature correction injection angle.
Wherein:
explosion-proof diesel engine main body 100, explosion-proof intake manifold 101 and explosion-proof exhaust manifold 102
The high-pressure common rail system 200, a common rail pipeline 201, an oil outlet pipeline 202, an oil nozzle 203, an electromagnetic valve 204, an oil inlet pipeline 205, an oil return pipeline 206 and an oil pump 207
Air filter 300
Explosion-proof supercharger 400
The device comprises an intercooling device 500, an intercooling heat exchange chamber body 501, a connecting angle steel 502, an intercooling first interface 503 and an intercooling second interface 504;
the device comprises a tail gas treatment box 600, a tail gas treatment box body 601, a partition plate 602, a gas inlet flange 603, a tail gas inlet pipe 604, a first waste gas pipe 605, a first waste gas pipe notch 605.1, a tail gas cover plate 606, a second waste gas pipe 607, a third waste gas pipe 608, a third waste gas pipe notch 608.1, a flow equalizing and gas guiding mechanism 609, a circular baffle 610, a vent hole 610.1, a fence seat 611, a fence pressing mechanism 612, a hinge column 612.1, a threaded column 612.2, a pressing bar 612.3, a pin 612.4, a nut 612.5, a guide plate 612.6, a guide column 612.7, a compression spring 612.8, a bar-shaped pressing block 612.9, a pressing block pin 612.10, an explosion-proof fence 613, a limiting column 614, a pressing plate 615, a fence upper cover plate 616, a waste gas pipe 617, a floating ball 618, a floating ball connecting pin 619, a floating ball screw 620, a water replenishing connecting rod 621, a water replenishing valve 622, a water replenishing seat;
air intake system 700, first supercharged air inlet pipe 701 and second supercharged air inlet pipe 702
Exhaust system 800
The air inlet damper comprises an air inlet damper assembly 900, a damper pipeline 901, an air inlet connecting flange 902, an air outlet connecting flange 903, a damper support seat 904, a damper cylinder 905, a damper 906, a damper rotating rod 907 and a swing rod 908;
air intake flame arrester 1000
An explosion-proof exhaust manifold cooling water path 1100, an explosion-proof exhaust manifold water supply pump water inlet pipeline 1101, an explosion-proof exhaust manifold water supply pump 1102, an explosion-proof exhaust manifold water supply pump water outlet pipeline 1103, an explosion-proof supercharger water inlet pipeline 1104, an explosion-proof supercharger water outlet pipeline 1105 and an exhaust bellows water return pipeline 1106
Exhaust bellows 1200
Explosion-proof diesel engine main body cooling water path 1300
The heat-dissipating water tank comprises a heat-dissipating water tank 1400, a core 1401, a heat-dissipating water tank top shell 1402, a heat-dissipating water tank bottom shell 1403, a heat-dissipating water tank left side plate 1404, a heat-dissipating water tank right side plate 1405, an upper sealing gasket 1406, a multiple water filling port cover 1407, a lower sealing gasket 1408, a water discharging switch 1409, a handle 1410, a heat-dissipating water tank support base 1411 and an air guide cover 1412.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1 to 18, the high-pressure common rail explosion-proof diesel engine system according to the present invention includes an explosion-proof diesel engine main body 100, a high-pressure common rail system 200, an air filter 300, an explosion-proof supercharger 400, an inter-cooling device 500, an exhaust gas treatment tank 600, and a heat dissipation water tank 1400, which are connected to each other through a plurality of air pipelines and a plurality of water pipelines; the inter-cooling device 500 and the heat radiation water tank 1400 are installed as a whole;
an explosion-proof intake manifold 101 is arranged at the air inlet end of the explosion-proof diesel engine main body 100, an explosion-proof exhaust manifold 102 is arranged at the exhaust end of the explosion-proof diesel engine main body 100, all air pipelines connected in front of the explosion-proof intake manifold 101 are collectively called an air inlet system 700, and all air pipelines connected behind the explosion-proof exhaust manifold 102 are collectively called an exhaust system 800; the air inlet system 700, the air outlet system 800 and the air path of the explosion-proof diesel engine main body 100 positioned between the air inlet system and the air outlet system form the whole air circulation system of the high-pressure common-rail explosion-proof diesel engine;
the air inlet system 700 sequentially comprises an air filter 300, an explosion-proof supercharger 400, an intercooling device 500, an air inlet air door assembly 900, an air inlet flame arrester 1000 and an explosion-proof air inlet manifold 101 from front to back, wherein an air outlet of the air filter 300 is connected with an air inlet of the explosion-proof supercharger 400, a supercharging air outlet of the explosion-proof supercharger 400 is connected with an air inlet of the intercooling device 500 through a first supercharging air inlet pipe 701, an air outlet of the intercooling device 500 is connected with an air inlet of the air inlet air door assembly 900 through a second supercharging air inlet pipe 702, an air outlet of the air inlet air door assembly 900 is connected with an air inlet of the air inlet flame arrester 1000, and an air outlet of the air inlet flame;
the exhaust system 800 comprises an explosion-proof exhaust manifold 102, an explosion-proof supercharger 400 and a tail gas treatment box 600 from front to back in sequence, an exhaust port of the explosion-proof exhaust manifold 102 is connected with a return air port of the explosion-proof supercharger 400, and an exhaust port of the explosion-proof supercharger 400 is connected with an air inlet of the tail gas treatment box 600 through an exhaust bellows 1200;
an explosion-proof exhaust manifold cooling water path 1100 is led out from a first water outlet end at the bottom of the heat radiation water tank 1400, and the explosion-proof exhaust manifold cooling water path 1100 returns to a first water return end at the top of the heat radiation water tank 1400 after passing through a plurality of components; wherein the explosion-proof exhaust manifold cooling water path 1100 sequentially comprises an explosion-proof exhaust manifold water supply pump water inlet pipeline 1101, an explosion-proof exhaust manifold water supply pump 1102, an explosion-proof exhaust manifold water supply pump water outlet pipeline 1103, an explosion-proof exhaust manifold 102, an explosion-proof supercharger water inlet pipeline 1104, an explosion-proof supercharger 400, an explosion-proof supercharger water outlet pipeline 1105, an exhaust bellows 1200 and an exhaust bellows water return pipeline 1106 from front to back, the water inlet end of the explosion-proof exhaust manifold water supply pump water inlet pipeline 1101 is connected with a first water outlet end at the bottom of the radiating water tank 1400, the water outlet end of the explosion-proof exhaust manifold water supply pump water inlet pipeline 1101 is connected with the water inlet end of the explosion-proof exhaust manifold water supply pump 1102, the water outlet end of the explosion-proof exhaust manifold water supply pump 1102 is connected with the water inlet end of the explosion-proof exhaust manifold water supply pump water outlet pipeline 1103, the, the water outlet end of the explosion-proof exhaust manifold 102 is connected with the water inlet end of an explosion-proof supercharger water inlet pipeline 1104, the water outlet end of the explosion-proof supercharger water inlet pipeline 1104 is connected with the water inlet end of an explosion-proof supercharger 400, the water outlet end of the explosion-proof supercharger 400 is connected with the water inlet end of an explosion-proof supercharger water outlet pipeline 1105, the water outlet end of the explosion-proof supercharger water outlet pipeline 1105 is connected with the water inlet end of an outer water jacket of an exhaust corrugated pipe 1200, the water outlet end of the outer water jacket of the exhaust corrugated pipe 1200 is connected with the water inlet end of an exhaust corrugated pipe water return pipeline 1106, and the water outlet end of the exhaust corrugated pipe water;
the high-pressure common rail system 200 comprises a common rail pipe 201, four oil outlet pipes 202 are connected to the common rail pipe 201, the four oil outlet pipes 202 are respectively connected with four oil nozzles 203, electromagnetic valves 204 are arranged on the oil nozzles, the oil nozzles 203 are arranged on oil inlets of all cylinder bodies of the explosion-proof diesel engine main body 100, an oil inlet pipe 205 and an oil return pipe 206 are further connected to the common rail pipe 201, the oil inlet pipe 205 and the oil return pipe 206 are respectively connected with an oil outlet and an oil return port of an oil pump 207, and the oil pump 207 is connected with an oil tank.
A second water outlet end at the bottom of the heat radiation water tank 1400 leads out an explosion-proof diesel engine main body cooling water path, and the explosion-proof diesel engine main body cooling water path returns to a second water return end at the top of the heat radiation water tank 1400 after passing through a plurality of components; the cooling water path of the main body of the explosion-proof diesel engine sequentially comprises a water inlet pipeline of the main body of the explosion-proof diesel engine, a water supply pump of the main body of the explosion-proof diesel engine, a water path inside the main body of the explosion-proof diesel engine, a temperature controller and a water return pipeline of the main body of the explosion-proof diesel engine from front to back;
the intercooling device 500 comprises an intercooling heat exchange chamber body 501, connecting angle steels 502 are arranged on the left side and the right side of the intercooling heat exchange chamber body 501, the intercooling heat exchange chamber body 501 is connected to one surface, far away from the explosion-proof diesel engine body 100, of the heat dissipation water tank 1400 through the two connecting angle steels 502, an intercooling first interface 503 and an intercooling second interface 504 are arranged on the top of the intercooling heat exchange chamber body 501, wherein the intercooling first interface 503 is an air inlet of the intercooling device 500, the intercooling first interface 503 is connected with a first supercharging air inlet pipe 701, the intercooling second interface 504 is an air outlet of the intercooling device 500, the intercooling second interface 504 is connected with a second supercharging air inlet pipe 702, the caliber of an intercooling air inlet connecting section on the top of the intercooling heat exchange chamber body 501 is gradually reduced from the intercooling first interface 503 inwards, and the caliber of an intercooling air outlet connecting, thereby making the air intake and air outtake smoother.
The heat radiation water tank 1400 comprises a core 1401, a heat radiation water tank top shell 1402, a heat radiation water tank bottom shell 1403, a heat radiation water tank left side plate 1404 and a heat radiation water tank right side plate 1405 are respectively connected to the upper side, the lower side, the left side and the right side of the core 1401, the heat radiation water tank left side plate 1404 and the heat radiation water tank right side plate 1405 are respectively tightly attached to the left side and the right side of the core 1401, the heat radiation water tank top shell 1402 is covered on the top of the core 1401, the heat radiation water tank top shell 1402 is in a hollow state, an upper sealing gasket 1406 is further arranged between the bottom of the heat radiation water tank top shell 1402 and the top of the core 1401, two compound water feeding port covers 1407 are arranged on the top of the heat radiation water tank top shell 1402, one side of the heat radiation water tank top shell 1402 is connected with a first water return end and a second water return end, the heat radiation water tank bottom shell 1403 is erected, a side of heat dissipation water tank drain pan 1403 is provided with two switches 1409 that drain, and the opposite side of heat dissipation water tank drain pan 1403 is connected with first water outlet end and second water outlet end, first section of the lateral surface of heat dissipation water tank left side board 1404 and heat dissipation water tank right side board 1405 all is provided with handle 1410, first section of the lateral surface of heat dissipation water tank left side board 1404 and heat dissipation water tank right side board 1405 all is provided with heat dissipation water tank support base 1411, and the junction between heat dissipation water tank support base 1411 and heat dissipation water tank left side board 1404 and heat dissipation water tank right side board 1405 is provided with the strengthening rib. And a wind scooper 1412 is arranged on one side of the heat dissipation water tank close to the explosion-proof diesel engine main body 100, and four sides of the wind scooper 1412 are respectively connected with the edges of a heat dissipation water tank top shell 1402, a heat dissipation water tank bottom shell 1403, a heat dissipation water tank left side plate 1404 and a heat dissipation water tank right side plate 1405.
The tail gas treatment box 600 comprises a tail gas treatment box body 601, the right section in the tail gas treatment box body 601 is an air inlet section, the left section in the tail gas treatment box body 601 is an air outlet section, the air inlet section and the air outlet section are separated by a partition plate 602, the front end and the rear end of the partition plate 602 are respectively connected with the front inner side wall and the rear inner side wall of the tail gas treatment box body 601, the upper end and the lower end of the partition plate 602 are respectively separated from the upper inner side wall and the lower inner side wall of the tail gas treatment box body 601 by a distance, the right section of the top plate of the tail gas treatment box body 601 is provided with an air inlet flange 603, the air inlet flange 603 is connected with a tail gas inlet pipe 604 to the tail gas treatment box body 601, the lower end of the tail gas inlet pipe 604 is separated from the bottom of the tail gas treatment box body 601 by a distance, the periphery of the middle-lower section of the tail gas inlet pipe 604, the tail gas cover plate 606 is away from the first waste gas pipe 605 by a certain distance, the periphery of the tail gas cover plate 606 is connected with a second waste gas pipe 607 downwards, the pipe diameter of the second waste gas pipe 607 is larger than that of the first waste gas pipe 605, the height of the lower opening of the second waste gas pipe 607 is lower than that of the upper opening of the first waste gas pipe 605, a third waste gas pipe 608 is surrounded at the periphery of the lower end of the tail gas inlet pipe 604, the bottom of the third waste gas pipe 608 is contacted with the bottom of the tail gas treatment box 601, the pipe diameter of the third waste gas pipe 608 is smaller than that of the first waste gas pipe 605, a flow equalizing gas guide mechanism 609 is arranged at the outlet of the lower end of the tail gas inlet pipe 604, the flow equalizing gas guide mechanism 609 is composed of a plurality of flow equalizing gas guide pieces with the same structure, preferably four flow equalizing gas guide pieces, each flow equalizing gas guide piece comprises an upper rectangular piece structure and a lower arc piece, the arc-shaped sheet structure of the plurality of flow-equalizing air guide sheets is bent clockwise from the overlooking angle, the outer edge of the arc-shaped sheet structure is tangent to the outer edge of the rectangular sheet structure, an arc-shaped notch is formed in the inner edge of the arc-shaped sheet structure, the lower end of the flow-equalizing air guide mechanism 609 extends below the lower opening of the tail gas inlet pipe 604, and the outer edge of the rectangular sheet structure of the flow-equalizing air guide sheet of the flow-equalizing air guide mechanism 609 is connected with the interior of the tail gas inlet; a third exhaust pipe notch 608.1 with an upward concave rectangular structure is uniformly arranged at the lower opening of the third exhaust pipe 608, the lower opening of the first exhaust gas pipe 605 is uniformly provided with a first exhaust gas pipe notch 605.1 which is concavely arranged upwards and has a rectangular structure, the third exhaust gas pipe notch 608.1 and the first exhaust gas pipe notch 605.1 are arranged in a staggered manner, the height of the third exhaust gas pipe notch 608.1 is smaller than that of the first exhaust gas pipe notch 605.1, preferably four third exhaust gas pipe notches 608.1 and four first exhaust gas pipe notches 605.1 are provided, a circular baffle plate 610 is arranged inside the third exhaust pipe 608, the height of the circular baffle plate 610 is consistent with the top height of the third exhaust pipe notch 608.1, a plurality of vent holes 610.1 which are vertically communicated are arranged on the circular baffle plate 610, preferably four vent holes 610.1, the positions of the vent holes 610.1 correspond to the position of the first exhaust pipe notch 605.1, namely the positions of the vent holes 610.1 are staggered with the position of the third exhaust pipe notch 608.1;
a fence seat 611 is arranged on the left section of the top plate of the tail gas treatment box 601, the fence seat 611 is of a rectangular frame structure, two vertically arranged fence pressing mechanisms 612 are respectively arranged on the left side frame and the right side frame of the fence seat 611, an anti-explosion fence 613 is upwards arranged on the inner edge of the rectangular frame structure of the fence seat 611, two left limiting columns and right limiting columns 614 are arranged on the front frame of the fence seat 611, the limiting columns 614 are used for front side positioning when the anti-explosion fence 613 is installed, a pressing plate 615 of the rectangular frame structure is connected between the two fence pressing mechanisms 612, the pressing plate 615 is used for pressing the anti-explosion fence 613, the fence pressing mechanism 612 comprises a hinged column 612.1 at the front end and a threaded column 612.2 at the rear end, the top ends of the hinged column 612.1 and the threaded column 38925 are directly connected with a pressing strip 385932, the front end of the pressing strip 2 is connected to the top of the hinged column 612.1 through a pin 612., an opening at the rear end of the pressing bar 612.3 is sleeved outside the top thread of the threaded column 612.2 and is locked by a nut 612.5, guide plates 612.6 which are longitudinally arranged are further arranged on the left and right frames of the fence seat 611, a front guide column 612.7 and a rear guide column 612.7 are upwards arranged on the guide plates 612.6, a compression spring 612.8 is sleeved on the guide columns 612.7, the rear end of the guide plate 612.6 is sleeved outside the bottom end of the threaded column 612.2, positioning holes of the left and right frames of the pressing plate 615 are respectively sleeved on the guide columns 612.7 of the left and right fence pressing mechanisms 612, the pressing plate 615 is positioned above the compression spring 612.8, a strip-shaped hollow which is through in the up-down direction is arranged in the middle of the pressing bar 612.3, a strip-shaped pressing block 612.9 is arranged in the strip-shaped pressing block 612.9, the middle of the strip-shaped pressing block 612.9 is connected with the middle of the pressing bar 612.3 through a transverse pressing block pin 612.10, the middle of the strip-shaped pressing block 612.9 is, so that the force is uniformly applied, a fence upper cover plate 616 is arranged above the anti-explosion fence 613, the fence upper cover plate 616 is connected with a temperature sensor 626, and the fence upper cover plate 616 is connected with an exhaust gas pipe 626 facing to the front lower part.
Be provided with back shroud 617 on the posterior lateral plate of tail gas treatment box 601, be provided with floater 618 in the section of giving vent to anger of tail gas treatment box 601, the lower extreme of floater 618 is connected with floater screw rod 620 through floater connecting pin 619, the one end threaded connection moisturizing connecting rod 621 of floater screw rod 620, moisturizing connecting rod 621 connects moisturizing valve body 622, moisturizing valve body 622 passes through moisturizing seat 623 and connects on the left side wall of tail gas treatment box 601, moisturizing connector 627 is connected to the outer end of moisturizing valve body 622, the left side wall lower extreme of tail gas treatment box 601 is provided with drain 624, be provided with piece formula ball valve 625 on the drain 624.
The air inlet and air door assembly 900 comprises an air door pipeline 901, an air inlet and an air outlet of the air door pipeline 901 are respectively provided with an air inlet connecting flange 902 and an air outlet connecting flange 903, the top of the outer side of the air door pipeline 901 is vertically connected with an air door supporting seat 904 in the horizontal direction, an air door cylinder 905 is arranged above the air door supporting seat 904, a round air door 906 matched with the inner wall of the air door pipeline 901 is arranged in the air door pipeline 901, the air door 906 is upwards connected with an air door rotating rod 907, the air door rotating rod 907 upwards extends out of the air door pipeline 901 and the air door supporting seat 904, the telescopic end of the air door cylinder 905 is connected with the upper end of the air door rotating rod 907 through a swing rod 908, and the air door 906.
A control method of a high-pressure common-rail explosion-proof diesel engine system comprises the following steps:
the high-pressure common rail explosion-proof diesel engine system is provided with a rotating speed sensor, a rail pressure sensor, an air inlet pressure temperature sensor, a cooling liquid temperature sensor and the like, wherein the rotating speed sensor is a crankshaft sensor and is arranged on a flywheel shell, the rotating speed sensor measures the rotating speed of the engine, the rail pressure sensor measures the rail pressure of the high-pressure common rail, the air inlet pressure temperature sensor measures the air inlet pressure and the air inlet temperature, the cooling liquid temperature sensor measures the cooling liquid temperature,
real-time data are transmitted to the ECU through the measurement of the parameters, the ECU calls the tables, and the control system calculates and then controls the opening and closing and the opening of each valve.
Selection of rail pressure referring to Table 1 in FIG. 19 of the specification:
the rail pressure of the real-time high-pressure common rail is controlled through the real-time rotating speed and the oil quantity in the table 1; be provided with rail pressure sensor on the common rail pipeline, rail pressure carries out real-time detection through rail pressure sensor and obtains real-time rail pressure value, obtains the theoretical rail pressure value of rail pressure through the rotational speed data of cam and bent axle, and real-time rail pressure value and theoretical rail pressure value carry out the comparison if there is the difference, then feed back to the high-pressure oil pump, thereby realize through the regulation of high-pressure oil pump that the regulation of real-time rail pressure value makes it tend to theoretical rail pressure value size.
Calculating a real-time injection angle of an oil nozzle of a high-pressure common rail system of the high-pressure common rail explosion-proof diesel engine system at a corresponding moment in real time according to the real-time parameters; the control of the real-time injection angle is controlled by an electromagnetic valve inside the oil injector.
Wherein: real-time spray angle = basic spray angle + water temperature correction spray angle water temperature correction coefficient
Selection of base spray angle referring to table 2 in fig. 20:
selection of water temperature correction injection angle referring to table 3 of fig. 21:
the water temperature correction factor is selected as follows:
the water temperature correction coefficient is 1.5 at minus 30 ℃, 1.25 at minus 20 ℃, 1 at minus 10 ℃, 0 at 0 ℃ and 0 at over 0 ℃, the linear change is a first linear change from minus 30 ℃ to minus 10 ℃, and the linear change is a second linear change from minus 10 ℃ to 0 ℃.
The above is only a specific application example of the present invention, and the protection scope of the present invention is not limited in any way. All the technical solutions formed by equivalent transformation or equivalent replacement fall within the protection scope of the present invention.

Claims (6)

1. The utility model provides an explosion-proof diesel engine air intake system of high pressure common rail, its characterized in that includes air filter (300) in proper order after to in the past, explosion-proof booster (400), well cold charge device (500), air inlet damper assembly (900) and fire arrester (1000) of admitting air until explosion-proof air intake manifold (101), wherein the air inlet of explosion-proof booster (400) is connected to the gas outlet of air filter (300), the air inlet of well cold charge device (500) is connected through first pressure boost intake pipe (701) in the pressure boost gas outlet of explosion-proof booster (400), the air inlet of air inlet damper assembly (900) is connected through second pressure boost intake pipe (702) in the gas outlet of well cold charge device (500), the air inlet of fire arrester (1000) is admitted in the connection of the gas outlet of air inlet damper assembly (900), the air inlet of explosion-proof air intake manifold (101) is connected to.
2. The air intake system of the high-pressure common-rail explosion-proof diesel engine according to claim 1, wherein the inter-cooling device (500) comprises an inter-cooling heat exchange chamber body (501), connecting angle steels (502) are arranged on the left and right sides of the inter-cooling heat exchange chamber body (501), the intercooling heat exchange chamber body (501) is connected to one surface of the heat radiation water tank (1400) far away from the explosion-proof diesel engine body (100) through two connecting angle steels (502), the top of the inter-cooling heat exchange chamber body (501) is provided with an inter-cooling first interface (503) and an inter-cooling second interface (504), the intercooling first interface (503) is an air inlet of the intercooling device (500), the intercooling first interface (503) is connected with the first supercharging air inlet pipe (701), the intercooling second interface (504) is an air outlet of the intercooling device (500), and the intercooling second interface (504) is connected with the second supercharging air inlet pipe (702).
3. The high-pressure common rail explosion-proof diesel engine air inlet system as claimed in claim 2, wherein the caliber of the intercooling air inlet connecting section positioned at the top of the intercooling heat exchange chamber main body (501) is gradually reduced from the intercooling first interface (503) inwards, and the caliber of the intercooling air outlet connecting section positioned at the top of the intercooling heat exchange chamber main body (501) is gradually reduced from the intercooling second interface (503) inwards.
4. The high-pressure common-rail explosion-proof diesel engine air inlet system as claimed in claim 2, wherein the heat-dissipating water tank (1400) comprises a core (1401), the core (1401) is connected with a heat-dissipating water tank top shell (1402), a heat-dissipating water tank bottom shell (1403), a heat-dissipating water tank left side plate (1404) and a heat-dissipating water tank right side plate (1405) at the upper, lower, left and right sides thereof respectively, the heat-dissipating water tank left side plate (1404) and the heat-dissipating water tank right side plate (1405) are respectively and tightly attached to the left and right sides of the core (1401), the heat-dissipating water tank top shell (1402) is covered on the top of the core (1401) and the heat-dissipating water tank top shell (1402) is in a hollow state, an upper sealing gasket (1406) is further arranged between the bottom of the heat-dissipating water tank top shell (1402) and the top of the core (1401), two compound water-adding covers (1407) are arranged, the heat dissipation water tank bottom shell (1403) is erected at the bottom of the core body (1401) and the heat dissipation water tank bottom shell (1403) is in a hollow state, an engine oil cooler is arranged inside the heat dissipation water tank bottom shell (1403), a lower sealing gasket (1408) is further arranged between the heat dissipation water tank bottom shell (1403) and the bottom of the core body (1401), one side surface of the heat dissipation water tank bottom shell (1403) is provided with two water discharging switches (1409), the other side of the heat dissipation water tank bottom shell (1403) is connected with a first water discharging end and a second water discharging end, handles (1410) are arranged on the upper half sections of the outer side surfaces of the heat dissipation water tank left side plate (1404) and the heat dissipation water tank right side plate (1405), heat dissipation water tank supporting bases (1411) are arranged on the lower half sections of the outer side surfaces of the heat dissipation water tank left side plate (1404) and the heat dissipation water tank right side plate (1405), reinforcing ribs are arranged at the joints between, one side of the heat dissipation water tank, which is close to the explosion-proof diesel engine main body (100), is provided with an air guide cover (1412), and four sides of the air guide cover (1412) are respectively connected with the edges of a heat dissipation water tank top shell (1402), a heat dissipation water tank bottom shell (1403), a heat dissipation water tank left side plate (1404) and a heat dissipation water tank right side plate (1405).
5. The air intake system of the high-pressure common-rail explosion-proof diesel engine according to claim 1, wherein the air intake damper assembly (900) comprises a damper pipe (901), an air intake connecting flange (902) and an air outlet connecting flange (903) are respectively arranged at an air intake and an air outlet of the damper pipe (901), an air damper support seat (904) is vertically connected to the top of the outer side of the damper pipe (901) in the horizontal direction, an air damper cylinder (905) is arranged above the air damper support seat (904), and a circular air damper (906) matched with the inner wall of the damper pipe (901) is arranged in the damper pipe (901).
6. The air intake system of the high-pressure common-rail explosion-proof diesel engine according to claim 5, characterized in that the air door (906) is connected with an air door rotating rod (907) upwards, the air door rotating rod (907) extends upwards out of the air door pipeline (901) and the air door supporting seat (904), the telescopic end of the air door cylinder (905) is connected with the upper end of the air door rotating rod (907) through a swing rod (908), and the opening and closing of the air door (906) can be controlled through the telescopic action of the air door cylinder (905).
CN201911098196.1A 2019-11-12 2019-11-12 High-pressure common-rail explosion-proof diesel engine air inlet system Withdrawn CN110657052A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201911098196.1A CN110657052A (en) 2019-11-12 2019-11-12 High-pressure common-rail explosion-proof diesel engine air inlet system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201911098196.1A CN110657052A (en) 2019-11-12 2019-11-12 High-pressure common-rail explosion-proof diesel engine air inlet system

Publications (1)

Publication Number Publication Date
CN110657052A true CN110657052A (en) 2020-01-07

Family

ID=69043343

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201911098196.1A Withdrawn CN110657052A (en) 2019-11-12 2019-11-12 High-pressure common-rail explosion-proof diesel engine air inlet system

Country Status (1)

Country Link
CN (1) CN110657052A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116101897A (en) * 2023-04-13 2023-05-12 山东鲁运智能装备有限公司 Single-rail crane truck of explosion-proof diesel engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116101897A (en) * 2023-04-13 2023-05-12 山东鲁运智能装备有限公司 Single-rail crane truck of explosion-proof diesel engine
CN116101897B (en) * 2023-04-13 2023-06-23 山东鲁运智能装备有限公司 Single-rail crane truck of explosion-proof diesel engine

Similar Documents

Publication Publication Date Title
CN202811059U (en) Piston type composite thermal power system
WO2008148256A1 (en) Two-stroke engine
CN101403350A (en) Internal combustion directly-heating steam engine
CN101289956B (en) Piston reciprocating internal-combustion engine turbocharging device
CN110657052A (en) High-pressure common-rail explosion-proof diesel engine air inlet system
CN102094702B (en) Novel four-stroke layered double-swirling combustion energy-saving internal-combustion engine with new air distribution mechanism
CN1934342A (en) Super-expansion four-stroke internal combustion engine
CN210977720U (en) High-pressure common-rail explosion-proof diesel engine air inlet system
CN210977667U (en) Inter-cooling device
CN210977722U (en) High-pressure common-rail explosion-proof diesel engine system
CN210977660U (en) Water cooling system of high-pressure common-rail explosion-proof diesel engine
CN210977648U (en) High-pressure common-rail explosion-proof diesel engine exhaust system
CN210977719U (en) Air circulation system of high-pressure common-rail explosion-proof diesel engine
CN1814997A (en) Water-sprinkling booster IC engine
CN210977649U (en) Tail gas treatment box
CN110671244A (en) High-pressure common-rail explosion-proof diesel engine system
CN110725742A (en) Water cooling system of high-pressure common-rail explosion-proof diesel engine
CN110657014A (en) High-pressure common-rail explosion-proof diesel engine exhaust system
CN110657040A (en) High-pressure common rail injection control method of high-pressure common rail explosion-proof diesel engine
CN101031705A (en) Engine with water fumigated charge air cooling system
CN110657053A (en) Air circulation system of high-pressure common-rail explosion-proof diesel engine
CN110671180A (en) Tail gas treatment box
CN201013446Y (en) Hybrid power engine
CN201372838Y (en) Turbo-charging six-stroke layering combustion energy-saving gasoline engine
CN213175841U (en) Air inlet control device with air throttle valves independently arranged in cylinders

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
WW01 Invention patent application withdrawn after publication
WW01 Invention patent application withdrawn after publication

Application publication date: 20200107