CN107120218A - Cryogenic gas bypass type temperature control air inlet pipe - Google Patents

Cryogenic gas bypass type temperature control air inlet pipe Download PDF

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Publication number
CN107120218A
CN107120218A CN201710516199.7A CN201710516199A CN107120218A CN 107120218 A CN107120218 A CN 107120218A CN 201710516199 A CN201710516199 A CN 201710516199A CN 107120218 A CN107120218 A CN 107120218A
Authority
CN
China
Prior art keywords
cryogenic gas
air inlet
inlet pipe
temperature control
engine
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
CN201710516199.7A
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Chinese (zh)
Inventor
赵红兵
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.)
Weichai Xigang New Energy Power Co Ltd
Original Assignee
Weichai Xigang New Energy Power 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 Weichai Xigang New Energy Power Co Ltd filed Critical Weichai Xigang New Energy Power Co Ltd
Priority to CN201710516199.7A priority Critical patent/CN107120218A/en
Publication of CN107120218A publication Critical patent/CN107120218A/en
Pending legal-status Critical Current

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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
    • F02M35/104Intake manifolds
    • 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
    • F02B29/0481Intake air cooling by means others than heat exchangers, e.g. by rotating drum regenerators, cooling by expansion or by electrical means
    • 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

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Abstract

The invention discloses a kind of cryogenic gas bypass type temperature control air inlet pipe, belong to cold technical field of temperature control in engine charge, including air inlet tube body, air inlet and exhaust outlet are offered on the air inlet tube body, cryogenic gas entrance and cryogenic gas outlet are additionally provided with the air inlet tube body, the air inlet pipe body interior is provided with cryogenic gas pipeline, and the cryogenic gas pipeline is respectively communicated with the cryogenic gas entrance and cryogenic gas outlet.The present invention reduces Engine Inlet Temperature, it is ensured that engine causes in high environment temperature, high cabin temperature etc. under the high environment of Engine Inlet Temperature, the dynamic property and reliability and good economy of engine by introducing cryogenic gas.

Description

Cryogenic gas bypass type temperature control air inlet pipe
Technical field
The invention belongs to cold technical field of temperature control in engine charge, more particularly to a kind of cryogenic gas bypass type temperature Control air inlet pipe.
Background technology
Engine can operationally produce very high temperature, and engine is typically mounted in closed space, so Temperature can be caused in enging cabin apparently higher than environment temperature.When ambient temperature is high, such as, in hot summer, start Machine is deteriorated with extraneous heat exchange, and natively ambient temperature is high in addition for the engine of high temperature, directly results in engine charge Temperature is too high, can at this time cause many problems, such as dynamic property is poor, less economical, combustion knock etc., can cause when serious Parking, or even engine are scrapped.
The content of the invention
The technical problems to be solved by the invention are:A kind of cryogenic gas bypass type temperature control air inlet pipe is provided, to solve hair Motivation intake air temperature height causes the technical problem of various faults.
In order to solve the above technical problems, the technical scheme is that:Cryogenic gas bypass type temperature control air inlet pipe, including enter Offered on tracheae body, the air inlet tube body and be additionally provided with cryogenic gas on air inlet and exhaust outlet, the air inlet tube body Entrance and cryogenic gas outlet, the air inlet pipe body interior are provided with cryogenic gas pipeline, and the cryogenic gas pipeline connects respectively Logical cryogenic gas entrance and the cryogenic gas outlet.
As an improvement, the cryogenic gas pipeline includes helical pipe and the rectilinear duct linked together, described Rectilinear duct is located inside the helical pipe.
As an improvement, the air inlet tube body includes housing and the cover plate positioned at the shell one end, the air inlet Mouth and the exhaust outlet are respectively arranged on the two side of the housing, and cryogenic gas entrance and the cryogenic gas outlet is located at described The outside of cover plate, the cryogenic gas pipeline is located at the inner side of the cover plate.
As an improvement, the cryogenic gas is the liquefied natural gas after vaporization or the compressed natural gas after decompression.
Employ after above-mentioned technical proposal, the beneficial effects of the invention are as follows:
Because the air inlet tube body of cryogenic gas bypass type temperature control air inlet pipe is provided with cryogenic gas entrance and cryogenic gas Outlet, the air inlet pipe body interior is provided with cryogenic gas pipeline, and the cryogenic gas pipeline is respectively communicated with the cryogenic gas Entrance and cryogenic gas outlet, thus when Engine Inlet Temperature is high, drawn cryogenic gas by cryogenic gas entrance Enter cryogenic gas pipeline, heat exchange is carried out with the intrinsic high-temperature gas of air inlet pipe, reach the effect of reduction Engine Inlet Temperature Really, the cryogenic gas after heat exchange is exported by cryogenic gas and discharged;When Engine Inlet Temperature is low, blocked by outside control The supply of cryogenic gas, so as to be unlikely to make the cold start-up of the too low influence engine of intake air temperature.
The cryogenic gas bypass type temperature control air inlet pipe that the present invention is provided, by introducing cryogenic gas, reduces engine and enters Temperature degree, it is ensured that engine causes in high environment temperature, high cabin temperature etc. under the high environment of Engine Inlet Temperature, engine Dynamic property and reliability and good economy.
Because the cryogenic gas pipeline includes the helical pipe linked together and rectilinear duct, thus pass through helix tube Road can increase the circulation area of cryogenic gas so that good effect of heat exchange.
Because the air inlet tube body includes housing and the cover plate positioned at the shell one end, thus facilitate manufacture and pacify Dress.
Brief description of the drawings
Fig. 1 is the structural representation of the embodiment of the present invention;
In figure:1- air inlet tube bodies, 11- housings, 12- cover plates, 2- air inlets, 3- exhaust outlets, 4- cryogenic gas entrances, 5- Cryogenic gas is exported, 6- cryogenic gas pipelines, 61- helical pipes, 62- rectilinear ducts.
Embodiment
In order to make the purpose , technical scheme and advantage of the present invention be clearer, it is right below in conjunction with drawings and Examples The present invention is further elaborated.It should be appreciated that the specific embodiments described herein are merely illustrative of the present invention, and It is not used in the restriction present invention.
As shown in figure 1, a kind of cryogenic gas bypass type temperature control air inlet pipe, including air inlet tube body 1, on air inlet tube body 1 Offer and cryogenic gas entrance 4 and cryogenic gas outlet 5, air inlet pipe are additionally provided with air inlet 2 and exhaust outlet 3, air inlet tube body 1 The inside of body 1 is provided with cryogenic gas pipeline 6, and cryogenic gas pipeline 6 is respectively communicated with cryogenic gas entrance 4 and cryogenic gas outlet 5.
In order to obtain good heat transfer effect, it is preferred that cryogenic gas pipeline 6 includes the helical pipe 61 linked together With rectilinear duct 62, rectilinear duct 62 is located inside helical pipe 61, so can increase cryogenic gas by helical pipe 61 Circulation area.In the present embodiment, the connection cryogenic gas of helical pipe 61 entrance 4, the connection cryogenic gas of rectilinear duct 62 goes out Mouth 5.Certainly, alternatively, it would however also be possible to employ the connection cryogenic gas of helical pipe 61 outlet 5, rectilinear duct 62 connects Connect cryogenic gas entrance 4.
Manufacture and install for convenience, in the present embodiment, above-mentioned air inlet tube body 1 includes housing 11 and positioned at housing 11 The cover plate 12 of one end, air inlet 2 and exhaust outlet 3 are respectively arranged on the two side of housing 11, and exhaust outlet 3 has four, and cryogenic gas enters Mouth 4 and cryogenic gas outlet 5 are located at the outsides of cover plate 12, and cryogenic gas pipeline 6 is located at the inner side of cover plate 12.
In natural gas engine, because the natural gas depressurization that hydraulic gas is vaporized after absorbing heat or compressing can also be inhaled Heat, cryogenic gas can be from the liquefied natural gas after vaporization or the compressed natural gas after decompression.
Its operation principle is as follows:
When Engine Inlet Temperature is high, cryogenic gas is introduced by cryogenic gas pipeline 6 by cryogenic gas entrance 4, with High-temperature gas in air inlet tube body 1 carries out heat exchange, reaches the effect of reduction Engine Inlet Temperature, the low temperature gas after heat exchange Body is discharged by cryogenic gas outlet 5;When Engine Inlet Temperature is low, the supply of cryogenic gas is blocked by outside control, So as to be unlikely to the cold start-up for making the too low influence engine of intake air temperature.
Cryogenic gas bypass type temperature control air inlet pipe provided in an embodiment of the present invention, by introducing cryogenic gas, reduces hair Motivation intake air temperature, it is ensured that engine causes in high environment temperature, high cabin temperature etc. under the high environment of Engine Inlet Temperature, The dynamic property and reliability and good economy of engine.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all essences in the present invention Any modifications, equivalent substitutions and improvements made within refreshing and principle etc., should be included in the scope of the protection.

Claims (4)

1. offered on cryogenic gas bypass type temperature control air inlet pipe, including air inlet tube body, the air inlet tube body air inlet and Exhaust outlet, it is characterised in that cryogenic gas entrance and cryogenic gas outlet, the air inlet pipe are additionally provided with the air inlet tube body Body interior is provided with cryogenic gas pipeline, and the cryogenic gas pipeline is respectively communicated with the cryogenic gas entrance and the low temperature gas Body is exported.
2. cryogenic gas bypass type temperature control air inlet pipe according to claim 1, it is characterised in that the cryogenic gas pipeline Including the helical pipe linked together and rectilinear duct, the rectilinear duct is located inside the helical pipe.
3. cryogenic gas bypass type temperature control air inlet pipe according to claim 1, it is characterised in that the air inlet tube body bag Housing and the cover plate positioned at the shell one end are included, the air inlet and the exhaust outlet are respectively arranged on the both sides of the housing Wall, cryogenic gas entrance and the cryogenic gas outlet is located at the outside of the cover plate, and the cryogenic gas pipeline is located at described The inner side of cover plate.
4. cryogenic gas bypass type temperature control air inlet pipe according to claim 1, it is characterised in that the cryogenic gas is vapour The compressed natural gas after liquefied natural gas or decompression after change.
CN201710516199.7A 2017-06-29 2017-06-29 Cryogenic gas bypass type temperature control air inlet pipe Pending CN107120218A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710516199.7A CN107120218A (en) 2017-06-29 2017-06-29 Cryogenic gas bypass type temperature control air inlet pipe

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710516199.7A CN107120218A (en) 2017-06-29 2017-06-29 Cryogenic gas bypass type temperature control air inlet pipe

Publications (1)

Publication Number Publication Date
CN107120218A true CN107120218A (en) 2017-09-01

Family

ID=59719799

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710516199.7A Pending CN107120218A (en) 2017-06-29 2017-06-29 Cryogenic gas bypass type temperature control air inlet pipe

Country Status (1)

Country Link
CN (1) CN107120218A (en)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1995030083A1 (en) * 1994-04-28 1995-11-09 Citimotors, Inc. Natural gas powered engine with inlet air and natural gas temperature control
CN102226432A (en) * 2011-06-11 2011-10-26 张海辉 Gas temperature control pipeline for gas engine
CN103206874A (en) * 2013-03-28 2013-07-17 尚小女 Automobile exhaust gas heat exchanger
EP2693146A1 (en) * 2012-08-03 2014-02-05 Dworek Polski Sp.J. Heat exchanger for sewer riser
CN104234777A (en) * 2013-06-18 2014-12-24 济南吉美乐电源技术有限公司 Device universal for low-temperature start of diesel engine
CN205119886U (en) * 2015-11-11 2016-03-30 雅安市名山区永祥茶机制造有限公司 Energy -saving heat exchanger
CN206845354U (en) * 2017-06-29 2018-01-05 潍柴西港新能源动力有限公司 Cryogenic gas bypass type temperature control air inlet pipe

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1995030083A1 (en) * 1994-04-28 1995-11-09 Citimotors, Inc. Natural gas powered engine with inlet air and natural gas temperature control
CN102226432A (en) * 2011-06-11 2011-10-26 张海辉 Gas temperature control pipeline for gas engine
EP2693146A1 (en) * 2012-08-03 2014-02-05 Dworek Polski Sp.J. Heat exchanger for sewer riser
CN103206874A (en) * 2013-03-28 2013-07-17 尚小女 Automobile exhaust gas heat exchanger
CN104234777A (en) * 2013-06-18 2014-12-24 济南吉美乐电源技术有限公司 Device universal for low-temperature start of diesel engine
CN205119886U (en) * 2015-11-11 2016-03-30 雅安市名山区永祥茶机制造有限公司 Energy -saving heat exchanger
CN206845354U (en) * 2017-06-29 2018-01-05 潍柴西港新能源动力有限公司 Cryogenic gas bypass type temperature control air inlet pipe

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Application publication date: 20170901

RJ01 Rejection of invention patent application after publication