Nothing Special   »   [go: up one dir, main page]

CN104279050B - In cold integration spiral case - Google Patents

In cold integration spiral case Download PDF

Info

Publication number
CN104279050B
CN104279050B CN201310273859.5A CN201310273859A CN104279050B CN 104279050 B CN104279050 B CN 104279050B CN 201310273859 A CN201310273859 A CN 201310273859A CN 104279050 B CN104279050 B CN 104279050B
Authority
CN
China
Prior art keywords
spiral case
air cooler
charge air
cold
annular charge
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.)
Active
Application number
CN201310273859.5A
Other languages
Chinese (zh)
Other versions
CN104279050A (en
Inventor
陈化
王增全
程江华
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.)
No70 Institute Of China North Industries Group Corp
Original Assignee
No70 Institute Of China North Industries Group Corp
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 No70 Institute Of China North Industries Group Corp filed Critical No70 Institute Of China North Industries Group Corp
Priority to CN201310273859.5A priority Critical patent/CN104279050B/en
Publication of CN104279050A publication Critical patent/CN104279050A/en
Application granted granted Critical
Publication of CN104279050B publication Critical patent/CN104279050B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/58Cooling; Heating; Diminishing heat transfer
    • F04D29/582Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps
    • F04D29/5826Cooling at least part of the working fluid in a heat exchanger
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/4206Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The present invention relates to cold integration spiral case in one, spiral case (5) with metal pattern compression casting be molded in be provided with in cold front gas channel (3), in cold rear gas channel (7), in cold front gas channel (3) and in be provided with annular charge air cooler (6) between cold rear gas channel (7), annular charge air cooler (6) is internally provided with reinforcement heat transfer radiating fin (14), radiating fin (14) points to and has angle and consistent with airflow direction with tangential direction, airflow inlet (1) it is provided with on spiral case (5), air stream outlet (8), cooling water intake (9) and delivery port (10), cooling water intake (9) and cooling water outlet (10) are in 180 ° of layouts of circumference.The present invention reduces the temperature of air after compression, improves engine power.While engine power lifting and thermic load and delivery temperature improvement, reduce the physical dimension of engine.

Description

In cold integration spiral case
Technical field
The present invention relates to turbo-charger technical field, be specifically related to cold integration spiral case in one.
Background technology
Engine improves charge density after supercharging, and then increases engine power, improves engine consumption.But with Pressure ratio to increase, the air themperature of blower outlet also increases, and limits the raising of charge density to a certain extent, Therefore often add charge air cooler after supercharging engine charge is cooled down.Experience have shown that, under given boost pressure, increase Pressure air themperature often declines 10 DEG C, and its density about increases 3%, when air oil consumption rate all keeps constant, and the merit of diesel engine Rate also can improve 3%.Along with the increase of engine power density, this effect can become apparent from.In order to increase the effect needs of cooling Increase the volume of charge air cooler, but the excessive charge air cooler of volume is unallowable for vehicular engine, even some car With engine due to the restriction in space, it is impossible to install charge air cooler.
Summary of the invention
In one cold integration spiral case, it include airflow inlet 1, impeller 2, diffuser 3, back of the body dish 4, compressor volute 5, Annular charge air cooler 6, gas channel 7, air stream outlet 8, water inlet 9, delivery port 10, O-ring seal 11, O-ring seal 12, fluid sealant Circle 13, after impeller 2 is arranged on the airflow inlet 1 of compressor volute 5, annular charge air cooler 6 is arranged in the gas channel 7 of annular, Compressor volute 5, the cavity between back of the body dish 4 and annular charge air cooler 6 is diffuser 3, and water inlet 9 is arranged on compressor volute 5 Bottom, delivery port 10 is arranged on compressor volute 5 top.
Fin 14 in described annular charge air cooler 6 is 20-60 degree with tangential direction angle.
Described annular charge air cooler 6 is fixed with back of the body dish 4 by the internal concave station of compressor volute 5.
In described, cold integration spiral case is provided with water inlet 9 and the delivery port of a cooling water of at least one cooling water 10, and water inlet 9 is circumferentially distributed in 180 ° with delivery port 10.
Described compressor volute 5 uses metal pattern compression casting to be molded.
Described annular charge air cooler 6 axial dimension L is at least 0.08 times of impeller 2 outlet diameter, annular charge air cooler 6 internal diameter D1 is at least 1.2 with the ratio of impeller 2 outlet diameter, and annular charge air cooler 6 outside diameter d 2 is 1.5 with the ratio of impeller 2 outlet diameter ~3。
Beneficial effects of the present invention:
The present invention uses and adds annular charge air cooler 6 between diffuser 3 and gas channel 7, by annular charge air cooler 6 The heat that after absorbing compression, fresh air transmits, reduces compressed-air actuated temperature.Inventive structure is simple, not only possesses routine and calms the anger The effect of machine spiral case, it is also possible to bear charge air cooler and reduce the effect of pressurization gas temperature, promotes and heat in engine power While load and delivery temperature are improved, decrease the physical dimension of engine.
Accompanying drawing explanation
Fig. 1 is the structural representation of cold integration spiral case in being;
Fig. 2 is the structural profile schematic diagram of cold integration spiral case in being;
Fig. 3 is the structural profile schematic diagram of annular charge air cooler;
Fig. 4 is annular charge air cooler Inlet and outlet water direction schematic diagram.
Detailed description of the invention
Fresh air enters compressor volute 5 by airflow inlet 1, and after impeller 2 acting compression, pressure and temp raises Enter cold front gas channel 3 diffusion reduction of speed in diffuser, colder in entering after annular charge air cooler 6 cooling after gas channel 7 Collected by it, transport to engine air inlet tube eventually through air stream outlet 8 or other use device of air.Cycle of engine cooling water is by entering The mouth of a river 9 enters annular charge air cooler 6, absorbs the high temperature gas flow heat of annular charge air cooler 6 transmission, reduces compressed-air actuated temperature, then Flowed out by cooling water outlet 10.

Claims (6)

1. a cold integration spiral case in, it includes airflow inlet (1), impeller (2), diffuser (3), back of the body dish (4), compressor Spiral case (5), annular charge air cooler (6), gas channel (7), air stream outlet (8), water inlet (9), delivery port (10), O-ring seal (11), O-ring seal (12), O-ring seal (13), it is characterised in that impeller (2) is arranged on the airflow inlet of compressor volute (5) (1), in, annular charge air cooler (6) is arranged in the gas channel (7) of annular, compressor volute (5) and annular charge air cooler (6) it Between cavity be diffuser (3), water inlet (9) is arranged on the bottom of compressor volute (5), and delivery port (10) is arranged on compressor Spiral case (5) top.
Cold integration spiral case in one the most according to claim 1, it is characterised in that in described annular charge air cooler (6) Fin (14) and air-flow tangential direction angle are 20-60 degree.
Cold integration spiral case in one the most according to claim 1, it is characterised in that described annular charge air cooler (6) passes through The internal concave station of compressor volute (5) is fixed with back of the body dish (4).
Cold integration spiral case in one the most according to claim 1, it is characterised in that in described, cold integration spiral case sets It is equipped with at least one cooling water inlet (9) of water and a delivery port (10) cooling down water, and water inlet (9) and delivery port (10) circumferentially distributed in 180 °.
Cold integration spiral case in one the most according to claim 1, it is characterised in that described compressor volute (5) uses Metal pattern compression casting is molded.
Cold integration spiral case in one the most according to claim 1, it is characterised in that described annular charge air cooler (6) axially chi Very little L is at least 0.08 times of impeller (2) outlet diameter, annular charge air cooler (6) internal diameter d1 and the ratio of impeller (2) outlet diameter At least 1.2, annular charge air cooler (6) outside diameter d 2 is 1.5 ~ 3 with the ratio of impeller (2) outlet diameter.
CN201310273859.5A 2013-07-02 2013-07-02 In cold integration spiral case Active CN104279050B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310273859.5A CN104279050B (en) 2013-07-02 2013-07-02 In cold integration spiral case

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310273859.5A CN104279050B (en) 2013-07-02 2013-07-02 In cold integration spiral case

Publications (2)

Publication Number Publication Date
CN104279050A CN104279050A (en) 2015-01-14
CN104279050B true CN104279050B (en) 2016-08-31

Family

ID=52254319

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310273859.5A Active CN104279050B (en) 2013-07-02 2013-07-02 In cold integration spiral case

Country Status (1)

Country Link
CN (1) CN104279050B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115217737B (en) * 2022-07-11 2023-12-22 珠海格力电器股份有限公司 Heat radiation structure of multistage compressed gas and multistage compressor

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007023142A1 (en) * 2007-05-16 2008-11-20 Audi Ag Exhaust gas compressor for automotive exhaust gas turbocharger has spiral wall incorporating cooling duct
CN101943034A (en) * 2010-09-18 2011-01-12 中国兵器工业集团第七○研究所 Water-cooled gas compressor spiral housing
CN102168607A (en) * 2011-05-25 2011-08-31 中国兵器工业集团第七○研究所 Inter-cooling integral volute
EP1832754A3 (en) * 2006-03-08 2014-04-02 Behr GmbH & Co. KG Supercharger for a combustion motor, heat exchanger

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7278472B2 (en) * 2002-09-20 2007-10-09 Modine Manufacturing Company Internally mounted radial flow intercooler for a combustion air changer

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1832754A3 (en) * 2006-03-08 2014-04-02 Behr GmbH & Co. KG Supercharger for a combustion motor, heat exchanger
DE102007023142A1 (en) * 2007-05-16 2008-11-20 Audi Ag Exhaust gas compressor for automotive exhaust gas turbocharger has spiral wall incorporating cooling duct
CN101943034A (en) * 2010-09-18 2011-01-12 中国兵器工业集团第七○研究所 Water-cooled gas compressor spiral housing
CN102168607A (en) * 2011-05-25 2011-08-31 中国兵器工业集团第七○研究所 Inter-cooling integral volute

Also Published As

Publication number Publication date
CN104279050A (en) 2015-01-14

Similar Documents

Publication Publication Date Title
CN101943034A (en) Water-cooled gas compressor spiral housing
CN105401986A (en) Flow channel arrangement structure of aero-engine high-pressure turbine cooling air
CN201133280Y (en) Engine central cooling system
CN104279050B (en) In cold integration spiral case
CN202883178U (en) Intake manifold with diversion structure
CN102168607A (en) Inter-cooling integral volute
CN201802460U (en) Cooler capable of high efficiency exhaust
CN103925069A (en) Intercooler for fire protection diesel engine
CN201843666U (en) Improved exhaust pipe for special vehicles
CN105332783B (en) The cooling system that water-cooled diesel engine integrated form axle center is arranged symmetrically
CN204610020U (en) A kind of vehicle intercooler
CN203515787U (en) Intercooler for firefighting diesel engine
CN202832673U (en) Turbosupercharger middle body
CN203271891U (en) Semi-shell-type exhaust branch pipe
CN207004624U (en) A kind of cold middle cold type charge air-cooling system of engine water
CN202811371U (en) Counter flow cooling structure of single-stage negative pressure Roots blower
CN203441592U (en) Low temperature cooling device applied to two stage turbocharged diesel engine
JP2013060820A (en) Arrangement structure of two-stage supercharging system
CN205908363U (en) Take water tank structure of intercooler
CN203769929U (en) Water and air mixed type intercooler
CN205533444U (en) A sound quality regulator for exhaust gas turbocharger compressor side of giving vent to anger
CN203201650U (en) Double-interface intercooler with high fluidity of gas
CN205400895U (en) Novel modified magnetic adsorption type car intercooler
CN202294785U (en) Automobile
CN206487550U (en) A kind of vapour vehicle tail gas and water burner again

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant