CN104279050B - In cold integration spiral case - Google Patents
In cold integration spiral case Download PDFInfo
- 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
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- 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.)
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/58—Cooling; Heating; Diminishing heat transfer
- F04D29/582—Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps
- F04D29/5826—Cooling at least part of the working fluid in a heat exchanger
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
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- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
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- 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
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.
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 |
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CN104279050A CN104279050A (en) | 2015-01-14 |
CN104279050B true CN104279050B (en) | 2016-08-31 |
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CN201310273859.5A Active CN104279050B (en) | 2013-07-02 | 2013-07-02 | In cold integration spiral case |
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CN (1) | CN104279050B (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
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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)
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)
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 |
-
2013
- 2013-07-02 CN CN201310273859.5A patent/CN104279050B/en active Active
Patent Citations (4)
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 |
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CN104279050A (en) | 2015-01-14 |
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