EP1692399A1 - K hlungsverfahren - Google Patents
K hlungsverfahrenInfo
- Publication number
- EP1692399A1 EP1692399A1 EP04797255A EP04797255A EP1692399A1 EP 1692399 A1 EP1692399 A1 EP 1692399A1 EP 04797255 A EP04797255 A EP 04797255A EP 04797255 A EP04797255 A EP 04797255A EP 1692399 A1 EP1692399 A1 EP 1692399A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- cooling
- liquid
- compressor wheel
- droplets
- cooling liquid
- 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- Withdrawn
Links
Classifications
-
- 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
- F04D29/70—Suction grids; Strainers; Dust separation; Cleaning
- F04D29/701—Suction grids; Strainers; Dust separation; Cleaning especially adapted for elastic fluid pumps
- F04D29/705—Adding liquids
-
- 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
- F04D29/5846—Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps cooling by injection
Definitions
- the invention relates to the field of exhaust gas powered turbochargers. It relates to a method for cooling the compressor impeller.
- Cooling with a gas is associated with less effort, because the gaseous cooling medium only has to be directed at the component to be cooled and flow around it. Often the gas is not recovered, i.e. no complex circuit and no heat exchanger are necessary. However, the cooling effect is limited.
- the invention has for its object to provide an efficient method for cooling the compressor wheel of an exhaust gas turbocharger.
- a cooling liquid is applied to the surface of the rotating compressor wheel that comes into contact with the gaseous medium to be compressed.
- the coolant evaporates at least partially due to the high temperatures of the compressor wheel.
- the temperature of the coolant drops and the cooled liquid thus has a cooling effect on the compressor wheel.
- the cooling liquid is advantageously applied to the surface of the compressor wheel by supplying the cooling liquid to the gaseous medium upstream of the compressor wheel.
- the figure shows schematically the cooling according to the invention on a compressor wheel. Way of carrying out the invention
- An exhaust gas turbocharger mainly consists of a compressor and an exhaust gas turbine.
- the compressor mainly comprises a housing and a compressor wheel arranged rotatably on a shaft in the housing.
- the housing surrounds an inflow channel, through which the air, as the medium to be compressed, is guided to the compressor wheel.
- the air is compressed by blades on the compressor wheel and then fed to a fuel engine through an outflow channel.
- an evaporable cooling liquid is added to the medium to be compressed upstream of the compressor wheel, that is to say before the flow reaches the compressor wheel and is consequently still not compressed and has a correspondingly low temperature.
- the cooling liquid is water or a water mixture.
- the cooling liquid is advantageously injected into the flow channel as a mist from many very fine droplets by means of at least one nozzle.
- the droplets advantageously have a diameter of less than 20 micrometers, with special nozzles even droplets with a diameter of less than 3 micrometers can be produced. The finer the droplets, the better the vaporizability. Shortly after the injection, due to the high friction heat mixing with the strong flow, the droplets partially evaporate, which lowers the temperature of the sprayed liquid mist.
- the compressor wheel must compress the combustion air for the engine as high as possible. Although the air is heated by the compression, the static temperature in the compressor channels is not particularly high due to the fast main flow in the compressor channels. However, heat flows which is formed by the deceleration and the intense friction on the back of the compressor wheel, from the back through the material of the compressor wheel and is released into the main flow via the surface.
- the droplets 21 come close to or against the wall of the compressor wheel 1, they are braked in the boundary layer (a) and can form a thin film 22.
- This film from the injected coolant absorbs heat on the one hand from the hot compressor wheel (e) and on the other hand due to friction from the main flow 3, since the speed difference between the main flow and the area of the film is much higher (b). Because of this heat absorption, at least a part of the film 23 is removed in gaseous form in the flow 3 by evaporation (c). The unevaporated part of the liquid film 24 is released into the flow again by the large, centrifugal forces (d). The evaporation has a cooling effect on the film and on the surface of the compressor wheel.
- the surface temperature is in the range of the so-called "wet bulb” temperature, i.e. the temperature that a moistened thermometer measures in the flow and which is lower than the temperature of the flow.
- the method according to the invention is extremely efficient.
- the use of the cooling method according to the invention is particularly interesting for compressors of turbochargers, since the compressor wheel is very difficult to cool with other methods.
- cooling the main flow improves compressor efficiency and water vapor reduces the NOx emissions of the internal combustion engine connected to the turbocharger.
- the compressor wheels of ordinary turbochargers are made of aluminum for economic reasons.
- the creep rupture strength of the material decreases very strongly with the temperature, which is the limit of use of aluminum compressors today limited to pressure ratios of about 5. If water is injected into the air flow shortly before the wheel enters, a significant reduction in the material temperature can be achieved, which allows pressure ratios up to 6 or 7 to be reached without having to switch to materials that are sometimes more expensive, such as titanium.
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)
- Supercharger (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE2003157711 DE10357711A1 (de) | 2003-12-09 | 2003-12-09 | Kühlungsverfahren |
PCT/CH2004/000698 WO2005057019A1 (de) | 2003-12-09 | 2004-11-19 | Kühlungsverfahren |
Publications (1)
Publication Number | Publication Date |
---|---|
EP1692399A1 true EP1692399A1 (de) | 2006-08-23 |
Family
ID=34672546
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP04797255A Withdrawn EP1692399A1 (de) | 2003-12-09 | 2004-11-19 | K hlungsverfahren |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP1692399A1 (de) |
DE (1) | DE10357711A1 (de) |
WO (1) | WO2005057019A1 (de) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102004028224A1 (de) * | 2004-06-09 | 2006-01-05 | Man B & W Diesel Ag | Verfahren zum Betreiben eines Turboladers sowie Turbolader |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB705387A (en) * | 1951-02-15 | 1954-03-10 | Power Jets Res & Dev Ltd | Improvements relating to radial-flow turbine or centrifugal compressors |
DE1056426B (de) * | 1951-05-16 | 1959-04-30 | Power Jets Res & Dev Ltd | Kuehleinrichtung an Gasturbinenanlagen |
JPH03130503A (ja) * | 1989-10-13 | 1991-06-04 | Jinichi Nishiwaki | ガスタービン高温部の水冷却方法 |
US6389799B1 (en) * | 1997-04-22 | 2002-05-21 | Hitachi, Ltd. | Gas turbine Installation |
NL1011383C2 (nl) * | 1998-06-24 | 1999-12-27 | Kema Nv | Inrichting voor het comprimeren van een gasvormig medium en systemen die een dergelijke inrichting omvatten. |
DE10390644B4 (de) * | 2002-02-19 | 2019-07-25 | Ansaldo Energia Switzerland AG | Turboverdichter und Verfahren zum Betrieb eines Turboverdichters |
-
2003
- 2003-12-09 DE DE2003157711 patent/DE10357711A1/de not_active Withdrawn
-
2004
- 2004-11-19 EP EP04797255A patent/EP1692399A1/de not_active Withdrawn
- 2004-11-19 WO PCT/CH2004/000698 patent/WO2005057019A1/de active Application Filing
Non-Patent Citations (1)
Title |
---|
See references of WO2005057019A1 * |
Also Published As
Publication number | Publication date |
---|---|
DE10357711A1 (de) | 2005-07-14 |
WO2005057019A1 (de) | 2005-06-23 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): DE FI NL |
|
17P | Request for examination filed |
Effective date: 20060516 |
|
DAX | Request for extension of the european patent (deleted) | ||
RBV | Designated contracting states (corrected) |
Designated state(s): DE FI NL |
|
17Q | First examination report despatched |
Effective date: 20091020 |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
INTG | Intention to grant announced |
Effective date: 20130705 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN |
|
18D | Application deemed to be withdrawn |
Effective date: 20131116 |