The present invention relates to a multi-stage jet suction pump for aspirating blow-by gases from internal combustion engines.
In order to reduce the negative pressure in the engine or to compensate for the pressure rise caused by an oil separator, active pumps for internal combustion engines are employed that actively aspirate blow-by gases, for example, by vacuum pumps or impeller pumps.
A disadvantage of jet suction pumps is their relatively poor efficiency. These pumps only utilize a small portion of the energy fed from the charged region behind the turbocharger in the form of pressurized air.
DE 10 2013 203 942 A1 describes a jet suction pump with a fuel line, a propulsion jet nozzle, an aspiration zone, a mixing tube, and a diffuser, wherein said propulsion jet nozzle and said mixing tube are oriented straight with respect to one another. As viewed in the flow direction, the diffuser has a course that deviates from the course of the mixing tube.
In DE 20 2006 001 287 U1, a jet suction pump that controls the negative pressure for the venting of an internal combustion engine in combination with a pressure control valve is provided as the pump.
In DE 44 00 958 C1, a multi-stage jet suction pump for a fuel pump is provided for improving the function thereof. Because of the multi-stage nature (two-stage, three-stage, four-stage, etc.) of the jet suction pump, the efficiency of the pump can be clearly increased. A liquid is conveyed in this case.
It is the object of the present invention to reduce the negative pressure in the engine, or to compensate for the pressure rise caused by an oil separator.
The present invention is illustrated and described herein with reference to the various drawings, in which like reference numbers denote like method steps and/or system components, respectively, and in which:
According to the invention, the above object is achieved in a first embodiment by a jet suction pump 7 for venting an internal combustion engine with a turbocharger 3 between an air filter 1 and a crankcase 4, characterized in that a charge air duct 5 has a branch to an at least two-stage jet suction pump 7, wherein the inlet of said jet suction pump 7 is connected with the crankcase 4 through the engine ventilation 6, and the outlet of said jet suction pump 7 is connected with the suction duct 2 between the air filter 1 and the turbocharger 3 for recirculating blow-by gas 9.
Multi-stage jet suction pumps 7 are particularly suitable for the present purpose, because the absence of moving parts leads one to expect a wear-free pump 7.
The multi-stage pump 7 acts by pressing a propulsion jet (e.g., pressurized air from the charged suction tube) through a small nozzle 10, so that the jet entrains gas at its circumference. After the first stage, the volume flow increased by the supply air is subsequently flowed through a second, larger, nozzle 12 and a third, even larger, nozzle 14, wherein a proportion of gas is again entrained.
At each nozzle 10, 12, 14, the propulsion jet entrains a fraction of the gas to be conveyed (blow-by gas). Because of the multi-stage property, the volume flow conveyed becomes significantly larger (a factor of 2, 3 or more) as with a one-stage jet suction pump. The more, the better.
Because of this improved efficiency, the conveyed volume flow as well as the pressure increase produced by the propulsion jet can be improved.
A basic disadvantage of the jet suction pump 7 is the fact that it also produces a pressure loss in a forced flow mode. The multi-stage property produces a sharply adjusted pump 7 that has no propulsion jet in a case where the internal combustion engine works in non-charged operation.
In this case, the blow-by gas would have to be pressed through the small nozzles, producing a pressure loss that is not desirable. For an optimally constructed multi-stage jet suction pump 7, this pressure loss is significant (5 to 100 mbar depending on the volume flow). Since this drawback may exceed the benefit of the jet suction pump 7, at least one bypass valve 8 and/or one check valve 8 is provided for this application in a preferred embodiment according to the invention, which in a case where the jet suction pump 7 does not produce a propulsion jet, directs the blow-by gas past the pump 7 and thus minimizes the pressure loss for this case.
When the engine works in turbocharging operation, the valve 8 is closed because of the higher pressure downstream the jet suction pump 7. When the engine works in non-charged operation, the blow-by gas can flow past the pump 7 without a pressure loss.
Thus, this operation mode is optimized by a combination of the jet suction pump 7 with the bypass valve 8 and/or the check valve 8.
The pump 7 is preferably made of plastic, for example, polyamide. Parts of the pump may also be manifested within the cylinder head cover 10.
In another embodiment of the present invention, the jet suction pump 7 may also be integrated in a cylinder head cover 10.
Alternatively, the complete component may also prepared as a module consisting of the jet suction pump 7 with the bypass valve 8 and/or the check valve 8 with hose connectors.
Number | Date | Country | Kind |
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10 2015 200 341 | Jan 2015 | DE | national |
Filing Document | Filing Date | Country | Kind |
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PCT/EP2016/050164 | 1/7/2016 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2016/113166 | 7/21/2016 | WO | A |
Number | Name | Date | Kind |
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267022 | Schutte | Nov 1882 | A |
742618 | Eynon | Oct 1903 | A |
1138125 | Leblanc | May 1915 | A |
20110073082 | Hattori et al. | Mar 2011 | A1 |
20150053188 | Kuribayashi et al. | Feb 2015 | A1 |
20150240732 | Makihara | Aug 2015 | A1 |
20150316074 | Tell | Nov 2015 | A1 |
20160319732 | Iwata | Nov 2016 | A1 |
Number | Date | Country |
---|---|---|
103930656 | Aug 2016 | CN |
92 10 497 | Dec 1993 | DE |
44 00 958 | Apr 1995 | DE |
198 08 548 | Sep 1999 | DE |
20 2006 001 287 | Jun 2007 | DE |
10 2010 043 060 | May 2012 | DE |
10 2013 202 348 | Aug 2013 | DE |
11 2011 105 854 | Aug 2014 | DE |
10 2013 203 942 | Sep 2014 | DE |
10 2014 218 822 | Mar 2015 | DE |
2 505 798 | Oct 2012 | EP |
2811127 | Dec 2014 | EP |
2013153096 | Oct 2013 | WO |
2014060831 | Apr 2014 | WO |
Entry |
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International Search Report for International Application No. PCT/EP2016/050164 dated Apr. 13, 2016. |
Number | Date | Country | |
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20180274410 A1 | Sep 2018 | US |