Methods and systems for increasing airflow through a charge air cooler to decrease charge air cooler condensate
US-2016169170-A1 · Jun 16, 2016 · US
US9890691B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9890691-B2 |
| Application number | US-201514829968-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 19, 2015 |
| Priority date | Aug 19, 2015 |
| Publication date | Feb 13, 2018 |
| Grant date | Feb 13, 2018 |
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Methods and systems for operating an engine that includes a compressor and charge air cooler are disclosed. In one example, air flow through the charge air cooler is increased in response to condensation accumulating in the charge air cooler without increasing engine torque. Air flow through the charge air cooler is increased to gradually reduce condensation within the charge air cooler.
Opening claim text (preview).
The invention claimed is: 1. A method for operating engine compressors, comprising: passing air through a first compressor and a second compressor in an engine air intake; and returning a portion of air passing through the second compressor to the engine air intake downstream of the first compressor and upstream of the second compressor via a controller opening a charge air cooler bypass valve, where the portion of air passing through the second compressor to the engine air intake downstream of the first compressor and upstream of the second compressor is returned in response to the controller estimating an amount of condensation in a charge air cooler greater than a threshold while operating an engine after determining engine operating conditions via sensors coupled to the controller, the amount of condensation estimated via the sensors. 2. The method of claim 1 , where the first compressor is a turbocharger compressor, and where the second compressor is an electrically driven compressor. 3. The method of claim 1 , further comprising increasing a speed of the second compressor via the controller in response to an indication of condensation in the charge air cooler greater than the threshold. 4. The method of claim 1 , further comprising returning the portion of air passing through the second compressor to an inlet of the charge air cooler. 5. The method of claim 1 , where the charge air cooler bypass valve bypasses the charge air cooler, and where the portion of air passing through the second compressor is returned in response to a charge air cooler condensation estimate that is based on output of a humidity sensor. 6. The method of claim 5 , where the charge air cooler condensation estimate is further based on air temperature and charge air cooler temperature sensor inputs to the controller. 7. A method for operating engine compressors, comprising: passing air through a first compressor and a second compressor in an engine air intake; and increasing flow of air passing through the second compressor via increasing speed of the second compressor and returning air to the engine air intake downstream of the first compressor and upstream of the second compressor via opening a charge air cooler bypass valve via a controller in response to a controller estimate of condensation in a charge air cooler exceeding a threshold while operating an engine after determining engine operating conditions via sensors coupled to the controller, the speed of the second compressor increased via the controller. 8. The method of claim 7 , further comprising closing an electric compressor bypass valve via the controller in response to the controller estimate of condensation in the charge air cooler, the controller estimate of condensation in the charge air cooler based on inputs from the sensors coupled to the controller. 9. The method of claim 8 , further comprising opening the electric compressor bypass valve and deactivating the second compressor via the controller in response to a controller determined desired engine air flow being greater than a threshold when the controller estimate of condensation exceeds the threshold, the controller determined desired engine air flow based on the inputs from the sensors coupled to the controller. 10. The method of claim 9 , further comprising closing the charge air cooler bypass valve via the controller in response to the controller determined desired engine air flow being greater than the threshold, the controller determined desired engine air flow based on the inputs from the sensors coupled to the controller. 11. The method of claim 7 , further comprising increasing a throttle inlet pressure via the controller in response to an increase in the controller estimate of condensation in the charge air cooler, the controller estimate of condensation in the charge air cooler based on inputs from the sensors coupled to the controller. 12. The method of claim 7 , further comprising decreasing a throttle inlet pressure via the controller in response to a decrease in the controller estimate of condensation in the charge air cooler, the controller estimate of condensation in the charge air cooler based on inputs from the sensors coupled to the controller. 13. The method of claim 7 , where the speed of the second compressor is increased via the controller to increase flow of air passing through the second compressor. 14. An engine system, comprising: an engine including an air intake; an exhaust gas driven compressor positioned along the air intake; an electrically driven compressor posited along the air intake downstream of the exhaust gas driven compressor; a charge air cooler including a charge air cooler bypass passage and a charge air cooler bypass valve; and a controller including non-transitory instructions to open the charge air cooler bypass valve in response to the controller estimating an amount of condensation in the charge air cooler exceeding a threshold while operating the engine after determining engine operating conditions via sensors coupled to the controller, the controller estimated amount of condensation in the charge air cooler based on inputs from the sensors coupled to the controller. 15. The engine system of claim 14 , further comprising an electrically driven compressor bypass passage and an electrically driven compressor bypass valve. 16. The engine system of claim 15 , further comprising additional non-transitory instructions to close the electrically driven compressor bypass valve in response to the controller estimating the amount of condensation in the charge air cooler exceeding the threshold, the controller estimated amount of condensation in the charge air cooler based on the inputs from the sensors coupled to the controller. 17. The engine system of claim 14 , further comprising additional non-transitory instructions to adjust a throttle inlet pressure in response to the controller estimating the amount of condensation in the charge air cooler, the controller estimated amount of condensation in the charge air cooler based on the inputs from the sensors coupled to the controller. 18. The engine system of claim 17 , further comprising additional non-transitory instructions to adjust the throttle inlet pressure in response to an engine air flow or a driver demand torque determined via the sensors coupled to the controller. 19. The engine system of claim 14 , further comprising additional non-transitory instructions to increase air flow through the charge air cooler via the electrically driven compressor while maintaining a substantially constant engine torque.
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