Diagnostic method for a compressor recirculation valve
US-2018112591-A1 · Apr 26, 2018 · US
US10962019B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10962019-B2 |
| Application number | US-201715697608-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 7, 2017 |
| Priority date | Dec 8, 2014 |
| Publication date | Mar 30, 2021 |
| Grant date | Mar 30, 2021 |
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Methods are provided for identifying degradation in components of a compressor recirculation valve (CRV). One method may include inferring degradation of the CRV based on adaptation of a compressor surge line outside an expected range.
Opening claim text (preview).
The invention claimed is: 1. A method for an engine, comprising: indicating degradation of a compressor recirculation valve based on a surge line adaptation of a surge line on a compressor map stored in a controller of the engine being outside an expected range for surge line adaptation. 2. The method of claim 1 , wherein the surge line adaptation is learned over one or more drive cycles of the engine; and wherein the expected range is defined by the left surge line boundary and the right surge line boundary. 3. The method of claim 2 , wherein learning the surge line adaptation includes learning a range of the surge line adaptations including a left surge line boundary and a right surge line boundary. 4. The method of claim 3 , wherein indicating degradation comprises indicating a compressor recirculation valve opening amount is less than a desired amount based on the surge line being adapted to a right side of the right surge line boundary. 5. The method of claim 4 , wherein indicating degradation comprises indicating the compressor recirculation valve opening amount is greater than the desired amount based on the surge line being adapted to a left side of the left surge line boundary. 6. The method of claim 3 , wherein the surge line adaptation is learned based on one or more of a compressor surge event, a number of surge events, a tip-out greater than a threshold amount and the compressor not surging during the tip-out, and a number of tip-outs, each tip-out greater than the threshold amount and the compressor not surging during each of the tip-outs. 7. The method of claim 6 , wherein the surge is detected based on a frequency of a throttle position sensor being greater than a threshold frequency, the sensor located downstream of the compressor. 8. The method of claim 6 , wherein the surge line is adapted to the left of an initial surge line in response to the number of tip-outs being greater than a threshold number of tip-outs. 9. The method of claim 6 , wherein the surge line is adapted to the right of an initial surge line in response to the number of surge events being greater than a threshold number of surge events. 10. An engine system comprising: an engine; a turbocharger for providing a boosted aft charge to the engine, the turbocharger including an exhaust turbine and an intake compressor; a continuously variable recirculation valve coupled across the compressor; a throttle coupled to the intake, downstream of the compressor; a throttle inlet pressure sensor located downstream of the compressor and upstream of the throttle; and a controller with computer readable instructions for, adapting a surge line of a compressor map stored in a memory of the controller based on at least one of a plurality of surge events and a plurality of tip-outs over one or more drive cycles of the engine; and detecting degradation of the continuously variable recirculation valve based on the adaptation of the surge line. 11. The system of claim 10 , wherein the controller includes further instructions for indicating the recirculation valve is stuck closed in response to an area to the left of the surge line being greater than a first threshold area. 12. The system of claim 11 , wherein the controller includes further instructions for indicating the recirculation valve is stuck open in response to an area to the left of the surge line being less than a second threshold area.
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